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Seismic vulnerability of existing RC buildings - Dipartimento di ...

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A Mamma, Papà e Titti


ACKNOWLEDGEMENTSI chose to deal with structural engineering wishing to give my personal contribution to thedevelopment and the protection <strong>of</strong> what man builds, becoming a place to live and a sign <strong>of</strong> hispassage.After my graduation, I had the opportunity to attend a PhD programme in <strong>Seismic</strong> Risk. It wasthe most special work I could ever do: when you make research, everything you do is aimed atleaving a sign, changing things and making them advance.During these years, I have been making research on seismic <strong>vulnerability</strong> <strong>of</strong> <strong>existing</strong> <strong>RC</strong><strong>buil<strong>di</strong>ngs</strong>. When I was in L’Aquila, in April 2009, I saw with my own eyes the pain and sorrowthat an earthquake can leave behind, and I understood that I was making the right thing puttingmy energy and time into this field.I first have to express my gratitude to Gerardo Mario Verderame, the man who guided meduring these years. He not only taught me everything I know about structural engineering. Healso taught me what research is, and how paying attention to everything and working hard canmake the <strong>di</strong>fference in this work. Above all, he always respected my character, which is muchmore tough than it may appear, and he always let me free to follow my inclinations.I express my thanks to Pr<strong>of</strong>essor Gaetano Manfre<strong>di</strong> for the opportunity he gave me to be part <strong>of</strong>the Department <strong>of</strong> Structural Engineering <strong>of</strong> the University <strong>of</strong> Naples Federico II.I would like to thank Matjaž Dolšek and Daniel Celarec for the opportunity they gave me towork together during my stay at the University <strong>of</strong> Ljubljana. They helped me in exten<strong>di</strong>ng myresearch on <strong>RC</strong> structures; the first results <strong>of</strong> this cooperation are included in this thesis.Special thanks to Marilena Esposito and Filippo Sansiviero; they <strong>of</strong>ten provided a great supportto my research activities.I would like to thank Giovanni De Carlo for his fundamental contribution to the review <strong>of</strong>beam-column joint models and, more generally, to the experimental and numerical research onthe behaviour <strong>of</strong> <strong>RC</strong> elements reported in this thesis. About two years ago we took <strong>di</strong>fferentways. It was too early. I will always remember with great pleasure the many long, enjoyable andstimulating <strong>di</strong>scussions we had, which deeply influenced my vision <strong>of</strong> structural engineering.During these years, I <strong>of</strong>ten put work at the first place, leaving too little time to the mostimportant people in my life. Despite this, they still stand close to me. Salvatore and Angela, Igive you not only my gratitude, but also my apologies.My deepest gratitude goes to the love <strong>of</strong> who was closest to me, giving me times full <strong>of</strong>happiness and making me a <strong>di</strong>fferent man. This is much more important to me than anythingthat could ever be written down on paper.Naples, December 2010


IndexIndexIntroduction 1Chapter IAssessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>1.1 INTRODUCTION 51.2 EMPIRICAL METHODS 81.2.1. Damage Probability Matrices 8Whitman et al., 1973 8Braga et al., 1982 9Di Pasquale et al., 2005 9Dolce et al., 2003 9EMS-98 scale (Grünthal, 1998) 10Giovinazzi and Lagomarsino, 2004 131.2.2. Continuous <strong>vulnerability</strong> curves 13Orsini, 1999 13Sabetta et al., 1998 13Rota et al., 2008 131.2.3. Vulnerability Index method 14Benedetti and Petrini, 1984 14i


Index1.2.4. Screening methods 15JBDPA, 1990 15Hassan and Sozen, 1997 16Yakut, 2004 16Ozdemir et al., 2005 161.3 ANALYTICAL METHODS 17Singhal and Kiremidjian, 1996 17Masi, 2003 20Rossetto and Elnashai, 2005 21Cosenza et al., 2005 21Iervolino et al., 2007 23HAZUS (FEMA, 2001) 24Giovinazzi, 2005 30Grant et al., 2006 31Ordaz et al., 2000 32Calvi, 1999 32DBELA (Pinho et al., 2002) 34SP-BELA (Borzi et al., 2008) 36VC (Dolce and Moroni, 2005) 381.4 HYBRID METHODS 40Kappos et al., 1995 40Singhal and Kiremidjian, 1998 401.5 EXPERT JUDGEMENT-BASED METHODS 41ATC, 1985 41REFERENCES 42ii


IndexChapter II<strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>2.1 GENERAL REMARKS 492.2 MEMBERS CONTROLLED BY FLEXURAL AND AXIAL LOADS 532.2.1. Code provisions for the assessment <strong>of</strong> ultimate deformationcapacity 532.2.1.1. EC8 part 3.3 – empirical approach 552.2.1.2. EC8 part 3.3 – mechanical approach 612.2.1.3. ASCE/SEI 41 approach 662.2.1.4. Critical review 712.2.2. A proposal for a new correction coefficient applied to the EC8capacity formulation for <strong>RC</strong> columns with smooth bars 742.2.2.1. Deformation capacity <strong>of</strong> <strong>RC</strong> columns with smooth bars 752.2.2.2. Calibration <strong>of</strong> correction factor 762.2.2.3. Discussion <strong>of</strong> results 812.2.3. Bond behaviour <strong>of</strong> smooth bars: experimental and analyticalinvestigation 842.2.4. The influence <strong>of</strong> transverse reinforcement anchorage detail onconfined concrete behaviour 892.2.5. Numerical modelling <strong>of</strong> <strong>RC</strong> members with smooth bars 922.3 MEMBERS CONTROLLED BY SHEAR 962.4 BEAM-COLUMN JOINTS 1022.5 STRUCTURAL PERFORMANCE OF <strong>RC</strong> BUILDINGS AFTER THE6TH APRIL 2009 L’AQUILA EARTHQUAKE, ITALY 1082.5.1. Reinforced concrete <strong>buil<strong>di</strong>ngs</strong> in L’Aquila 1082.5.2. Overview <strong>of</strong> past seismic code provisions 1112.5.3. Spectral considerations 1152.5.4. Field survey <strong>of</strong> structural damage 118iii


IndexREFERENCES 127Chapter IIIInfluence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete<strong>buil<strong>di</strong>ngs</strong>3.1 INTRODUCTION 1373.2 BEHAVIOUR OF <strong>RC</strong> FRAMES WITH MASONRY INFILLS 1383.2.1. Influence <strong>of</strong> openings 1443.2.2. Brittle failure in <strong>RC</strong> members due to local interaction with infills 1453.2.3. Out-<strong>of</strong>-plane behaviour 1483.2.4. Models for the analysis <strong>of</strong> infilled <strong>RC</strong> frames 1483.3 EXPERIMENTAL BEHAVIOUR OF INFILLED <strong>RC</strong> STRUCTURES 1593.4 ANALYTICAL INVESTIGATION OF ELASTIC PERIODOF INFILLED <strong>RC</strong> MRF BUILDINGS 1763.4.1. The period <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> 1763.4.1.1 Empirical estimate <strong>of</strong> period <strong>of</strong> <strong>RC</strong> MRF <strong>buil<strong>di</strong>ngs</strong> 1773.4.1.2 Empirical estimate <strong>of</strong> period <strong>of</strong> <strong>RC</strong> SW <strong>buil<strong>di</strong>ngs</strong> 1783.4.1.3 Empirical estimate <strong>of</strong> period <strong>of</strong> infilled <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> 1793.4.1.4 Numerical estimate <strong>of</strong> period <strong>of</strong> infilled <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> 1813.4.2. Modelling <strong>of</strong> infill stiffness 1823.4.3. Numerical estimate <strong>of</strong> period <strong>of</strong> infilled <strong>RC</strong> MRF <strong>buil<strong>di</strong>ngs</strong> 1863.4.3.1 Buil<strong>di</strong>ng population 1863.4.3.2 Evaluation <strong>of</strong> period 1893.4.4. Analysis <strong>of</strong> results 1903.4.4.1. Uncracked infills 191iv


Index3.4.4.2. Cracked infills 2003.4.5. Comparison with literature formulas 203REFERENCES 208Chapter IVNumerical investigation <strong>of</strong> seismic capacity <strong>of</strong> reinforcedconcrete <strong>buil<strong>di</strong>ngs</strong> with infills4.1 INTRODUCTION 2174.2 NUMERICAL INVESTIGATION OF SEISMIC BEHAVIOUR OFINFILLED <strong>RC</strong> BUILDINGS:STATE OF THE ART 2184.3 SEISMIC CAPACITY ASSESSMENT OF A FOUR-STOREY GLDBUILDING WITH DIFFERENT INFILL CONFIGURATIONS 2284.3.1. Case study structure: numerical modelling and analysismethodology 2284.3.2. Sensitivity analysis 2364.3.2.1. Uniformly Infilled frame 2394.3.2.2. Pilotis frame 2544.3.2.3. Bare frame 2654.3.3. Comparison between <strong>di</strong>fferent infill configurations 2744.3.3.1. Comparison between <strong>di</strong>fferent infill configurations:IN2 curves 2744.3.3.2. Comparison between <strong>di</strong>fferent infill configurations:fragility curves 2794.3.4. Comparison with simplified models based on Shear-Typeassumption 2894.3.4.1. Uniformly infilled frame 290v


Index4.3.4.2. Pilotis frame 2944.3.4.3. Bare frame 2974.3.4.4. Summary <strong>of</strong> remarks 303REFERENCES 304Chapter VSimplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong><strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>: the case study <strong>of</strong> Avellino5.1 INTRODUCTION 3095.2 A SIMPLIFIED PROCEDURE FOR THE ASSESSMENTOF SEISMIC VULNERABILITY OF <strong>RC</strong> BUILDINGS 3105.2.1. Definition <strong>of</strong> input data 3105.2.2. Simulated design procedure 3125.2.3. Characterization <strong>of</strong> nonlinear response 3155.2.4. Calculation <strong>of</strong> pushover curve 3185.2.5. <strong>Seismic</strong> assessment 3215.2.6. Evaluation <strong>of</strong> fragility curves 3225.2.7. Calculation <strong>of</strong> failure probability 3255.2.8. Example applications 3265.3 URBAN SCALE VULNERABILITY ASSESSMENT:THE CASE STUDY OF AVELLINO 3385.3.1. Data collection and field survey results 3385.3.1.1. Survey form 3385.3.1.2. Analysis <strong>of</strong> buil<strong>di</strong>ng stock data 3475.3.2. <strong>Seismic</strong> <strong>vulnerability</strong> assessment <strong>of</strong> <strong>RC</strong> buil<strong>di</strong>ng stock 356vi


Index5.3.2.1. Input data <strong>of</strong> the seismic <strong>vulnerability</strong> assessmentprocedure 3565.3.2.2. Analysis <strong>of</strong> results 3635.4 FUTURE RESEA<strong>RC</strong>H 378REFERENCES 379vii


1IntroductionThe assessment <strong>of</strong> seismic <strong>vulnerability</strong> <strong>of</strong> the <strong>existing</strong> buil<strong>di</strong>ng stock plays akey role in the development <strong>of</strong> instruments aimed at the evaluation and themitigation <strong>of</strong> seismic risk. The investigation <strong>of</strong> seismic <strong>vulnerability</strong> <strong>of</strong> <strong>existing</strong>Reinforced Concrete (<strong>RC</strong>) <strong>buil<strong>di</strong>ngs</strong> is <strong>of</strong> fundamental importance since thisbuil<strong>di</strong>ng typology represents a large part <strong>of</strong> the <strong>existing</strong> buil<strong>di</strong>ng stock in manyareas subjected to high seismic risk; moreover, the seismic behaviour <strong>of</strong> these<strong>buil<strong>di</strong>ngs</strong> is <strong>of</strong>ten affected by deficiencies due to the absence <strong>of</strong> compliancewith the modern earthquake engineering design principles or, even, to theabsence <strong>of</strong> a seismic design.In this thesis, the seismic <strong>vulnerability</strong> <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> isinvestigated from <strong>di</strong>fferent points <strong>of</strong> view.First, an overview <strong>of</strong> literature methods is carried out, illustrating mainempirical and analytical approaches to large scale <strong>vulnerability</strong> assessment(Chapter I).Hence, in Chapter II the seismic behaviour <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> isinvestigated through experimental and numerical activities focused on thedeformation capacity <strong>of</strong> substandard <strong>RC</strong> members, with emphasis on memberswith smooth bars. To this aim, code and literature formulations for theevaluation <strong>of</strong> deformation capacity <strong>of</strong> <strong>RC</strong> members are illustrated and<strong>di</strong>scussed; then, based on experimental data, a new proposal for the assessment<strong>of</strong> deformation capacity <strong>of</strong> columns with smooth bars is presented. Then, bondbetween steel and concrete for this kind <strong>of</strong> reinforcement is investigatedthrough an experimental study and the formulation <strong>of</strong> an analytical model basedon the obtained data. The influence <strong>of</strong> the absence <strong>of</strong> proper transversereinforcement details is experimentally investigated, too. Finally, the so-called


Type assumption. The proposed method employs few data – such as number <strong>of</strong>storeys, global <strong>di</strong>mensions and type <strong>of</strong> design – to define the structural modelby means <strong>of</strong> a simulated design procedure. Nonlinear static response <strong>of</strong> thestructural model, inclu<strong>di</strong>ng infill elements, is characterized, and pushoveranalysis is carried out in closed-form. Fragility curves and correspon<strong>di</strong>ng failureprobability at <strong>di</strong>fferent Limit States are calculated, once seismic hazard hasbeen defined. Finally, the proposed method is applied to the Avellino city(southern Italy), employing data about buil<strong>di</strong>ng stock from a field survey,inclu<strong>di</strong>ng structural typology, global buil<strong>di</strong>ng <strong>di</strong>mensions and age <strong>of</strong>construction. Obtained results show the influence <strong>of</strong> main characteristics, suchas the number <strong>of</strong> storeys and type <strong>of</strong> design, on the seismic <strong>vulnerability</strong> <strong>of</strong> thebuil<strong>di</strong>ng stock.3


6 Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>Loss models provide the expected losses at a given site <strong>of</strong> interest and in agiven time window by convolving the seismic hazard, the <strong>vulnerability</strong> <strong>of</strong> thestructures and infrastructures composing the built environment and the exposedvalue (accounting for costs <strong>of</strong> repair or replacement <strong>of</strong> structures, contentslosses and interruption <strong>of</strong> activities due to the loss <strong>of</strong> functionality).In this framework, structural <strong>vulnerability</strong> is given by methodologies whichprovide the probability <strong>of</strong> a given level <strong>of</strong> damage as a function <strong>of</strong> a parameterrepresenting the seismic intensity (e.g., macroseismic intensity, Peak GroundAcceleration (PGA)). A method for the assessment <strong>of</strong> seismic <strong>vulnerability</strong> <strong>of</strong> abuil<strong>di</strong>ng stock has to represent the best compromise between reliability andreasonable demand <strong>of</strong> computational effort, depen<strong>di</strong>ng on the availability <strong>of</strong>data (that is, the availability <strong>of</strong> time and money necessary to gather them) andon the required level <strong>of</strong> detail.A fundamental <strong>di</strong>stinction has to be made between empirical and analytical<strong>vulnerability</strong> methods: in empirical methods the assessment <strong>of</strong> expecteddamage for a given buil<strong>di</strong>ng typology is based on the observation <strong>of</strong> damagesuffered during past seismic events; in analytical methods the relationshipbetween seismic intensity and expected damage is provided by a model with<strong>di</strong>rect physical meaning.Reliability and significance <strong>of</strong> observed data allow empirical methods togive a realistic in<strong>di</strong>cation about expected damage, provided they are applied toa buil<strong>di</strong>ng stock with similar characteristic compared with the one used for theirconstruction. However, <strong>di</strong>fferent <strong>di</strong>sadvantages come from the use <strong>of</strong> empiricalmethods. These methods do not allow to account for the vibrationcharacteristics <strong>of</strong> the <strong>buil<strong>di</strong>ngs</strong>. They do not explicitly model the <strong>di</strong>fferentsources <strong>of</strong> uncertainty, thus not allowing to remove the uncertainty in theseismic demand from the <strong>vulnerability</strong> assessment. A macroseismic measure is<strong>of</strong>ten used to define the seismic intensity, but macroseismic intensity is, in turn,obtained from observed damage, thus seismic intensity and damage are notindependent (Crowley et al., 2009). The collection <strong>of</strong> data about buil<strong>di</strong>ngdamage after a seismic event, required for the derivation <strong>of</strong> any empirical


Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 7relationship between seismic intensity and expected damage, is affected by<strong>di</strong>fferent shortcomings such as a not homogeneous availability <strong>of</strong> data, resultingin a higher statistical reliability for the low damage/ground motion rangecompared with the high damage/ground motion range, or the errors due toinadequate compilation <strong>of</strong> the post-earthquake assessment forms (Colombi etal., 2008). Also, empirical methods do not allow to model the influence <strong>of</strong>retr<strong>of</strong>it solutions on <strong>vulnerability</strong>, given by the improvement in structuralresponse.On the contrary, the use <strong>of</strong> an algorithm to evaluate the structural<strong>vulnerability</strong> allows to take into account <strong>di</strong>rectly and transparently, in a detailedway, the various characteristics <strong>of</strong> buil<strong>di</strong>ng stock, and also to explicitly accountfor the uncertainties involved in the assessment procedure. An analyticalapproach allows to include in the <strong>vulnerability</strong> assessment structurescharacterized by <strong>di</strong>fferent (or new) construction practices, as well as to considerthe influence <strong>of</strong> retr<strong>of</strong>itting on the response <strong>of</strong> <strong>existing</strong> structures. Furthermore,analytical methods can take advantage <strong>of</strong> advances in seismic hazardassessment, such as the derivation <strong>of</strong> seismic hazard maps in terms <strong>of</strong> spectralor<strong>di</strong>nates (e.g., INGV-DPC S1, 2007), <strong>di</strong>fferent from macroseismic intensity orPGA. However, generally speaking analytical methods need a larger amount <strong>of</strong>detailed data and a higher computational effort, compared with empiricalmethods. Therefore, the effective increase in accuracy <strong>of</strong> <strong>vulnerability</strong>assessment, when analytical methods are adopted, should be checked by means<strong>of</strong> a comparison with observed damage data. Further critical issues in theapplication <strong>of</strong> analytical methods have to be carefully considered: first <strong>of</strong> all,the degree <strong>of</strong> confidence in the capability <strong>of</strong> a numerical model to accuratelypre<strong>di</strong>ct the response <strong>of</strong> real structures and, in particular, the confidence in thecorrelation between the assumed analytical damage index (such as theinterstorey drift or a cyclic damage index) and the actual structural damage.Also, many <strong>of</strong> the collapses observed after seismic events are due toconstructive errors and deficiencies, which normally are not considered in ananalytical model (e.g., Verderame et al., 2010).


8 Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>Empirical and analytical methods can be used complementing each other, ashappens in so-called “hybrid” methods. Moreover, relationships betweenseismic intensity and expected damage for <strong>di</strong>fferent structural typologies canalso be based on expert-judgement.A very comprehensive and detailed review <strong>of</strong> seismic <strong>vulnerability</strong>assessment methodologies can be found in (Calvi et al., 2006). In the following,main <strong>vulnerability</strong> assessment procedures are illustrated, referring toReinforced Concrete (<strong>RC</strong>) <strong>buil<strong>di</strong>ngs</strong>.1.2 EMPIRICAL METHODSFirst developments <strong>of</strong> seismic <strong>vulnerability</strong> assessment <strong>of</strong> buil<strong>di</strong>ng stockstook place in 1970s, through empirical methods based on macroseismicintensity; at the time, the major part <strong>of</strong> hazard maps adopted this kind <strong>of</strong>measure for the seismic intensity.Different types <strong>of</strong> empirical methods for the seismic <strong>vulnerability</strong>assessment <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong> can be <strong>di</strong>stinguished:− Damage Probability Matrices (DPMs), expressing in a <strong>di</strong>screte formthe con<strong>di</strong>tional probability <strong>of</strong> reaching a damage level D = j due to aground motion <strong>of</strong> intensity I = i, P ij = P [ D = j | I = i ];− <strong>vulnerability</strong> functions, expressing in a continuous form theprobability P ij = P [ D ≥ j | I = i ];− methods based on a so-called “Vulnerability Index”;− screening methods.1.2.1. Damage Probability MatricesFirst DPMs have been proposed in (Whitman et al., 1973), see Figure1.2.1.1. for a given structural typology, the probability <strong>of</strong> being in a given state<strong>of</strong> structural and non-structural damage is provided. For each damage state, thedamage ratio is provided too, representing the ratio between the cost <strong>of</strong> repairand the cost <strong>of</strong> replacement. These DPMs are compiled for <strong>di</strong>fferent structural


10 Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>1998).Figure 1.2.1.2. Vulnerability classes adopted in (Di Pasquale et al., 2005)Accor<strong>di</strong>ng to EMS-98 scale six <strong>vulnerability</strong> buil<strong>di</strong>ng classes (A to F, seeFigure 1.2.1.3) are defined, then for each class a qualitative description ( “few”,“many” and “most”, see Figure 1.2.1.4) <strong>of</strong> the proportion <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong> sufferinga given level <strong>of</strong> damage (1 to 5, see Figure 1.2.1.5) is provided as a function <strong>of</strong>the seismic intensity level, ranging from V to XII. Hence, DPMs are implicitlydefined in EMS-98 scale. Nevertheless, they are incomplete (the proportion <strong>of</strong><strong>buil<strong>di</strong>ngs</strong> suffering a given damage level for a given seismic intensity is notprovided for all possible combinations <strong>of</strong> damage levels and seismic intensities)and vague (proportion <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong> is described only qualitatively)


Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 11Figure 1.2.1.3. Vulnerability classes accor<strong>di</strong>ng to EMS-98 scale (Grünthal, 1998)Figure 1.2.1.4. Definition <strong>of</strong> quantities “few”, “many” and “most” accor<strong>di</strong>ng to EMS-98 scale(Grünthal, 1998)


12 Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>Figure 1.2.1.5. Definition <strong>of</strong> damage grades to <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> accor<strong>di</strong>ng to EMS-98 scale(Grünthal, 1998)


Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 13Giovinazzi and Lagomarsino (2004) start from these matrices and overcometheir limits <strong>of</strong> incompleteness and vagueness, then relate the obtained DPMs tothe buil<strong>di</strong>ng stock through a <strong>vulnerability</strong> index.1.2.2. Continuous <strong>vulnerability</strong> curvesRelationships between seismic intensity and expected damage based onempirical data can also be derived in a continuous form.Orsini (1999) elaborates the data <strong>of</strong> the damage survey carried out after the1980 Irpinia earthquake in order to evaluate, for each municipality, a value <strong>of</strong>seismic intensity accor<strong>di</strong>ng to the Parameterless Scale <strong>of</strong> Intensity (PSI)proposed by Spence et al. (1991). The main hypothesis at the basis <strong>of</strong> the PSImodel is that the intensity at which the structures belonging to a single<strong>vulnerability</strong> class overcome a given damage threshold is continuously<strong>di</strong>stributed accor<strong>di</strong>ng to a Gaussian model. The use <strong>of</strong> PSI allows the definition<strong>of</strong> continuous <strong>vulnerability</strong> functions depen<strong>di</strong>ng on a macroseismic intensityparameter, tackling the problem that macroseismic intensity is not a continuousvariable. After determining PSI values for each municipality, Orsini (1999)proposes <strong>vulnerability</strong> curves for apartment units as a function <strong>of</strong> thiscontinuous parameter.Sabetta et al. (1998) derive <strong>vulnerability</strong> curves depen<strong>di</strong>ng on PGA, AriasIntensity and effective peak acceleration based on the elaboration <strong>of</strong> about50000 buil<strong>di</strong>ng damage surveys from past Italian earthquakes, by calculatingfor each municipality a mean damage index as the weighted average <strong>of</strong> thefrequencies <strong>of</strong> each damage level for each structural class.Rota et al. (2008) select more than 91000 damage survey forms from pastItalian earthquakes out <strong>of</strong> a total amount <strong>of</strong> 164000 ones, (i) <strong>di</strong>sregar<strong>di</strong>ng thedata affected by important information missing and (ii) inclu<strong>di</strong>ng only datarelated to municipalities surveyed for at least 60%, thus avoi<strong>di</strong>ng a biasedsample. The authors sub<strong>di</strong>vide these data into 23 <strong>di</strong>fferent buil<strong>di</strong>ng typologiesand 10 ground motion intervals. Both PGA and Housner intensity areconsidered as ground motion parameters; their values are estimated for each


14 Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>municipality using the attenuation law <strong>of</strong> Sabetta and Pugliese (1987, 1996) forrock con<strong>di</strong>tions, with the parameters (magnitude and epicentral coor<strong>di</strong>nates) <strong>of</strong>the earthquake <strong>of</strong> interest. The adopted damage scale is similar to the EMS-98scale, consisting <strong>of</strong> five levels <strong>of</strong> damage plus the case <strong>of</strong> no damage. DPMs areextracted from the data for all <strong>of</strong> the 23 considered <strong>vulnerability</strong> classes,accor<strong>di</strong>ng to the defined damage scale and seismic intensity scale. Hence,continuous <strong>vulnerability</strong> curves are obtained by fitting with lognormal<strong>di</strong>stributions the data evaluated in form <strong>of</strong> DPMs; also, when carrying out thisfitting, for each sample (given a buil<strong>di</strong>ng class, a seismic intensity and adamage level) the inverse <strong>of</strong> the estimated standard deviation is used as aweight expressing the reliability <strong>of</strong> the single sample.It is to be noted that when the seismic intensity is measured by means <strong>of</strong> aparameter related to the spectral acceleration or spectral <strong>di</strong>splacement at thefundamental period <strong>of</strong> vibration (e.g., Rossetto and Elnashai, 2003), <strong>di</strong>fferentfrom macroseismic intensity or PGA, the <strong>vulnerability</strong> curves show a betterpre<strong>di</strong>ction capacity, because taking into consideration the relationship betweenthe frequency content <strong>of</strong> the ground motion and the dynamic characteristics <strong>of</strong>the buil<strong>di</strong>ng stock.1.2.3. Vulnerability Index methodThe “Vulnerability Index” method is first proposed in (Benedetti andPetrini, 1984; GNDT, 1993). The index I v is evaluated by means <strong>of</strong> a fieldsurvey form where “scores” K i (from A to D) are assigned to eleven parametershaving a high influence on buil<strong>di</strong>ng <strong>vulnerability</strong> (e.g., plan and elevationconfiguration, type <strong>of</strong> foundation, structural and non-structural elements); then,the index is defined as the weighted sumI11= ∑ K W(1.2.3.1)v i ii=1accor<strong>di</strong>ng to the importance assigned to each parameter.Based on observed damage data from past earthquakes, for <strong>di</strong>fferent values <strong>of</strong>


Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 15this <strong>vulnerability</strong> index a relationship can be calibrated between seismicintensity and damage ratio (see Figure 1.2.3.1).Figure 1.2.3.1. Vulnerability functions to relate damage ratio and PGA for <strong>di</strong>fferent values <strong>of</strong><strong>vulnerability</strong> index (adapted from Guagenti and Petrini (1989)) (from (Calvi et al., 2006))The use <strong>of</strong> Vulnerability Index Method was quite widespread; it was alsoadopted in <strong>di</strong>fferent projects such as RISK-UE (Mouroux and Le Brun, 2006)and “Progetto Catania” (Faccioli et al., 1999; Faccioli and Pessina, 2000).1.2.4. Screening methodsAccor<strong>di</strong>ng to the Japanese <strong>Seismic</strong> Index Method (JBDPA, 1990), theseismic performance <strong>of</strong> the buil<strong>di</strong>ng is represented by a seismic performanceindex, I S , evaluated by means <strong>of</strong> a screening procedure. The procedure can becarried out accor<strong>di</strong>ng to three <strong>di</strong>fferent levels <strong>of</strong> detail. I S is calculated for eachstorey in every frame <strong>di</strong>rection accor<strong>di</strong>ng to the following expression:I= E S T(1.2.4.1)S 0 Dwhere E 0 , S D and T correspond to the basic structural performance, to thestructural design and to the time-dependent deterioration <strong>of</strong> the buil<strong>di</strong>ng,respectively. E 0 is given by the product between C and F, respectively


16 Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>representing the ultimate strength and the ductility <strong>of</strong> the buil<strong>di</strong>ng, depen<strong>di</strong>ngon the failure mode, the total number <strong>of</strong> storeys and the position <strong>of</strong> theconsidered storey. S D accounts for irregularity in stiffness and/or mass<strong>di</strong>stribution. A field survey is needed to define T. The calculated seismicperformance index I S is compared with the seismic judgement index I S0 todetermine the degree <strong>of</strong> safety <strong>of</strong> the buil<strong>di</strong>ng. I S0 represents a storey shear forceand is given byIS0= E ZGU(1.2.4.2)Swhere E S conservatively increases with the decreasing accuracy <strong>of</strong> the screeningprocedure, Z is a zone index mo<strong>di</strong>fying the ground motion intensity assumed atthe site <strong>of</strong> the buil<strong>di</strong>ng, G accounts for local effects such as ground-buil<strong>di</strong>nginteraction or stratigraphic and topographic amplification and U is a kind <strong>of</strong>importance factor depen<strong>di</strong>ng on the function <strong>of</strong> the buil<strong>di</strong>ng. In the 1998revised version <strong>of</strong> the Japanese Buil<strong>di</strong>ng Standard Law the index IS0is taken asthe spectral acceleration (in terms <strong>of</strong> g) at the period <strong>of</strong> the considered buil<strong>di</strong>ng,and it should be <strong>di</strong>stributed along the height <strong>of</strong> the structure accor<strong>di</strong>ng to atriangular <strong>di</strong>stribution.Preliminary assessment methods based on screening procedures have beenproposed in Turkey, too, during last years. Some methods require the<strong>di</strong>mensions <strong>of</strong> the lateral load resisting elements to be defined: the “PriorityIndex” proposed by Hassan and Sozen (1997) is a function <strong>of</strong> a wall index (area<strong>of</strong> walls and infill panels <strong>di</strong>vided by total floor area) and a column index (area<strong>of</strong> columns <strong>di</strong>vided by total floor area); the “Capacity Index” proposed byYakut (2004) depends on orientation, size and material properties <strong>of</strong> the lateralload-resisting structural system as well as the quality <strong>of</strong> workmanship andmaterials and other features such as short columns and plan irregularities. The<strong>Seismic</strong> Safety Screening Method (SSSM) by Ozdemir et al. (2005) derivesfrom the Japanese <strong>Seismic</strong> Index Method (JBDPA, 1990): in this method, too,the seismic capacity <strong>of</strong> a buil<strong>di</strong>ng is represented by a seismic index value whichis a function <strong>of</strong> structural strength and ductility; this index value has to be


Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 17compared with a seismic demand index value – representing the seismic hazard<strong>of</strong> the zone where the buil<strong>di</strong>ng is located – for assessing the degree <strong>of</strong> safety <strong>of</strong>the buil<strong>di</strong>ng.1.3 ANALYTICAL METHODSSinghal and Kiremidjian (1996) estimate <strong>vulnerability</strong> curves and DPMs for<strong>di</strong>fferent <strong>RC</strong> frames (from Low-Rise, Mid-Rise and High-Rise classes,respectively) through nonlinear dynamic analyses and using the Monte Carlosimulation technique (see Figure 1.3.1).Figure 1.3.1. General framework <strong>of</strong> the methodology adopted in (Singhal and Kiremidjian,1996)The uncertainties associated with structural capacities and demands aremodelled. Uncertainty in capacity is simulated assuming as random variablesthe compressive strength <strong>of</strong> concrete and the yield strength <strong>of</strong> steel. Uncertaintyin seismic demands is accounted for by simulating 100 artificial time histories.Then, the con<strong>di</strong>tional probability <strong>of</strong> reaching or excee<strong>di</strong>ng a damage state given


18 Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>a ground motion intensity is determined by the Monte Carlo simulation method.100 Latin hypercube samples are used for the nonlinear dynamic analyses ateach ground motion level (expressed in terms <strong>of</strong> spectral acceleration value).After performing nonlinear dynamic analyses, for each level <strong>of</strong> ground motionthe statistics <strong>of</strong> the Park and Ang (1985) damage index are used to obtain theparameters <strong>of</strong> a lognormal probability <strong>di</strong>stribution function at that groundmotion level (see Figure 1.3.2).Figure 1.3.2. Probability <strong>di</strong>stribution <strong>of</strong> Park and Ang’s damage index at S a =3g (Singhal andKiremidjian, 1996)The lognormal probability functions at each level <strong>of</strong> ground motion are thenused to obtain the probabilities <strong>of</strong> reaching or excee<strong>di</strong>ng a damage state,adopting given threshold values for the <strong>di</strong>fferent damage states (see Figure1.3.3).


Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 19Figure 1.3.3. Ranges <strong>of</strong> Park and Ang's damage index for <strong>di</strong>fferent damage states (Singhal andKiremidjian, 1996)Discrete points representing the probabilities <strong>of</strong> <strong>di</strong>fferent damage states for agiven spectral acceleration value are evaluated from the probability<strong>di</strong>stributions <strong>of</strong> the damage measure. Hence, smooth <strong>vulnerability</strong> curves areobtained fitting lognormal <strong>di</strong>stribution functions to these points (see Figure1.3.4).Figure 1.3.4. Vulnerability curves for Mid-Rise frames (Singhal and Kiremidjian, 1996)The relationship between the Mo<strong>di</strong>fied Mercalli Intensity (MMI) and theaverage spectral acceleration (that is, the con<strong>di</strong>tional probability <strong>of</strong> a spectralacceleration at a specified MMI value) in each period band, which is assumedto be lognormal, is developed in the paper based on average spectral


20 Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>acceleration values <strong>of</strong> the ground motions recorded on firm sites and the MMIvalues from these earthquakes at the respective recor<strong>di</strong>ng stations (see Figure1.3.5).Finally, DPMs are evaluated from the fragility curves by calculating theprobability <strong>of</strong> reaching or excee<strong>di</strong>ng a given damage state for a given MMIintensity (see Figure 1.3.6). This probability is obtained by convolving (i) theprobability <strong>of</strong> reaching or excee<strong>di</strong>ng the given damage state for a specifiedMMI and spectral acceleration and (ii) the con<strong>di</strong>tional probability <strong>of</strong> a spectralacceleration at specified MMI.Figure 1.3.5. Correlation between MMI intensity and spectral acceleration over period range0.5-0.9 s (Singhal and Kiremidjian, 1996)Figure 1.3.6. Damage Probability Matrix for Mid-Rise frames (Singhal and Kiremidjian, 1996)


Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 21A similar approach is adopted in (Masi, 2003), where three main structuraltypologies are examined: bare frames, regularly infilled frames and pilotisframes, designed for gravity loads only. Structural models are generatedthrough a simulated design procedure considering current practice and codes inforce at the age <strong>of</strong> construction. Nonlinear dynamic analyses with groundmotions <strong>of</strong> various levels <strong>of</strong> intensity are carried out. Based on the obtainedresults, each type <strong>of</strong> buil<strong>di</strong>ng can be assigned to a <strong>di</strong>fferent <strong>vulnerability</strong> class<strong>of</strong> EMS-98 scale.Rossetto and Elnashai (2005) derive <strong>vulnerability</strong> curves for a low-riseinfilled <strong>RC</strong> frame with inadequate seismic provisions accor<strong>di</strong>ng to thefollowing methodology: a population <strong>of</strong> 25 <strong>buil<strong>di</strong>ngs</strong> is generated from a singlebuil<strong>di</strong>ng through consideration <strong>of</strong> material parameter uncertainty; uncertainty indemand is accounted for through the use <strong>of</strong> 30 <strong>di</strong>fferent accelerograms; for each<strong>of</strong> the generated <strong>buil<strong>di</strong>ngs</strong>, an adaptive pushover analysis is carried out, and theperformance point is found following the Capacity Spectrum framework <strong>of</strong>assessment, for all the accelerograms; a damage scale experimentally calibratedto maximum inter-storey drift is adopted. Hence, the results <strong>of</strong> the populationassessment are used to generate second-order response surfaces, one for eachdamage state. Vulnerability curves are generated from response surfacesthrough re-sampling. The derived curves show good correlation withobservational post-earthquake damage statistics.In (Cosenza et al., 2005) a procedure to evaluate the seismic capacity <strong>of</strong> abuil<strong>di</strong>ng class is proposed that enables to reduce <strong>di</strong>spersion <strong>of</strong> results depen<strong>di</strong>ngon the level <strong>of</strong> knowledge. A buil<strong>di</strong>ng class is defined in terms <strong>of</strong> age <strong>of</strong>construction and number <strong>of</strong> storeys. The level <strong>of</strong> knowledge <strong>of</strong> the <strong>buil<strong>di</strong>ngs</strong>tock is accounted for through a “specification” <strong>of</strong> buil<strong>di</strong>ng classes in <strong>di</strong>fferentorders depen<strong>di</strong>ng on the level <strong>of</strong> knowledge <strong>of</strong> the parameters. <strong>RC</strong> rectangularshaped frame <strong>buil<strong>di</strong>ngs</strong> are considered.For each class, a number <strong>of</strong> buil<strong>di</strong>ng models is generated by means <strong>of</strong> a


22 Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>simulated design procedure, based on the probabilistic <strong>di</strong>stribution <strong>of</strong> thestructural (geometrical and mechanical) parameters. <strong>Seismic</strong> capacity isdetermined in terms <strong>of</strong> base shear coefficient and global drift for each <strong>of</strong> thegenerated <strong>buil<strong>di</strong>ngs</strong> <strong>of</strong> the buil<strong>di</strong>ng class, through a mechanics-based approach:3n z predefined mechanisms, where n z is the number <strong>of</strong> storeys, are considered(see Figure 1.3.7) and the correspon<strong>di</strong>ng base shear, V bi , is calculated for eachmechanism assuming a linear <strong>di</strong>stribution <strong>of</strong> horizontal seismic forces.Figure 1.3.7. Predefined collapse mechanisms (Cosenza et al., 2005)The ultimate ro<strong>of</strong> <strong>di</strong>splacement ∆ ui is determined as a function <strong>of</strong> the ultimaterotation θ u <strong>of</strong> the structural elements:( H H )∆ = θ ⋅ − (1.3.1)u,1 u n k∆u,2= θu ⋅ Hk(1.3.2)( H )∆ = θ ⋅ − (1.3.3)u,3 u kHk − 1The collapse mechanism is identified by the lowest value <strong>of</strong> V bi . Then, thecapacity <strong>of</strong> the buil<strong>di</strong>ng is finally evaluated in terms <strong>of</strong> base shear coefficientC b,i (= ratio between the base shear V b,i and the seismic weight W) andcorrespon<strong>di</strong>ng lateral (drift u ) i (= ratio between the ultimate ro<strong>of</strong> <strong>di</strong>splacement∆ u,i and the buil<strong>di</strong>ng height H n ) for the determined collapse mechanism:CVb,ib,i= (1.3.4)W


Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 23( drift )∆u,iu= (1.3.5)iHnStarting from the capacity <strong>of</strong> the analyzed <strong>buil<strong>di</strong>ngs</strong>, the response surfacemethod is adopted and the influence <strong>of</strong> each parameter is investigated. Capacitycurves expressing the probability <strong>of</strong> having a capacity lower than the assignedvalue are obtained through a Monte Carlo simulation technique. The influence<strong>of</strong> the knowledge level on the probability <strong>of</strong> reaching a fixed capacity threshol<strong>di</strong>s shown, too.However, this study only provides cumulative frequency <strong>di</strong>stributions <strong>of</strong>capacity parameters (base shear coefficient and ultimate ro<strong>of</strong> drift) within abuil<strong>di</strong>ng class. No <strong>vulnerability</strong> curve, relating a seismic demand measure to theprobability <strong>of</strong> reaching or excee<strong>di</strong>ng a given damage state, is provided.In (Iervolino et al., 2007) a complete seismic risk assessment framework ispresented, where the mechanisms-based approach is overcome.In order to investigate the buil<strong>di</strong>ng class capacity, n geometrical and mechanicalcharacteristics <strong>of</strong> the <strong>buil<strong>di</strong>ngs</strong> are identified as random variables. Then, apossible range <strong>of</strong> variation and a correspon<strong>di</strong>ng “scanning step” are assumedfor each one <strong>of</strong> this variables. A simulated design procedure, a nonlinear FEmodelling <strong>of</strong> the structure and a Static PushOver (SPO) analysis are carried outfor all <strong>of</strong> the resulting combinations <strong>of</strong> values. Hence, response surfaces areobtained for the capacity parameters T (period), C S (strength) and C d(<strong>di</strong>splacement capacity) <strong>of</strong> the equivalent SDOF system (see Figure 1.3.8),expressed as function <strong>of</strong> the assumed random variables.


24 Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>Figure 1.3.8. Capacity parameters (Iervolino et al., 2007)<strong>Seismic</strong> demand is provided by Probabilistic <strong>Seismic</strong> Hazard Analysis (PSHA).Hence, a calculation <strong>of</strong> seismic risk can be carried out through a Monte Carlosimulation technique, accor<strong>di</strong>ng to the following steps:- sampling <strong>of</strong> N values <strong>of</strong> the n input random variables describing <strong>di</strong>fferentgeometrical and mechanical buil<strong>di</strong>ng characteristics accor<strong>di</strong>ng to theProbability Density Functions (PDFs) respectively assigned;- evaluation <strong>of</strong> N arrays <strong>of</strong> capacity parameters {T, C S , C d } as a function <strong>of</strong>the sampled random variables by linearly interpolating between the pointsobtained from the SPO analyses;- sampling <strong>of</strong> N values <strong>of</strong> elastic spectral <strong>di</strong>splacement demand S d,e accor<strong>di</strong>ngto the probability <strong>di</strong>stribution given by the PSHA;- evaluation <strong>of</strong> the correspon<strong>di</strong>ng N values <strong>of</strong> me<strong>di</strong>an inelastic <strong>di</strong>splacementdemand Sd,i = Sd,e ⋅ CRaccor<strong>di</strong>ng to the Capacity Spectrum Methodassessment procedure (Fajfar, 1999);- sampling <strong>of</strong> N values <strong>of</strong> the random variableεC Rrepresenting thevariability <strong>of</strong> the inelastic <strong>di</strong>splacement demand, accor<strong>di</strong>ng to the assignedPDF, thus giving the N final values <strong>of</strong> the <strong>di</strong>splacement demandD = S d,i⋅ε CR;- comparison between the N values <strong>of</strong> <strong>di</strong>splacement capacity C d and thecorrespon<strong>di</strong>ng N values <strong>of</strong> <strong>di</strong>splacement demand D, thus lea<strong>di</strong>ng to thenumber N f <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong> for which the capacity is exceeded by the demand;


Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 25Nf- estimation <strong>of</strong> the failure probability as Pf= .NHAZUS (HAZard in United States) is an earthquake loss estimationmethodology inclu<strong>di</strong>ng many components. It was developed by the FederalEmergency Management Agency (FEMA) under agreements with the NationalInstitute <strong>of</strong> Buil<strong>di</strong>ng Sciences (NIBS) (FEMA, 2001; Kircher et al., 1997a;Kircher et al., 1997b; Whitman et al., 1997).Estimates <strong>of</strong> buil<strong>di</strong>ng damage are used as inputs to other damage modules.Most importantly, buil<strong>di</strong>ng damage is used as an input to a number <strong>of</strong> lossmodules (see Figure 1.3.9).Figure 1.3.9. Buil<strong>di</strong>ng-related modules <strong>of</strong> HAZUS methodology (FEMA, 2001)HAZUS damage functions for ground shaking have two basic components:capacity curves and fragility curves.Capacity curves are defined by two control points: the yield capacity and theultimate capacity. The yield capacity accounts for design strength, redundanciesin design, conservatism in code requirements and expected (rather thannominal) strength <strong>of</strong> materials. Design strengths <strong>of</strong> model buil<strong>di</strong>ng types arebased on the requirements <strong>of</strong> US seismic code provisions or on an estimate <strong>of</strong>lateral strength for <strong>buil<strong>di</strong>ngs</strong> not designed for earthquake loads. The ultimate


26 Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>capacity represents the maximum strength <strong>of</strong> the buil<strong>di</strong>ng when the globalstructural system has reached a full mechanism. Up to yield, the buil<strong>di</strong>ngcapacity curve is assumed to be linear with stiffness based on an estimate <strong>of</strong> theexpected “elastic” period <strong>of</strong> the buil<strong>di</strong>ng. From yield to the ultimate point, thecapacity curve transitions in slope from an essentially elastic state to a fullyplastic state. The capacity curve is assumed to remain plastic past the ultimatepoint (see Figure 1.3.10).Figure 1.3.10. Example buil<strong>di</strong>ng capacity curve and control points (FEMA, 2001)36 <strong>di</strong>fferent buil<strong>di</strong>ng structural typologies are considered. For each typology,values <strong>of</strong> the parameters defining the capacity curves are provided. As anexample, see Figure 1.3.11 and Figure 1.3.12 for C1M buil<strong>di</strong>ng class (Mid-RiseConcrete Moment Frame).


Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 27Figure 1.3.11. “Elastic” period values and average inter-story drift ratios <strong>of</strong> capacity curvecontrol points and structural damage state thresholds (fragility me<strong>di</strong>ans) for C1M 1 buil<strong>di</strong>ngclass (FEMA, 2001)Figure 1.3.12. Capacity curves and structural damage-state thresholds (fragility me<strong>di</strong>ans) forfive seismic design levels (Special High, High, Moderate, Low and Pre-Code) for C1M buil<strong>di</strong>ngclass (FEMA, 2001)Capacity Spectrum Method is adopted in HAZUS to evaluate the demandcorrespon<strong>di</strong>ng to a given seismic intensity. To this end, the inelastic demand


28 Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>spectrum is obtained reducing the 5%-damped elastic response spectrum bymeans <strong>of</strong> an effective damping value which is defined as the total energy<strong>di</strong>ssipated by the buil<strong>di</strong>ng during peak earthquake response and is the sum <strong>of</strong> anelastic damping term, β E , and a hysteretic damping term, β H , associated withpost-yield, inelastic response and influenced by ground motion duration. Then,peak response <strong>di</strong>splacement and acceleration are determined from theintersection between the demand spectrum and the buil<strong>di</strong>ng’s capacity curve(see Figure 1.3.13).Figure 1.3.13. Example demand spectrum construction and calculation <strong>of</strong> peak response<strong>di</strong>splacement (D) and acceleration (A) (FEMA, 2001)HAZUS provides fragility curves for damage to structural system, nonstructuralcomponents sensitive to drift and non-structural components (andcontents) sensitive to acceleration. Fragility curves are lognormal functionsdefined by a me<strong>di</strong>an value <strong>of</strong> the demand parameter, which corresponds to thethreshold <strong>of</strong> that damage state, and by the variability associated with thatdamage state. For example, the spectral <strong>di</strong>splacement S d that defines thethreshold <strong>of</strong> a particular damage state ds is given by


Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 29Sd= Sd,ds⋅εds(1.3.6)where S d,ds is the me<strong>di</strong>an value <strong>of</strong> spectral <strong>di</strong>splacement <strong>of</strong> damage state ds andε ds is a lognormal random variable with a unit me<strong>di</strong>an value and a logarithmicstandard deviation β ds , which controls the slope <strong>of</strong> the fragility curve andaccounts for the variability and uncertainty associated with capacity curveproperties, damage states and ground shaking.Four damage states are defined: Slight, Moderate, Extensive and Complete (seeFigure 1.3.14). Me<strong>di</strong>an values <strong>of</strong> spectral <strong>di</strong>splacement associated with eachdamage state are evaluated calculating the average interstorey drift ratio (i.e.,ro<strong>of</strong> <strong>di</strong>splacement <strong>di</strong>vided by buil<strong>di</strong>ng height) correspon<strong>di</strong>ng to the step <strong>of</strong>pushover analysis at which a certain fraction <strong>of</strong> structural elements reaches acertain deformation limit. The value <strong>of</strong> this fraction is defined as the repair orreplacement cost <strong>of</strong> components at limit <strong>di</strong>vided by the total replacement value<strong>of</strong> the structural system.Figure 1.3.14. Example fragility curves for Slight, Moderate, Extensive and Complete damage(FEMA, 2001)The lognormal standard deviation β ds , which describes the total variability <strong>of</strong>fragility-curve damage state ds, is given by three contributions:


30 Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>( CONV [ , ]) 2( ) 2β = β β + β (1.3.7)ds C D T,dswhere β C is the lognormal standard deviation parameter that describes thevariability <strong>of</strong> the capacity curve, β D is the lognormal standard deviationparameter that describes the variability <strong>of</strong> the demand spectrum and β T,ds is thelognormal standard deviation parameter that describes the variability <strong>of</strong> thethreshold <strong>of</strong> damage state ds. Since the demand spectrum is dependent onbuil<strong>di</strong>ng capacity, a convolution process is required to combine their respectivecontributions to total variability, while the third contribution to total variability,β T,ds , is assumed mutually independent <strong>of</strong> the first two and is combined with theresults <strong>of</strong> the convolution process using the square-root-sum-<strong>of</strong>-the squares(SRSS) method. The convolution process involves a complex numericalcalculation that would be very <strong>di</strong>fficult for most users to perform. To avoid this<strong>di</strong>fficulty, sets <strong>of</strong> pre-calculated values <strong>of</strong> damage state Beta’s are proposed.These Beta values are given as a function <strong>of</strong> buil<strong>di</strong>ng height group, post-yielddegradation <strong>of</strong> the structural system, damage state threshold variability andcapacity curve variability.Estimation <strong>of</strong> β C and β T,ds must be made by users on a judgmental basis, basedon the consideration that these variability values are influenced by uncertaintyin capacity curve properties and thresholds <strong>of</strong> damage states and by buil<strong>di</strong>ngpopulation (i.e., in<strong>di</strong>vidual buil<strong>di</strong>ng or group <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong>): relatively lowvariability <strong>of</strong> damage states would be expected for an in<strong>di</strong>vidual buil<strong>di</strong>ng withwell known properties (e.g., complete set <strong>of</strong> as-built drawings, material testdata, etc.) and whose performance and failure modes are known withconfidence. Relatively high variability <strong>of</strong> damage states would be expected fora group <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong> whose properties are not well known and for which theuser has low confidence in the results (<strong>of</strong> pushover analysis) that representperformance and failure modes <strong>of</strong> all <strong>buil<strong>di</strong>ngs</strong> <strong>of</strong> the group.Giovinazzi (2005) proposes a method for seismic risk assessment based onthe assumption that, dealing with a territorial <strong>vulnerability</strong> assessment, buil<strong>di</strong>ng


Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 31seismic response can be represented by simplified bilinear capacity curvesdefined by three parameters: the yield acceleration, the yield period <strong>of</strong> vibrationand the structural ductility capacity.The yield acceleration can be derived as a function <strong>of</strong> the seismic code designlateral force, multiplied by another factor in order to consider me<strong>di</strong>an values <strong>of</strong>material strength instead <strong>of</strong> nominal ones. The period can be evaluated throughsimplified expressions proposed by code. The ductility capacity can be derivedfrom the behaviour factor adopted in design, if any; otherwise, for <strong>buil<strong>di</strong>ngs</strong>non-specifically designed to have <strong>di</strong>ssipation capacity, a value <strong>of</strong> 2.5 is arbitraryassumed.For non designed structures, the author states that bilinear capacity curve can bederived taking into account the geometrical and the technological featurescharacterizing on the average the typology (number <strong>of</strong> floors, code level,material strength, drift capacity, age, etc.) and hypothesizing a certain collapsemode.Displacement demand assessment for a given seismic intensity is carried outaccor<strong>di</strong>ng to the Capacity Spectrum Method.Four damage states are considered. Mean values <strong>of</strong> the correspon<strong>di</strong>ng<strong>di</strong>splacement threshold are proposed as a function <strong>of</strong> the yiel<strong>di</strong>ng and ultimate<strong>di</strong>splacements, based on expert judgement, and are verified on the basis <strong>of</strong> theresults <strong>of</strong> pushover analyses performed on prototype <strong>buil<strong>di</strong>ngs</strong>.In order to define fragility curves for the considered damage states, uncertaintyin the estimate has to be evaluated. To this end, a <strong>di</strong>fferent approach fromHAZUS is proposed: the overall uncertainty in the damage estimation isevaluated in order to represent the same <strong>di</strong>spersion <strong>of</strong> observed damage datathat are well fitted by binomial <strong>di</strong>stributions. Repeating this procedure for<strong>di</strong>fferent <strong>buil<strong>di</strong>ngs</strong> typologies a lognormal standard deviation is found,depen<strong>di</strong>ng on the ductility correspon<strong>di</strong>ng the mean damage values.Grant et al. (2006) also adopt a code-based approach to the evaluation <strong>of</strong>buil<strong>di</strong>ng seismic <strong>vulnerability</strong>. In order to carry out a first, rapid and very


32 Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>simplified step <strong>of</strong> a multi-level screening procedure aimed at defining prioritiesand timescales for seismic intervention in school <strong>buil<strong>di</strong>ngs</strong>, authors evaluate thePGA capacity from the code-prescribed seismic input at the age <strong>of</strong> construction,based on the assumption <strong>of</strong> a “perfect” code compliance. To this aim, startingfrom the design inelastic acceleration capacity prescribed by the seismic code inforce at the age <strong>of</strong> construction, a sort <strong>of</strong> “back-analysis” is applied, thuscalculating the correspon<strong>di</strong>ng PGA, also accounting for modern seismic coderequirements inclu<strong>di</strong>ng adjustments for ductility capacity (i.e., the behaviourfactor) and buil<strong>di</strong>ng importance. In a very conservative (but unrealistic) way theauthors also assume that <strong>buil<strong>di</strong>ngs</strong> designed for Gravity Loads only have a nullseismic capacity. Following this procedure, the seismic <strong>vulnerability</strong> can beevaluated in terms <strong>of</strong> a “PGA deficit” obtained as the <strong>di</strong>fference between theevaluated PGA capacity and the PGA demand, which is derived from modernseismic hazard stu<strong>di</strong>es.However, a quite critical shortcoming can affect a procedure that evaluateseismic capacity based on the assumption <strong>of</strong> a perfect code compliance withseismic codes in force at the age <strong>of</strong> construction, since the actual seismiccapacity <strong>of</strong> a buil<strong>di</strong>ng stock can <strong>di</strong>ffer greatly from the pre<strong>di</strong>ction <strong>of</strong> such a codeprescription-based model. At least, factors accounting for material overstrengthshould be accounted for (e.g., Giovinazzi, 2005). Moreover, designconservatism approximations usually should lead to a higher capacity,compared with code prescriptions. Hence, a code-based procedure maysystematically underestimate seismic capacity. This approach may be justifiedas conservative, but actually a seismic <strong>vulnerability</strong> assessment for a large scaleearthquake loss model should not be conservative; it should rather provide aseismic capacity estimation as reliable as possible.Ordaz et al. (2000) adopt a <strong>vulnerability</strong> analysis procedure where thedamage level is expressed as a function <strong>of</strong> the maximum interstorey drift, whichis evaluated as a function <strong>of</strong> the spectral acceleration. The relationship between


Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 33the maximum expected interstorey drift and the spectral acceleration demand isevaluated through a simplified model based on the analogy with equivalentcantilever beams subjected to shear and flexural deformations. In this model,coefficients are used to account, among others, for the structural type, for theheight <strong>of</strong> the structure and for the ratio between inelastic and elastic demand.Moreover, further coefficients are used to account for the increase in seismic<strong>vulnerability</strong> due to some factors inclu<strong>di</strong>ng, for instance, irregularities inelevation and/or in plan or the presence <strong>of</strong> short columns.Calvi (1999) first proposes an approach for the evaluation <strong>of</strong> the<strong>vulnerability</strong> <strong>of</strong> buil<strong>di</strong>ng classes based on the Displacement-Based method (e.g.,Priestley, 1997).For each limit state, a <strong>di</strong>splacement shape is assumed and a correspon<strong>di</strong>ng<strong>di</strong>splacement capacity is evaluated, depen<strong>di</strong>ng on the attainment <strong>of</strong> a localdeformation limit [material strain capacity -> section curvature capacity ->element drift capacity -> buil<strong>di</strong>ng <strong>di</strong>splacement capacity (on the equivalentSDOF model)]. A possible range <strong>of</strong> variation for the evaluated capacity isdefined. At the same time, a possible range <strong>of</strong> variation for the period <strong>of</strong>vibration (secant to the <strong>di</strong>splacement capacity) is defined, too. Hence, for eachlimit state, rectangles representing the possible “positions” <strong>of</strong> the pointsrepresenting the buil<strong>di</strong>ng capacity in a period-<strong>di</strong>splacement plane are obtained.A uniform probability density function over the rectangles is assumed,describing the variability <strong>of</strong> the capacity.<strong>Seismic</strong> demand is represented by <strong>di</strong>splacement response spectra adjusted toinclude the nonlinear response, wherein a reduction <strong>of</strong> the spectral or<strong>di</strong>nates isapplied to account for the energy <strong>di</strong>ssipation capacity <strong>of</strong> the structure as afunction <strong>of</strong> the target <strong>di</strong>splacement and the structural response.Capacity and demand can be <strong>di</strong>rectly compared to each other as a function <strong>of</strong>the period: the rectangle area below the demand spectrum represents theexpected proportion <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong> reaching (or excee<strong>di</strong>ng) the limit statecapacity (see Figure 1.3.15).


34 Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>Figure 1.3.15. An example <strong>of</strong> the intersection <strong>of</strong> capacity areas and demand spectrum (Calvi,1999)The methodology proposed by Calvi (1999) is subsequently developed(Pinho et al., 2002; Glaister and Pinho, 2003; Crowley et al., 2004; Crowley etal., 2006) lea<strong>di</strong>ng to the Displacement-Based Earthquake Loss Assessment(DBELA) procedure.The main improvements to the original procedure by Calvi (1999) may besummarized in (i) the theoretical improvement <strong>of</strong> structural and non-structural<strong>di</strong>splacement capacity equations, (ii) the derivation <strong>of</strong> an equation betweenyield period and height for European <strong>buil<strong>di</strong>ngs</strong> both with and without infillpanels (Crowley and Pinho, 2004, 2006) and (iii) the development <strong>of</strong> a fullyprobabilistic framework accounting for uncertainties in geometrical andmechanical properties, in capacity models and in demand spectrum.In DBELA the <strong>di</strong>splacement capacity can be expressed as a function <strong>of</strong> thebuil<strong>di</strong>ng height; this relationship can be transformed into a <strong>di</strong>rect relationshipbetween <strong>di</strong>splacement capacity and period, through the substitution <strong>of</strong> anequation relating the height <strong>of</strong> a buil<strong>di</strong>ng to its limit state period. Hence, a


Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 35<strong>di</strong>rect comparison is possible at any period between the <strong>di</strong>splacement capacity<strong>of</strong> a buil<strong>di</strong>ng class and the <strong>di</strong>splacement demand pre<strong>di</strong>cted from a responsespectrum (see Figure 1.3.16).Figure 1.3.16. Deformation based seismic <strong>vulnerability</strong> assessment procedure (Glaister andPinho, 2003)The probabilistic treatment <strong>of</strong> the uncertainties involved in the assessmentprocedure leads to the definition <strong>of</strong> a Joint Probability Density Function (JPDF)<strong>of</strong> <strong>di</strong>splacement capacity and period (see Figure 1.3.17), which was originallyassumed to be uniform (Calvi, 1999).Figure 1.3.17. Joint Probability Density Function (JPDF) <strong>of</strong> <strong>di</strong>splacement capacity andperiod (Crowley et al., 2004)


36 Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>The Simplified Pushover-Based Earthquake Loss Assessment (SP-BELA)by Borzi et al. (2008a) combines the definition <strong>of</strong> a pushover curve using asimplified mechanics-based procedure – similar to (Cosenza et al., 2005) – todefine the base shear capacity <strong>of</strong> the buil<strong>di</strong>ng stock with a <strong>di</strong>splacement-basedframework similar to that in DBELA, such that the <strong>vulnerability</strong> <strong>of</strong> buil<strong>di</strong>ngclasses at <strong>di</strong>fferent limit states can be obtained.Simplified pushover curves are derived accor<strong>di</strong>ng to the following procedure: aprototype structure representing the buil<strong>di</strong>ng class is defined first, for which thecollapse mechanism and, therefore, the collapse multiplier under a linear<strong>di</strong>stribution <strong>of</strong> lateral forces is determined. Based on limit con<strong>di</strong>tions given interms <strong>of</strong> element chord rotations, the buil<strong>di</strong>ng <strong>di</strong>splacement capacity (in terms<strong>of</strong> the equivalent SDOF) is evaluated for <strong>di</strong>fferent Limit States. Then, theperiod <strong>of</strong> vibration for each Limit State is calculated, correspon<strong>di</strong>ng to thesecant stiffness to the <strong>di</strong>splacement capacity.In order to derive <strong>vulnerability</strong> curves using this type <strong>of</strong> analytical procedure, aset <strong>of</strong> random variables is defined – together with the correspon<strong>di</strong>ng probability<strong>di</strong>stributions – inclu<strong>di</strong>ng geometrical <strong>di</strong>mensions, material properties anddesign loads.<strong>Seismic</strong> demand is defined in terms <strong>of</strong> inelastic <strong>di</strong>splacement demand spectra,and the uncertainty in this demand is taken into account assuming the cornerperiods <strong>of</strong> the spectrum and the spectral amplification coefficient as randomvariables.A Monte Carlo simulation approach is adopted, and random variables aregenerated through a Latin Hypercube Sampling procedure. Hence, <strong>vulnerability</strong>curves can be derived for a class <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong> and for <strong>di</strong>fferent Limit States,carrying out the following steps:- definition <strong>of</strong> a number <strong>of</strong> buil<strong>di</strong>ng samples through the generation <strong>of</strong>assumed random variables;- definition <strong>of</strong> buil<strong>di</strong>ng capacity through a pushover curve for each generatedbuil<strong>di</strong>ng;- definition <strong>of</strong> the <strong>di</strong>splacement demand;


Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 37- comparison between demand and capacity to define the number <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong>– out <strong>of</strong> the generated population – excee<strong>di</strong>ng the given Limit Statecon<strong>di</strong>tions.SP-BELA has been further developed in order to approximately account for thepresence <strong>of</strong> infill panels in (Borzi et al., 2008b). Two possible <strong>di</strong>stributions <strong>of</strong>the infill panels are considered: a uniform <strong>di</strong>stribution along the height <strong>of</strong> thebuil<strong>di</strong>ng or a “pilotis” <strong>di</strong>stribution. It is assumed that the panels have aninfluence on the lateral resistance <strong>of</strong> the buil<strong>di</strong>ng up to the yield limit state.When the frames evolve into the nonlinear range, the panels are considered tocollapse and, therefore, they no longer contribute to the base shear resistance.The behaviour <strong>of</strong> the single strut representing the infill panel is assumed to belinear up to failure. The influence <strong>of</strong> the panels is not considered in defining the<strong>di</strong>splacement capacity on the pushover curve as the panels are <strong>of</strong>ten notperfectly in contact with the frames and they are assumed to play a role on theoverall buil<strong>di</strong>ng performance only after the frames have already been deformedbeyond their elastic limit. On the other hand, the panels are assumed to collapsebefore the frames reach the significant damage limit con<strong>di</strong>tion.Hence, the only way the influence <strong>of</strong> infill panels is accounted for is that theyare assumed to increase the lateral strength <strong>of</strong> the buil<strong>di</strong>ng up to the yiel<strong>di</strong>ng <strong>of</strong>the <strong>RC</strong> structure. In other terms, the presence <strong>of</strong> infill panels leads to a lowervalue <strong>of</strong> the secant period to the yiel<strong>di</strong>ng Limit State by increasing the yieldstrength, thus decreasing the correspon<strong>di</strong>ng failure probability within theadopted Displacement-Based assessment framework. No influence at all isconsidered on other Limit States.However, authors do not clarify how the presence <strong>of</strong> elements characterized bya brittle behaviour (such as infill trusses) can be accounted for in amechanisms-based approach, where all the structural elements should have anelastic-perfectly plastic behaviour.


38 Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>VC (Vulnerabilità Calcestruzzo armato, reinforced concrete <strong>vulnerability</strong>),by Dolce and Moroni (2005), is a simplified procedure – implemented in aspreadsheet s<strong>of</strong>tware – for the <strong>vulnerability</strong> assessment <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>. TwoLimit States are considered: Slight Damage and Collapse. The <strong>vulnerability</strong> isexpressed as the PGA values lea<strong>di</strong>ng the attainment <strong>of</strong> these Limit States. Theprocedure is based on the evaluation <strong>of</strong> the storey strength at each storey and onthe application <strong>of</strong> a ductility coefficient accounting for the inelastic<strong>di</strong>splacement capacity.S<strong>of</strong>t-storey (concentration <strong>of</strong> the inelastic demand only in columns in onestorey) is the only collapse mechanism considered. In authors’ opinion, this isthe most probable collapse mechanism for <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>, due t<strong>of</strong>requent weak column/strong beam con<strong>di</strong>tions.Infill elements can be taken into account, both in terms <strong>of</strong> stiffness andstrength.For the definition <strong>of</strong> Slight Damage Limit State an interstorey drift limit, basedon Italian code prescriptions, is assumed. An elastic behaviour is assumed up tothis limit. Hence, interstorey shear stiffness has to be evaluated. To this end, thesum <strong>of</strong> column stiffness values is calculated, also considering the influence <strong>of</strong>the restrain con<strong>di</strong>tion given by the beams; a cracked stiffness is considered, too.If infill panels are present, their contribution is taken into account assuming thestiffness model provided by Italian code. Hence, a value <strong>of</strong> interstorey shearlea<strong>di</strong>ng to the attainment <strong>of</strong> Slight Damage Limit State (V OPER ) is evaluated ateach storey, correspon<strong>di</strong>ng to the prescribed interstorey drift limit.For Collapse Limit State the ultimate value <strong>of</strong> interstorey shear strength (V COLL )at each storey is evaluated. The ultimate interstorey shear strength is calculatedas the sum <strong>of</strong> the ultimate shear strength <strong>of</strong> each column, given by the flexuralcapacity <strong>of</strong> the column section, also considering the influence <strong>of</strong> the restraincon<strong>di</strong>tion given by the beams on the moment <strong>di</strong>stribution along the elementand, therefore, on the correspon<strong>di</strong>ng shear value. Possible shear failures areconsidered, too. If infill panels are present, their contribution to the ultimateshear strength is taken into account considering <strong>di</strong>fferent possible collapse


Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 39mechanisms <strong>of</strong> the panels. Subsequently, this value is multiplied by acoefficient accounting for the inelastic <strong>di</strong>splacement capacity in order toevaluate the interstorey shear value lea<strong>di</strong>ng to Collapse in a spectral elasticapproach, thus implicitly applying the equal rule between overstrength andductility (R=µ).The procedure can be summarized in the following steps (each step is carriedout in both buil<strong>di</strong>ng <strong>di</strong>rections):- at each storey, interstorey shear lea<strong>di</strong>ng to Slight Damage drift limit (V OPER )and ultimate interstorey shear strength (V COLL ) are evaluated, as abovedescribed;- the interstorey shear demand <strong>di</strong>stribution is evaluated, assuming a baseshear demand equal to the weight <strong>of</strong> the structure (that is, a pseudoaccelerationequal to 1g) and a linear <strong>di</strong>stribution <strong>of</strong> lateral <strong>di</strong>splacements;- at each storey, the ratios between V OPER and V COLL and the interstorey sheardemand are evaluated, representing the pseudo-acceleration values S D(OP)and S D(COLL) (expressed in g) lea<strong>di</strong>ng to the attainment <strong>of</strong> a shear demandequal to V OPER and V COLL , respectively;- at each storey, the PGA values correspon<strong>di</strong>ng to S D(OP) and S D(COLL) areevaluated by means <strong>of</strong> <strong>di</strong>fferent coefficients: α PM (accounting for theparticipating mass ratio <strong>of</strong> the first mode), α AD (aimed at evaluating thePGA from the spectral pseudo-acceleration depen<strong>di</strong>ng on the period <strong>of</strong>vibration and the shape <strong>of</strong> the demand spectrum), α DS (accounting for thestructural <strong>di</strong>ssipation capacity) and α DUT (accounting for the inelastic<strong>di</strong>splacement capacity). Obviously, α DUT is equal to 1 for Slight DamageLimit State. For Collapse Limit State, a coefficient α DUT,pil is evaluated foreach column as a function <strong>of</strong> the axial load ratio; it is assumed equal to 1 ifthe column behaviour is controlled by shear. Then, α DUT is given by aweighted average <strong>of</strong> α DUT,pil extended to all the columns in the storey. α DUTcan be reduced by means <strong>of</strong> coefficients accounting for the presence <strong>of</strong> as<strong>of</strong>t storey or for irregularities in strength/stiffness/mass <strong>di</strong>stribution. If thepresence <strong>of</strong> infill panels is taken into account α DUT is assumed equal to 1.5


40 Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>since in this case in authors’ opinion the failure mechanism is controlled bybrittle interaction mechanisms between structural and non-structuralelements;- for both Limit States, the minimum PGA value between all the valuescalculated at each storey and in each <strong>di</strong>rection is evaluated, representing thePGA capacity <strong>of</strong> the buil<strong>di</strong>ng.1.4 HYBRID METHODSHybrid methods allow to produce DPMs and <strong>vulnerability</strong> curves as acombination <strong>of</strong> analytical data from mechanical models and empirical datafrom observed damage, thus allowing, for example, to calibrate analyticalmodels or to provide for the lack <strong>of</strong> empirical damage data at certain intensitylevels for the geographical area under consideration.In (Kappos et al., 1995; Kappos et al., 1998) DPMs are provided which arepartially derived from observed damage data from past earthquakes, through the<strong>vulnerability</strong> index procedure, and partially obtained from nonlinear dynamicanalyses carried out on buil<strong>di</strong>ng models representing <strong>di</strong>fferent buil<strong>di</strong>ng classes.In order to include such analytical results into the DPMs, an empiricalcorrelation between intensity and PGA values at which the accelerograms werescaled is used, and a correlation is also established between an analytical globaldamage index obtained from the analyses and the damage expressed as the cost<strong>of</strong> repair. 6 structural models representing <strong>existing</strong> Greek <strong>buil<strong>di</strong>ngs</strong>, 10accelerograms and 2 intensities are considered, thus lea<strong>di</strong>ng to a total number <strong>of</strong>120 nonlinear dynamic analyses. The damage results are then combined withthe observed damage from the 1978 earthquake in Thessaloniki.In (Singhal and Kiremidjian, 1998) the analytical <strong>vulnerability</strong> curvesproposed in (Singhal and Kiremidjian, 1996) for Low-Rise <strong>RC</strong> frames areupdated based on the observational data obtained on 84 <strong>buil<strong>di</strong>ngs</strong> damagedduring the 1994 Northridge earthquake, by means <strong>of</strong> a Bayesian updatingtechnique accounting for the reliability <strong>of</strong> <strong>di</strong>fferent data sources.Nevertheless, special attention should be addressed to the treatment <strong>of</strong>


Chapter I – Assessing seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 41uncertainties when using hybrid methods since analytical and empirical<strong>vulnerability</strong> data include <strong>di</strong>fferent sources <strong>of</strong> uncertainty and are thus not<strong>di</strong>rectly comparable. Hence, in order to improve an analytical model through acomparison with an empirical model, it probably would be better to calibratethe former in order to obtain only me<strong>di</strong>an values equal to the ones provided bythe latter. In this way, each source <strong>of</strong> uncertainty can be properly taken intoaccount through a specific and explicit modelling (Calvi et al., 2006).1.5 EXPERT JUDGEMENT-BASED METHODSAn example <strong>of</strong> Damage Probability Matrices derived from expert judgementcan be found in ATC-13 (ATC, 1985), where DPMs are provided which werederived from the judgement <strong>of</strong> more than 50 senior earthquake engineeringexperts. Each expert provided, accor<strong>di</strong>ng to his engineering judgement andexperience, an estimate <strong>of</strong> low, best and high values <strong>of</strong> the damage ratio foreach <strong>of</strong> 36 <strong>di</strong>fferent buil<strong>di</strong>ng classes, as a function <strong>of</strong> the seismic intensityexpressed accor<strong>di</strong>ng to the MMI scale. These values were assumed ascorrespon<strong>di</strong>ng to 5 th , 50 th and 95 th percentiles, respectively, <strong>of</strong> a lognormal<strong>di</strong>stribution representing the estimated damage factor for a given seismicintensity. The estimates provided by the experts were also weighted accor<strong>di</strong>ngto the experience and confidence level <strong>of</strong> each expert for the consideredbuil<strong>di</strong>ng class.


42 Chapter I - Assessing the seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>REFERENCES− ATC, 1985. Earthquake damage evaluation data for California. ReportATC-13, Applied Technology Council, Redwood City, California,USA.− Benedetti D., Petrini V., 1984. Sulla vulnerabilità <strong>di</strong> e<strong>di</strong>fici in muratura:proposta <strong>di</strong> un metodo <strong>di</strong> valutazione. L’industria delle Costruzioni,149(1), 66-74. (in Italian)− Borzi B., Pinho R., Crowley H., 2008a. Simplified pushover-based<strong>vulnerability</strong> analysis for large scale assessment <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>.Engineering Structures, 30(3), 804-820.− Borzi B., Crowley H., Pinho R., 2008b, The influence <strong>of</strong> infill panels on<strong>vulnerability</strong> curves for <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>. Procee<strong>di</strong>ngs <strong>of</strong> the 14 th WorldConference on Earthquake Engineering, Beijing, China, October 12-17.Paper 09-01-0111.− Braga F., Dolce M., Liberatore D., 1982. A statistical study on damaged<strong>buil<strong>di</strong>ngs</strong> and an ensuing review <strong>of</strong> the MSK-76 scale. Procee<strong>di</strong>ngs <strong>of</strong>the 7 th European Conference on Earthquake Engineering, Athens,Greece. Pp. 431-450.− Calvi G.M., 1999. A <strong>di</strong>splacement-based approach for <strong>vulnerability</strong>evaluation <strong>of</strong> classes <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong>. Journal <strong>of</strong> Earthquake Engineering,3(3), 411-438.− Calvi G.M., Pinho R., Magenes G., Bommer J.J., Restrepo-Veléz L.F.,Crowley H., 2006. The development <strong>of</strong> seismic <strong>vulnerability</strong> assessmentmethodologies for variable geographical scales over the past 30 years.ISET Journal <strong>of</strong> Earthquake Technology, 43(3), 75-104.− Colombi M., Borzi B., Crowley H., Onida M., Meroni F., Pinho R., 2008.Deriving <strong>vulnerability</strong> curves using Italian earthquake damage data.Bulletin <strong>of</strong> Earthquake Engineering, 6(3), 485-504.


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44 Chapter I - Assessing the seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>(vulnerabilità c.a.) e VM (vulnerabilità muratura), Atti del <strong>Dipartimento</strong><strong>di</strong> Strutture, Geotecnica, Geologia applicata all’ingegneria, N. 4/2005.(in Italian)− Faccioli E., Pessina V. (e<strong>di</strong>tors), 2000. The Catania project: earthquakedamage scenarios for a high risk area in the Me<strong>di</strong>terranean. CNR-Gruppo Nazionale per la Difesa dai Terremoti, Rome, Italy.− Faccioli E., Pessina V., Calvi G.M., Borzi B., 1999.A study on damagescenarios for residential <strong>buil<strong>di</strong>ngs</strong> in Catania city. Journal <strong>of</strong>Seismology, 3(3), 327-343.− Fajfar P., 1999. Capacity spectrum method based on inelastic demandspectra. Earthquake Engineering and Structural Dynamics, 28(9), 979-993.− FEMA, 2001. HAZUS99 Technical Manual. Service Release 2. FederalEmergency Management Agency, Washington, D.C., USA.− Giovinazzi S., 2005. The <strong>vulnerability</strong> assessment and the damagescenario in seismic risk analysis. PhD Thesis, Technical UniversityCarolo-Wilhelmina at Braunschweig, Braunschweig, Germany andUniversity <strong>of</strong> Florence, Florence, Italy.− Giovinazzi S., Lagomarsino S., 2004. A macroseismic method for the<strong>vulnerability</strong> assessment <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong>. Procee<strong>di</strong>ngs <strong>of</strong> the 13 th WorldConference on Earthquake Engineering, Vancouver, Canada, August 1-6. Paper No. 896.− Glaister S., Pinho R., 2003. Development <strong>of</strong> a simplified deformationbasedmethod for seismic <strong>vulnerability</strong> assessment. Journal <strong>of</strong>Earthquake Engineering, 7(SI1), 107-140.− GNDT, 1993. Rischio sismico <strong>di</strong> e<strong>di</strong>fici pubblici. Parte I: aspettimetodologici. CNR-Gruppo Nazionale per la Difesa dai Terremoti,Rome, Italy.− Grant D., Bommer J.J., Pinho R., Calvi G.M., 2006. Defining prioritiesand timescales for seismic intervention in school <strong>buil<strong>di</strong>ngs</strong> in Italy.ROSE Research Report No. 2006/03, IUSS Press, Pavia, Italy.


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46 Chapter I - Assessing the seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>− Masi A., 2003. <strong>Seismic</strong> <strong>vulnerability</strong> assessment <strong>of</strong> Gravity LoadDesigned R/C frames. Bulletin <strong>of</strong> Earthquake Engineering, 1(3), 371-395.− Mouroux P., Le Brun B., 2006. Presentation <strong>of</strong> RISK-UE project. Bulletin<strong>of</strong> Earthquake Engineering, 4(4), 323-339.− Ordaz M., Miranda E., Reinoso E., Pérez-Rocha L.E., 2000. <strong>Seismic</strong> Lossestimation model for Mexico City. Procee<strong>di</strong>ngs <strong>of</strong> the 12 th WorldConference on Earthquake Engineering, Auckland, New Zealand,January 30-February 4. Paper No. 1902.− Orsini G., 1999. A model for <strong>buil<strong>di</strong>ngs</strong>’ <strong>vulnerability</strong> assessment usingthe Parameterless Scale <strong>of</strong> <strong>Seismic</strong> Intensity (PSI). Earthquake Spectra,15(3), 463-483.− Ozdemir P., Boduroglu M.H., Ilki A., 2005. <strong>Seismic</strong> safety screeningmethod. Procee<strong>di</strong>ngs <strong>of</strong> the International Workshop on <strong>Seismic</strong>Performance Assessment and Rehabilitation <strong>of</strong> Existing Buil<strong>di</strong>ngs(SPEAR), Ispra, Italy, April 4-5. Paper No. 23.− Park Y.J., Ang A.H.S., 1985. Mechanistic seismic damage model forreinforced concrete. ASCE Journal <strong>of</strong> Structural Engineering, 111(4),722-739.− Pinho R., Bomber J.J., Glaister S., 2002. A simplified approach to<strong>di</strong>splacement-based earthquake loss estimation analysis. Procee<strong>di</strong>ngs <strong>of</strong>the 12 th European Conference on Earthquake Engineering, London, UK,September 9-13. Paper No. 738.− Priestley M.J.N., 1997. Displacement-based seismic assessment <strong>of</strong>reinforced concrete <strong>buil<strong>di</strong>ngs</strong>. Journal <strong>of</strong> Earthquake Engineering, 1(1),157-192.− Rossetto T., Elnashai A., 2003. Derivation <strong>of</strong> <strong>vulnerability</strong> functions forEuropean-type <strong>RC</strong> structures based on observational data. EngineeringStructures, 25(10), 1241-1263.


Chapter I – Assessing the seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 47− Rossetto T., Elnashai A., 2005. A new analytical procedure for thederivation <strong>of</strong> <strong>di</strong>splacement-based <strong>vulnerability</strong> curves for populations <strong>of</strong><strong>RC</strong> structures. Engineering Structures, 7(3), 397-409.− Rota M., Penna A., Strobbia C., Magenes G., 2008. Direct derivation <strong>of</strong>fragility curves from Italian post-earthquake survey data. Procee<strong>di</strong>ngs <strong>of</strong>the 14 th World Conference on Earthquake Engineering, Beijing, China,October 12-17. Paper 09-01-0148.− Sabetta F., Goretti A., Lucantoni A., 1998. Empirical fragility curvesfrom damage surveys and estimated strong ground motion. Procee<strong>di</strong>ngs<strong>of</strong> the 11 th European Conference on Earthquake Engineering, Paris,France, September 6-11.− Sabetta F., Pugliese A., 1987. Attenuation <strong>of</strong> peak horizontal accelerationand velocity from Italian strong-motion records. Bulletin <strong>of</strong> theSeismological Society <strong>of</strong> America, 77(5), 1491-1513.− Sabetta F., Pugliese A., 1996. Estimation <strong>of</strong> response spectra andsimulation <strong>of</strong> nonstationary earthquake ground motions. Bulletin <strong>of</strong> theSeismological Society <strong>of</strong> America, 86(2), 337-352.− Singhal A., Kiremidjian A.S., 1996. Method for probabilistic evaluation<strong>of</strong> seismic structural damage. ASCE Journal <strong>of</strong> Structural Engineering,122(12), 1459-1467.− Singhal A., Kiremidjian A.S., 1998. Bayesian updating <strong>of</strong> fragilities withapplication to <strong>RC</strong> frames. ASCE Journal <strong>of</strong> Structural Engineering,124(8), 922-929.− Spence R.J.S., Coburn A.W., Sakai S., Pomonis A., 1991. Aparameterless scale <strong>of</strong> seismic intensity for use in the seismic riskanalysis and <strong>vulnerability</strong> assessment. International Conference onEarthquake, Blast and Impact, Manchester, UK, September 19-20. Pp.19-30.− Verderame G.M., De Luca F., Ricci P., Manfre<strong>di</strong> G., 2010. Preliminaryanalysis <strong>of</strong> a s<strong>of</strong>t storey mechanism after the 2009 L’Aquila earthquake.


48 Chapter I - Assessing the seismic <strong>vulnerability</strong> <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>Earthquake Engineering and Structural Dynamics. DOI:10.1002/eqe.1069− Whitman R.V., Anagnos T., Kircher C.A., Lagorio H.J., Lawson R.S.,Schneider P., 1997. Development <strong>of</strong> a national earthquake lossestimation methodology. Earthquake Spectra, 13(4), 643-661.− Whitman R.V., Reed J.W., Hong S.T., 1973. Earthquake DamageProbability Matrices. Procee<strong>di</strong>ngs <strong>of</strong> the 5 th World Conference onEarthquake Engineering, Rome, Italy, June 25-29. Vol. 2, pp. 2531-2540.− Yakut A., 2004. Preliminary seismic performance assessment procedurefor <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>. Engineering Structures, 26(10), 1447-1461.


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 49Chapter II<strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete<strong>buil<strong>di</strong>ngs</strong>2.1 GENERAL REMARKSOr<strong>di</strong>nary reinforced concrete structures cannot sustain large earthquakesremaining in elastic field: they have to be enough ductile to <strong>di</strong>ssipate energywithstan<strong>di</strong>ng large deformations into inelastic field without collapsing. Thiscould appear like a trivial issue, but it is the main idea at the basis <strong>of</strong> the majorbreakthrough in earthquake engineering philosophy: the shift from Force-Basedto Deformation-Based approach and the formulation <strong>of</strong> “Capacity Design”principles (Hollings, 1968a,b; Paulay and Priestley, 1992). Accor<strong>di</strong>ng to theseprinciples, when designing a reinforced concrete structure for earthquake loads,a desired collapse mechanism has to be established first. This mechanism has tobe the most energy-<strong>di</strong>ssipating possible, i.e., under this mechanism the structurehas to show the largest <strong>di</strong>splacement (ductility) capacity. To this end, among allthe possible mechanisms, the one that is characterized by the lowest localductility demand, given equal the global ductility (i.e., the one that ischaracterized by the highest global ductility, given equal the local ductilitydemand), is chosen, thus lea<strong>di</strong>ng to the well-known global collapse mechanism(see Figure 2.1.1).


50 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>Figure 2.1.1. Comparison <strong>of</strong> energy-<strong>di</strong>ssipating mechanisms (Paulay and Priestley, 1992)Furthermore, the “strength hierarchy” principle has to be respected, ensuringthe development <strong>of</strong> inelastic deformations in the highest possible number <strong>of</strong>ductile elements and not in elements with lower rotational capacity (that is, inbeams and not in columns, due to the <strong>di</strong>fferent axial load) and provi<strong>di</strong>ng anoverstrength to undesired failure mechanisms – such as shear failure, buckling<strong>of</strong> longitu<strong>di</strong>nal reinforcement, anchorage failure or beam-column joint failure –since these kinds <strong>of</strong> brittle failure mechanisms would limit or even inhibit thedevelopment <strong>of</strong> ductile, energy-<strong>di</strong>ssipating mechanisms (see Figure 2.1.2), suchas the flexural ones.Figure 2.1.2. The chain analogy: the strength <strong>of</strong> brittle links has to be higher than the strength <strong>of</strong>ductile links, in order to ensure a ductile failure mechanism to develop instead <strong>of</strong> a brittle one(Paulay and Priestley, 1992)


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 51These concepts lead to a series <strong>of</strong> design prescriptions. For instance, a shearstrength higher than the flexural strength has to be provided to each element,independent <strong>of</strong> the force demand evaluated from analysis, in order to preventany possibility <strong>of</strong> shear failure. The development <strong>of</strong> inelastic deformations inbeams rather that in columns, thus avoi<strong>di</strong>ng a local column-sway (less energy<strong>di</strong>ssipating)collapse mechanism (see Figure 2.1.1), is ensured provi<strong>di</strong>ng anhigher flexural strength to column elements compared to beam elements (weakbeam/strong column con<strong>di</strong>tion).Prescriptions are provided not only to avoid the onset <strong>of</strong> brittle failuremechanisms, but also to increase the ductility capacity: higher the materialstrain ductility, higher the section curvature ductility, higher the elementrotational ductility, higher the global structural ductility.At material level, for instance, a higher ductility <strong>of</strong> concrete is given by ahigher confinement: to this end, prescriptions about spacing and anchoragedetail <strong>of</strong> transverse reinforcement in plastic hinge region are <strong>of</strong> importance. Therepresentation <strong>of</strong> the beneficial influence <strong>of</strong> these prescriptions at material orsection level is <strong>of</strong>ten completely conventional and far from the actual structuralbehaviour. As an example, an upper limit to longitu<strong>di</strong>nal reinforcement ratio isprescribed in order to the increase the section curvature capacity, but at large<strong>di</strong>splacements the plane section assumption in critical regions is quite far fromreality, and it makes no sense to talk about section curvature. However, theseprescriptions at material or section level do have a <strong>di</strong>rect beneficial effect onelement ductility capacity. A way to account for this effect has to be found,although it is not easy to be modelled. From this point <strong>of</strong> view, experimentalactivity is <strong>of</strong> fundamental importance.At element level, an increase in ductility capacity can be achieved (or better,a limitation in ductility capacity can be avoided) through prescription aimed atavoi<strong>di</strong>ng the onset <strong>of</strong> brittle failure mechanisms such as buckling <strong>of</strong>compressed longitu<strong>di</strong>nal reinforcement or anchorage failure.At structural level, a regular <strong>di</strong>stribution <strong>of</strong> mass, stiffness and strength isalso prescribed, in order to avoid a collapse mechanism characterized by a


52 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>localization <strong>of</strong> inelastic <strong>di</strong>splacement demand since this kind <strong>of</strong> mechanismwould provide – as already illustrated – a low global ductility. For the samereason, modern seismic codes also prescribe a local increase in design seismicdemand to account for the effects <strong>of</strong> an irregular <strong>di</strong>stribution <strong>of</strong> nonstructuralelements such as infill walls (e.g., “pilotis” effect).Most <strong>of</strong> the <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> in seismic areas were not designed incompliance with the above illustrated principles, even if they were designed forseismic loads. As far as Italy is concerned, Capacity Design method was fullyadopted only by very recent seismic codes (see Section 2.5.2), while a majorpart <strong>of</strong> the buil<strong>di</strong>ng stock was constructed in compliance with older seismiccodes or even for gravity loads only since not all the national territory wasclassified yet as seismic.As a result, even if an <strong>existing</strong> <strong>RC</strong> buil<strong>di</strong>ng was properly designedaccor<strong>di</strong>ng to an old seismic code, anyhow it does not have the same (local andglobal) ductility as a contemporary buil<strong>di</strong>ng since its design procedure <strong>di</strong>d notrespect some fundamental principles <strong>of</strong> modern earthquake engineering (e.g.,strength hierarchy).Furthermore, some critical issues have to be considered when capacitymodels are formulated for elements that were not designed accor<strong>di</strong>ng to theabove illustrated principles (i.e., substandard elements). For instance, ductiledeformation mechanisms can <strong>di</strong>ffer greatly from the same mechanisms incontemporary elements.In this Chapter, specific issues about the (ductile) deformation mechanisms<strong>of</strong> substandard elements are <strong>di</strong>scussed in Section 2.2, with emphasis on <strong>RC</strong>columns with smooth bars.Then, main capacity models for shear resistance <strong>of</strong> <strong>RC</strong> members and forbeam-column joints are briefly reported and <strong>di</strong>scussed (Sections 2.3, 2.4).Finally, an analysis <strong>of</strong> structural damage to <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> in L’Aquila afterthe 6 th April 2009 earthquake is presented, together with an overview <strong>of</strong> pastseismic code prescriptions, thus highlighting the typical deficiencies <strong>of</strong> <strong>existing</strong><strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> through observed damage (Section 2.5).


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 532.2 MEMBERS CONTROLLED BY FLEXURAL AND AXIAL LOADSIn this Section, specific issues about ductile deformation mechanisms <strong>of</strong> <strong>RC</strong>members are <strong>di</strong>scussed, with emphasis on members with smooth bars. As amatter <strong>of</strong> fact, this kind <strong>of</strong> reinforcement is widely spread among <strong>existing</strong> <strong>RC</strong><strong>buil<strong>di</strong>ngs</strong>, and its presence can highly influence the deformation mechanisms <strong>of</strong><strong>RC</strong> members.The results reported herein were published in (Verderame et al., 2010).A <strong>di</strong>scussion about code formulations for the assessment <strong>of</strong> deformationcapacity <strong>of</strong> <strong>RC</strong> members is carried out in Section 2.2.1.Then, an experimental-based study on ultimate deformation capacities <strong>of</strong>column with smooth bars is presented, lea<strong>di</strong>ng to a new proposal about codeprescriptions (Section 2.2.2).Bond between concrete and reinforcing bars can significantly influencedeformation mechanisms <strong>of</strong> <strong>RC</strong> members. Hence, an experimental study onbond capacities <strong>of</strong> smooth bars is reported, together with the formulation <strong>of</strong> acapacity model (Section 2.2.3).The deformation capacity <strong>of</strong> substandard <strong>RC</strong> members may be affected bylimitations due to the absence <strong>of</strong> proper seismic details. Among these,transverse reinforcement details (i.e., stirrup spacing and anchorage) are <strong>of</strong>importance. In Section 2.2.4 this issue is analyzed through the results <strong>of</strong> anexperimental campaign.In Section 2.2.5 the fixed-end rotation mechanism is investigated through anumerical model <strong>of</strong> a column element inclu<strong>di</strong>ng the end hooked bars,representing a typical anchorage detail for this kind <strong>of</strong> elements.2.2.1. Code provisions for the assessment <strong>of</strong> ultimate deformation capacityThe use <strong>of</strong> non-linear analysis methods to determine the seismic capacity <strong>of</strong><strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> requires knowledge <strong>of</strong> the actual post-elastic rotational capacities<strong>of</strong> each element (beams, columns) both in monotonic field, for non-linear staticanalysis, and in cyclic field, for non-linear dynamic analysis. In monotonicfield, a series <strong>of</strong> parameters (yiel<strong>di</strong>ng, peak resistance, ultimate state) has to be


54 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>defined, in order to define the response curve <strong>of</strong> the element. In cyclic field,hysteretic rules and strength and stiffness degradation models have to bedefined; they significantly influence the assessment <strong>of</strong> ultimate rotationalcapacity. Nevertheless, these rules are not easy to define, due to the number <strong>of</strong>geometrical and mechanical parameters and to the uncertainties involved. Forexample, the type <strong>of</strong> loa<strong>di</strong>ng influences in a not negligible way the response <strong>of</strong>the <strong>RC</strong> element. Most <strong>of</strong> the code prescriptions only define the deformationcapacity at characteristic envelope points, such as the elastic limit (yiel<strong>di</strong>ng)and the ultimate con<strong>di</strong>tion (collapse); therefore, based on these prescriptions, itis not possible to completely define the strength degradation <strong>of</strong> the monotonicenvelope, nor the hysteretic behaviour through appropriate rules.Generally, deformation at yiel<strong>di</strong>ng is evaluated as a chord rotation,accounting for <strong>di</strong>fferent contributions correspon<strong>di</strong>ng to ben<strong>di</strong>ng, shear andfixed-end rotation deformation mechanisms.The rotational capacity is generally evaluated referring to a fixed strengthdecay (20%) with respect to the peak resistance, evaluated on the force<strong>di</strong>splacementenvelope curve. It is clear that this definition is stronglyinfluenced by the maximum resistance con<strong>di</strong>tion, as well as the post-peakdegradation, monotonic or cyclic. It is <strong>di</strong>fficult to define a relationship betweenthe element parameters and the rotational capacity, due to the complexphenomena influencing the post-elastic deformation behaviour and to thenatural variability affecting these phenomena.European code (CEN, 2005), consistent with the methodologies develope<strong>di</strong>n literature, proposes two main approaches: a mechanical-empirical approach,based on plastic hinge length concept, and a purely empirical approach.Accor<strong>di</strong>ng to the USA code approach (referring in particular to ASCE/SEI41 update provisions (Elwood et al., 2007)), deformation capacity is evaluatedfrom a dataset <strong>of</strong> empirical data (Berry et al., 2004), assuming a categorization<strong>of</strong> columns based on failure mode and selecting target probabilities <strong>of</strong> failurefor each failure mode.In this Section, both European and USA code prescriptions for the


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 55evaluation <strong>of</strong> deformation capacity <strong>of</strong> <strong>RC</strong> members – with a special focus onthe assessment <strong>of</strong> <strong>existing</strong> <strong>buil<strong>di</strong>ngs</strong> – are reported and <strong>di</strong>scussed, together withtheir background theory.2.2.1.1. EC8 part 3.3 – empirical approachEurocode 8–Part 3 at Section A.3.2.2 (Limit State <strong>of</strong> Near Collapse)provides expressions for the evaluation <strong>of</strong> ultimate element capacity <strong>of</strong> <strong>RC</strong>elements. The value <strong>of</strong> total chord rotation capacity under cyclic loa<strong>di</strong>ng,following an empirical approach, is given by [EC8 - Eq. (A.1)]:0.35 ⎛ fyw⎞⎜αρsxf ⎟⎝ c ⎠ 100ρd25 (1.25 )( ′)( )1 νθum= 0.016 ⋅ (0.30 ) ⎢ fc ⎥γelmax 0.01;ω⎛ L⎜⎝ hV⎞⎟⎠⎡ max 0.01;ω⎣⎤⎦0.225(2.2.1.1)where γ el , equal to 1.5 for primary seismic elements and to 1.0 for secondaryseismic elements, is meant to convert mean values <strong>of</strong> chord rotation to meanminus-one-standard-deviationones. The code also provides another expressionfor the evaluation <strong>of</strong> the plastic part <strong>of</strong> the ultimate chord rotation [EC8 - Eq.(A.3)]:0.35 ⎛ fyw⎞αρsx0.2 L⎛ V ⎞ ⎜ f ⎟⎝ c ⎠ 100ρdfc25 (1.275 )( ′)( )1 ⎡max 0.01;ω0.0145 (0.25 )⎣plνθum= θum − θy= ⋅ ⎢ ⎥γelmax 0.01;ω⎜⎝h⎟⎠⎤⎦0.3(2.2.1.2)To evaluate the total chord rotation, the plastic part calculated accor<strong>di</strong>ng tothis formula should be added to the rotation at yiel<strong>di</strong>ng [EC8 - Eq. (A.10)].The values <strong>of</strong> chord rotation calculated accor<strong>di</strong>ng to (2.2.1.1) and (2.2.1.2)apply to elements with ribbed bars, seismically detailed and without lapping <strong>of</strong>longitu<strong>di</strong>nal bars in the vicinity <strong>of</strong> the end region where yiel<strong>di</strong>ng is expected(plastic hinge region).The correction coefficient applied to members with ribbed bars without


56 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>seismic detailing is equal to 0.825 for both formulas. If the longitu<strong>di</strong>nal ribbedbars are lapped, expressions (2.2.1.1) and (2.2.1.2) should be applied doublingthe mechanical compression reinforcement ratio ( ω′). Moreover, if the laplength is less than the minimum valuel ou, min :⎡f yw ⎤l ou,min= dbLfyL / ⎢(1.05+ 14.5α1ρsx ) fc⎥(2.2.1.3)⎣fc⎦Another reduction factor equal to ( lo / lou,min ) should be applied, calibratedonly for expression (2.2.1.2), that is only for the plastic part <strong>of</strong> chord rotation.Corrections applied to the chord rotation at yiel<strong>di</strong>ng are given at SectionA.3.2.4(3) <strong>of</strong> the code; they are omitted here for the sake <strong>of</strong> brevity.In elements with smooth bars the chord rotation evaluated accor<strong>di</strong>ng to(2.2.1.1) should be multiplied by 0.575, while the plastic part <strong>of</strong> chord rotationgiven by (2.2.1.2) should be multiplied by to 0.375. It is worth noting that bothcoefficients already include the reduction factor equal to 0.825, accounting forthe lack <strong>of</strong> seismic detailing. If longitu<strong>di</strong>nal bars are lapped in members withsmooth bars, another coefficient has to be adopted, depen<strong>di</strong>ng on the lap lengthl ) and the shear span ( L ). For total chord rotation, it is given by:( o[ min(50,l / d )](1− l / L )V0.0025180+o bL o V(2.2.1.4)while for the only plastic part it is:[ min(50,l / d )](1− l / L )0.0035 60 + o bL o V(2.2.1.5)Moreover, shear span in expressions (2.2.1.1) and (2.2.1.2) should bereduced by the lap length l o , assuming that the ultimate con<strong>di</strong>tion is controlledby the region right after the end <strong>of</strong> the lap.A document has been presented (“Corrigenda to EN 1998-3” – DocumentCEN/TC250/SC8/N437A (CEN, 2009)) changing some provisions <strong>of</strong> Eurocode8 – part 3 (CEN, 2005), also inclu<strong>di</strong>ng prescriptions about ultimate deformationcapacity <strong>of</strong> members with smooth bars, which have been illustrated herein. Thecoefficients 0.575 and 0.375, applied to Eqs. (2.2.1.1) and (2.2.1.2) for


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 57elements with smooth bars, have been changed into 0.80 and 0.75 respectively.In both cases, these coefficients already include the reduction factor accountingfor the lack <strong>of</strong> seismic detailing, which has been changed from 0.825 to(1/1.20=0.833). Formulations (2.2.1.4) and (2.2.1.5), for elements with lapping<strong>of</strong> longitu<strong>di</strong>nal smooth bars, have been significantly changed, too. Expression(2.2.1.4), applied to total ultimate chord rotation, has been replaced by:[ min(40,l / d )]0.019 10 +o bL(2.2.1.4a)Expression (2.2.1.5), applied to the plastic part <strong>of</strong> ultimate chord rotation,has been replaced by:0bL.019min(40,lo / d )(2.2.1.5a)In these cases, coefficients do not include the reduction factor accountingfor the lack <strong>of</strong> seismic detailing – equal to 1/1.20 – which has to be applied.The deformation capacity <strong>of</strong> elements with smooth bars – evaluated bymeans <strong>of</strong> coefficients applied to Eq. (2.2.1.1) or Eq. (2.2.1.2) – accor<strong>di</strong>ng to(CEN, 2009) is higher than previously prescribed by (CEN, 2005).In the following, both the formulations given in draft 2005 <strong>of</strong> Eurocode 8 –part 3 and the later proposed changes will be reported. They will by referred toas (CEN, 2005) and (CEN, 2009) respectively.Background theoryFormulas for the evaluation <strong>of</strong> rotational capacity can be obtained with atotally empirical approach, based on experimental data, with pure numericalregression analyses.In (Haselton and Deierlein, 2007), based on 255 experimental tests fromPEER database (Berry et al., 2004), empirical expressions for characteristicparameters <strong>of</strong> a <strong>RC</strong> element model (e.g., stiffness, rotation capacity, etc.), alsoinclu<strong>di</strong>ng cyclic behaviour. These parameters are chosen accor<strong>di</strong>ng to the modelproposed in (Ibarra et al., 2005). Empirical expressions for the ultimatedeformation capacity are also proposed in (Rossetto, 2002; Zhu et al, 2007).This kind <strong>of</strong> formulations can also be derived from a small number <strong>of</strong>


58 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>experimental data, when a specific typology <strong>of</strong> <strong>RC</strong> element is investigated. In(Lam et al., 2003), based on a few number <strong>of</strong> experimental tests, expressionsfor the assessment <strong>of</strong> deformation capacity <strong>of</strong> rectangular <strong>RC</strong> columns with lowlateral confinement and high-axial load are proposed.A <strong>di</strong>fferent approach is proposed in (Peruš et al., 2006; Peruš et al., 2007).Authors elaborate a method for the pre<strong>di</strong>ction <strong>of</strong> flexural deformation capacity,but also <strong>of</strong> the whole force-drift envelope, by means <strong>of</strong> CAE method (a specialtype <strong>of</strong> multi-<strong>di</strong>mensional non-parametric regression) applied to a subset <strong>of</strong>Far<strong>di</strong>s and PEER databases. This method shows a better pre<strong>di</strong>ction capacitycompared to EC8 formulations.Among the <strong>di</strong>fferent empirical expressions proposed in literature, theexpression proposed in (Panagiotakos et al., 2001) represents a reference for theabove illustrated code formulas (CEN, 2005). This experimental databaseconsists in 633 cyclic tests and 242 monotonic tests on beams, columns andwalls, which do not present brittle failure mechanisms. The relationship is alinear regression <strong>of</strong> the logarithm <strong>of</strong>θ u on the control variables or theirlogarithms, without coupling. Only control variables which turn out to bestatistically significant for the pre<strong>di</strong>ction <strong>of</strong> θ u are retained. Separate regressionanalyses for monotonic tests and for cyclic ones are performed. To obtain amore representative experimental database, with particular regard to memberswith unsymmetric reinforcement well represented in monotonic tests, anotherregression analysis on all 875 tests is performed, lea<strong>di</strong>ng to the followingexpression:θu= αst⋅αcyc⎛ αsl⎞⎛α⋅⎜1+⎟⎜1−⎝ 2.3 ⎠⎝3( 0.01;ω )( 0.01;ω )ν ⎡ max ′ ⎤(0.20 ) ⎢fcmax⎥⎣⎦0.275wall⎛ L⎜⎝ hV⎞⎟⎠⎞⎟⎠0.451.1⎛ fyw ⎞⎜100αρsx⎟⎝ fc ⎠(1.30100ρ d)(2.2.1.6)The ratio between the experimental ultimate rotation and the numericalvalue provided by (2.2.1.6) has mean equal to 1.06, me<strong>di</strong>an equal to 1.00 and


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 59CoV <strong>of</strong> 47%.During years, together with the extension <strong>of</strong> the experimental database, thecoefficients in this expression have been slightly mo<strong>di</strong>fied. The last proposal,given in (Far<strong>di</strong>s, 2007), is based on 1307 monotonic and cyclic tests:θu= αst⋅(1− 0.43αcyc( 0.01;ω )( 0.01;ω )ν ⎡ max ′ ⎤(0.30 ) ⎢fcmax⎥⎣⎦⎛ αsl⎞⎛3) ⋅⎜1+⎟⎜1−α⎝ 2 ⎠⎝80.225⎛ L⎜⎝ hV⎞⎟⎠0.3525wall⎞⎟⎠⎛ fyw ⎞⎜ αρsx ⎟⎝ fc ⎠(1.25100ρ d)(2.2.1.7)The mean value <strong>of</strong> the ratio between the experimental ultimate rotation andthe numerical value provided by (2.2.1.7) is 1.05, the me<strong>di</strong>an is equal to 0.995and the CoV is <strong>of</strong> 42.8%. The comparison between the coefficients <strong>of</strong> variationclearly shows the better pre<strong>di</strong>ction capacity <strong>of</strong> (2.2.1.7), due to the growth <strong>of</strong>experimental knowledge state.In the same work, a regression analysis for the only plastic part is alsopresented, which was already proposed in (CEB-FIB, 2003) based on 1100experimental tests. The expression is:θplu= αplst⋅(1− 0.52αcyc( 0.01;ω )( 0.01;ω )ν ⎡ max ′ ⎤(0.25 ) ⎢max⎥⎣⎦⎛ αsl⎞) ⋅⎜1+⎟⎝ 1.6 ⎠0.300.20fc⎛ L⎜⎝ h( 1−0.4α)V⎞⎟⎠0.3525wall⎛ fyw ⎞⎜ αρsx ⎟⎝ fc ⎠(1.275100ρ d)(2.2.1.8)The mean value <strong>of</strong> the ratio between the experimental ultimate rotation andthe correspon<strong>di</strong>ng numerical pre<strong>di</strong>ction is 1.05, the me<strong>di</strong>an is equal to 0.995and the CoV is <strong>of</strong> 42.7%, against the 47% in the first proposal (see Eq. 2.2.1.6).Expressions (2.2.1.1) and (2.2.1.2) proposed in EC8 almost perfectly agreewith (2.2.1.7) and (2.2.1.8), assumingslip),α wall =0 (only beams and columns) and α st =α cyc =1 (cyclic loa<strong>di</strong>ng), α sl =1 (withplstα =0.0185 (hot-rolledductile steel).Consistent with the characteristic <strong>of</strong> tests included in the experimental


60 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>database, the proposed expressions for the ultimate rotational capacity shouldbe applied only to members with ribbed bars, with seismic detailing andwithout lapping <strong>of</strong> longitu<strong>di</strong>nal bars in the vicinity <strong>of</strong> plastic hinge region, thatis, to members which are not representative <strong>of</strong> <strong>existing</strong> <strong>buil<strong>di</strong>ngs</strong>. Authorsdefine correction coefficients allowing to extend the use <strong>of</strong> these expressions tomembers with <strong>di</strong>fferent characteristics. These coefficients are calibrated tocounterbalance the mean error evaluated through the comparison betweenvalues from expressions (2.2.1.7) and (2.2.1.8) and results <strong>of</strong> experimental testson non-conforming members, not included in the original (primary) database.This approach, certainly approximated, is necessary because <strong>of</strong> the smallnumber <strong>of</strong> experimental data for these members. Because <strong>of</strong> the low number <strong>of</strong>these data, it seems to be allowed to suppose that their inclusion in the databasewould have not led to any significant change in the regression expression.Moreover, applying the primary expression to members <strong>of</strong> <strong>di</strong>fferent typologies,only using a multiplicative coefficient, is the same as postulating that theultimate rotation depends on the control parameters by the same way,independently <strong>of</strong> the specific characteristics <strong>of</strong> considered elements.Nevertheless, the assumed methodology seems to be the only one that can befollowed, due to the few experimental data now available for this kind <strong>of</strong>elements. A higher reliability can be obtained only by exten<strong>di</strong>ng theexperimental database, so that a wider range <strong>of</strong> loa<strong>di</strong>ng con<strong>di</strong>tions andgeometrical and mechanical characteristics can be covered. In Table 2.2.1.1correction coefficients and the extension <strong>of</strong> the correspon<strong>di</strong>ng experimentaldatabases used for calibrations are reported.


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 61Element Typew/o seismicdetailing and w/continuousribbed barsw/o seismicdetailing w/hooked smoothbars and w/ orw/o lap-splicingover plastichingelengthw/o seismicdetailing w/hooked smoothbars and w/ orw/o lap-splicingover plastichingelengthCorrectionFactor# <strong>of</strong>data0.85 270.825 42( ( ))0.015 ⋅ 10 + min 40;lodb15(1 / 1.20 ⋅ 0.019 ⋅ 10+min 40;lodb(-Mean - Me<strong>di</strong>anCoV(corrected data)(-) – (1.00)(-)(1.00) – (1.005)(33.6%)(1.07) – (0.975)(32%)(-) – (-)(-)Table 2.2.1.1. Correction factors for non-detailed membersReference(Panagiotakoset al., 2002;CEB-FIB,2003)(Biskinis andFar<strong>di</strong>s, 2004;CEN, 2005)(Far<strong>di</strong>s, 2006)(CEN, 2009)2.2.1.2. EC8 part 3.3 – mechanical approachAccor<strong>di</strong>ng to (CEN, 2005), the ultimate rotation may also be calculatedfollowing an equivalent mechanical approach through the evaluation <strong>of</strong> theplastic ultimate section curvature φ − φ ) , assumed to be constant over theplastic hinge length( u yL pl , which is empirically calibrated. Hence, the ultimaterotational capacity may be evaluated accor<strong>di</strong>ng to [EC8 - Eq. (A.4)]:θum1=γel⎛⎜θ⎝y+ ( φu− φy)Lpl⎛ L⎜1− 0.5⎝ LplV⎞⎞⎟⎟⎠⎠(2.2.1.9)Section curvatures at ultimate and at yiel<strong>di</strong>ng are calculated based on thefirst principles, with the constitutive relationships given by Eurocode 2 (CEN,2004). If the concrete confinement model given in 3.1.9 in Eurocode 2 is


62 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>assumed, the plastic hinge length is equal to [EC8 - Eq. (A.5)]:dbLfyL pl = 0.10LV+ 0.17h + 0.24(2.2.1.10)fcIf the confinement model proposed by Eurocode 8 – part 3 is adopted, betterrepresenting the effects <strong>of</strong> confinement under cyclic loa<strong>di</strong>ng, the plastic hingelength is given by:LdbLfy= 0.11(2.2.1.11)30fVL pl + 0.20h +cFor expressions (2.2.1.10) and (2.2.1.11) no correction factor accounting forthe above mentioned deficiencies is given. Therefore, they should only beapplied to members with ribbed bars, seismically detailed and without lapping<strong>of</strong> longitu<strong>di</strong>nal bars.Background theoryFrom a phenomenological standpoint, the plastic hinge region can beidentified with the zone <strong>of</strong> the element where yiel<strong>di</strong>ng <strong>of</strong> reinforcement andconcrete crushing take place. The plastic hinge length used in the evaluation <strong>of</strong>the element rotational capacity is, instead, purely conventional. It onlyrepresents the length over which ultimate section curvature, assumed to beconstant, is integrated, following an equivalent ben<strong>di</strong>ng approach, to calculatethe effective chord rotation inclu<strong>di</strong>ng shear and fixed-end rotation contributionsto the overall deformability <strong>of</strong> the member; the curvature is calculated based onBernoulli’s plane section assumption.The plastic hinge length can not be evaluated based on a purely mechanicalapproach. As a matter <strong>of</strong> fact, based on section equilibrium con<strong>di</strong>tions and fullinteractionhypothesis, in a post-peak phase the curvature should increase onlyat the base section <strong>of</strong> the element (zero length hinge problem) (Daniell et al.,2008; Haskett et al., 2009). Moreover, a purely mechanical approach, lea<strong>di</strong>ng tothe evaluation <strong>of</strong> flexural deformability, would not account for other


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 63deformation mechanisms such as shear deformability and slippage <strong>of</strong>reinforcing bars from the connection element. These contributions are notnegligible at all. Shear mechanisms may contribute in the overall post-elasticmember deformability up to 30% (Fenwick and Megget, 1993), whilst the endrotation due to the slippage <strong>of</strong> reinforcing bars may contribute up to 40%(Sezen, 2002).Therefore, researchers over years have empirically calibrated the plastichinge length over which theoretical ultimate section curvature is integrated,aiming at achieving the best agreement with experimental values <strong>of</strong> ultimatechord rotation.Following this approach, rotational capacity <strong>of</strong> an element may be expressedas:θ = θ + ( φ − φ ) L(2.2.1.12)uyuwhere the plastic hinge lengthy<strong>di</strong>fferent deformation mechanisms:plpl,flexpl,shearplpl,slipL pl is made up <strong>of</strong> three terms, correspon<strong>di</strong>ng toL = L + L + L(2.2.1.13)Table 2.2.1.2 reports main formulations that have been proposed over years,starting from the first fundamental work by Baker (1956). These expressionsshow that the shear span L V and the section depth h are the major variablesinfluencing the plastic hinge length, while the term correspon<strong>di</strong>ng to fixed-endrotation is generally proportional to <strong>di</strong>ameter and yiel<strong>di</strong>ng strength <strong>of</strong>longitu<strong>di</strong>nal reinforcement bars. First proposed formulations are mainlycalibrated based on experimental tests on beam elements, therefore the fixedendrotation contribution is not clearly evaluated. In recent formulations,calibrated also on column elements, this contribution is clearly represente<strong>di</strong>nstead.


64 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>Reference Plastic hinge length (L pl )(Baker, 1956) ( ) 1 4k k k ⋅ z d ⋅ d1 2 3(Mattock, 1964)d ⎡ ⎛ '1 1.14 ⎞⎛⎛1 1⎤− ⎞ ⎞⋅ ⎢ + ⎜ − ⎟⎜−⎜ ⎟⎥2 ⎢ ⎝ d ⎠⎜⎜ q b ⎟ 16.2 ⎟⎥⎣⎝ ⎝ ⎠ ⎠⎦(Corley, 1966)d z+ 0.22 d(Mattock, 1967)d+ 0.05z2(Park, 1982) 0.4h(Priestley et al., 1987) 0.08L+ 6dv b(Paulay et al., 1992) 0.08L + 0.022d fv b y(Panagiotakos et al., 2001)0.12L + 0.014 α d f for cyclic loa<strong>di</strong>ngv sl b y0.18L + 0.021 α d f for monotonic loa<strong>di</strong>ngv sl b y(Far<strong>di</strong>s, 2007)0.09L+ 0.2 h for cyclic loa<strong>di</strong>ngv0.04L+ 1.2 h for monotonic loa<strong>di</strong>ngvTable 2.2.1.2. Empirically derived plastic hinge lengthsMoreover, in (2.2.1.12) the ultimate con<strong>di</strong>tion is given in terms <strong>of</strong> curvatureφ u , depen<strong>di</strong>ng, based on plane section hypothesis, on steel or concrete failure.Nevertheless, the evaluation <strong>of</strong> ultimate curvature is not easy or univocal, dueto the influence <strong>of</strong> some aspects as concrete confinement, spalling <strong>of</strong> theconcrete cover or buckling <strong>of</strong> compressive reinforcing bars. For example, theuse <strong>of</strong> <strong>di</strong>fferent confinement models may significantly influence thedetermination <strong>of</strong> the ultimate curvature, therefore the plastic hinge length canassume very <strong>di</strong>fferent values.The plastic hinge formulation proposed in (Panagiotakos et al., 2001) is themost interesting among the expressions presented in literature. It is based on anextensive experimental database, which will be <strong>di</strong>scussed in the next paragraph.


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 65θuThe ultimate chord rotation is given by:φyL=3V+ ( φu− φy)Land the plastic hinge lengthpl⎛ L⎜1− 0.5⎝ LplV⎞⎟⎠(2.2.1.14)L pl is given as a linear function <strong>of</strong> shear span(ben<strong>di</strong>ng contribution) and <strong>of</strong> the product ( f y d bL)(fixed-end contribution):Lpl= αL+ β(fd )(2.2.1.15)VybLCoefficients α and β are derived from a regression analysis onexperimental data; they are equal, respectively, to 0.12 and to 0.0014 for cyclictests and to 0.18 and 0.0021 for monotonic ones. The ultimate curvatureL Vφ u isevaluated accounting both for the concrete confinement and for the spalling <strong>of</strong>the concrete cover. In particular, for cyclic tests the mean and me<strong>di</strong>an <strong>of</strong> theexperimental-to-pre<strong>di</strong>cted ratio for expression (2.2.1.14), using (2.2.1.15), areequal to 1.23 and 0.99 respectively, with a Coefficient <strong>of</strong> Variation (CoV) <strong>of</strong>83%; while for monotonic tests the mean and me<strong>di</strong>an are equal to 1.37 and 1.01respectively, with a CoV <strong>of</strong> 94%.The last plastic hinge expression proposed by (Far<strong>di</strong>s, 2007), based on amore extensive experimental database, is depen<strong>di</strong>ng not on the shear spanbut also on the height h <strong>of</strong> the section. Moreover, the fixed-end rotationcontribution is evaluated with a separate term:θu= θwith:Ly⎛ Lpl⎞+ ( θ u,slip − θ y,slip ) + ( φ u − φ y )Lpl⎜1− 0.5⎟(2.2.1.16)⎝ LV⎠= 0.09L 0.20h(2.2.1.17)pl V +where:φyLV⎛ h ⎞ φydbLfyθ y = + 0.0013 1 1.5 +3⎜ +L⎟(2.2.1.18)⎝ V ⎠ 8 fcL V


66 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>φydbLfyθ y,slip =(2.2.1.19)8 fcφudbLfyθ u,slip =(2.2.1.20)16 fcThe use <strong>of</strong> the illustrated relationships, together with the confinement modelshown in the same work, leads to an experimental-to-pre<strong>di</strong>cted ratio with meanand me<strong>di</strong>an, on a database <strong>of</strong> 1307 experimental tests, equal to 1.105 and 0.994respectively, with a CoV <strong>of</strong> 53.6%.Expressions (2.2.1.14) e (2.2.1.16), although provi<strong>di</strong>ng a <strong>di</strong>fferentevaluation <strong>of</strong> the fixed-end contribution, present the same control variables <strong>of</strong>the code expression (2.2.1.9), which <strong>di</strong>rectly shows, in the calculation <strong>of</strong> plastichinge length, the dependence on all the above mentioned parameters.2.2.1.3. ASCE/SEI 41 approachASCE/SEI 41 (2007) is the latest in a series <strong>of</strong> documents developed toassist engineers with the seismic assessment and rehabilitation <strong>of</strong> <strong>existing</strong><strong>buil<strong>di</strong>ngs</strong> (FEMA 273, 1997; FEMA 356, 2000). A document has beenproposed (Elwood et al., 2007) for updating provisions related to <strong>existing</strong>reinforced concrete <strong>buil<strong>di</strong>ngs</strong>. Based on experimental data and empiricalmodels, this document also provides a revision <strong>of</strong> deformation capacityparameters for older-type <strong>RC</strong> columns. This proposal is described in thefollowing.<strong>RC</strong> columns with 135 degree hooked transverse reinforcement arecharacterized by three <strong>di</strong>fferent failure modes:• Con<strong>di</strong>tion i: Flexure failure (flexural yiel<strong>di</strong>ng without shear failure)• Con<strong>di</strong>tion ii: Flexure-shear failure (shear failure following flexuralyiel<strong>di</strong>ng)• Con<strong>di</strong>tion iii: Shear failure (shear failure before flexural yiel<strong>di</strong>ng)depen<strong>di</strong>ng on the ratio between the plastic shear (which represents the demand


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 67shear, correspon<strong>di</strong>ng to the flexural strength <strong>of</strong> the element) V p and the nominalshear strength V n , as reported in Table 2.2.1.3.V /(V / k)0.60ACI conformingdetails with 135°hooksTransverse Reinforcement DetailsClosed hoopswith 90° hooksOther (inclu<strong>di</strong>nglap-splicedtransversereinforcement)p n≤ Con<strong>di</strong>tion i Con<strong>di</strong>tion ii Con<strong>di</strong>tion ii1.00≥ Vp /(Vn/ k) > 0.60 Con<strong>di</strong>tion ii Con<strong>di</strong>tion ii Con<strong>di</strong>tion iiiV /(V / k)1.00p n> Con<strong>di</strong>tion iii Con<strong>di</strong>tion iii Con<strong>di</strong>tion iiiTable 2.2.1.3. Categorization <strong>of</strong> failure modes for older-type <strong>RC</strong> columns (Elwood et al., 2007)The nominal shear strength V n is evaluated accor<strong>di</strong>ng to (Sezen andMoehle, 2004), see Section 2.3, while parameter k is defined to be equal to 1.00for <strong>di</strong>splacement ductility less than 2, to be equal to 0.60 for <strong>di</strong>splacementductility excee<strong>di</strong>ng 6 (more conservative compared to the original assumption<strong>of</strong> 0.70), and to vary linearly for interme<strong>di</strong>ate <strong>di</strong>splacement ductilities.To provide further confidence <strong>of</strong> achieving a flexural failure, Con<strong>di</strong>tion i islimited to columns with a transverse reinforcement ratiothan 0.002, and a spacing-to-depth ratio lower than 0.5."ρ = Av/ bwsgreaterFor Vp /(Vn/ k) ≤ 0. 60 , the Con<strong>di</strong>tion is adjusted from i to ii for columnswith 90 degree hooks or lap-spliced transverse reinforcement. For1.00≥ Vp /(Vn/ k) >0.60 , the Con<strong>di</strong>tion is adjusted from ii to iii only for lapspicedtransverse reinforcement.Moreover, another Con<strong>di</strong>tion is considered (Con<strong>di</strong>tion iv): “failurecontrolled by inadequate development or splicing”, assuming that this failuremode takes place when the calculated steel stress at the splice exceeds the steelstress specified by equation:f2/3⎛ lb⎞s = 1.25⎜ f y(2.2.1.21)ld⎝⎟ ⎟ ⎠


68 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>where f s is the maximum stress that can be developed in the bar for the straightdevelopment, hook, or lap-splice length l b provided, f y the nominal yieldstrength <strong>of</strong> reinforcement and l d the length required by ACI 318 (2005).In particular, accor<strong>di</strong>ng to ACI 318, the development length for deformedbars in tension terminating in a standard hook (l dh ) is determined from thefollowing expression:ldh0.02ψefy= 0.80 db(2.2.1.22)λ fcwhereψ e and λ are taken as 1.0 while 0.80 is the mo<strong>di</strong>fication factor due to thepresence <strong>of</strong> 180 degree hooks. For smooth straight bars, hooked bars, and lapsplicedbars, development and splice lengths is taken as twice the valuesdetermined in accordance with ACI 318.Based on these prescriptions, a Con<strong>di</strong>tion is identified for the column andcorrespon<strong>di</strong>ng values <strong>of</strong> capacity parameters a and b (see Figure 2.2.1.1) areprovided, depen<strong>di</strong>ng on <strong>di</strong>fferent parameters:P− , where P is the axial load level, transverse reinforcementA f '−−gcratio, A g is the gross cross-sectional area and f’ c is the concretecompressive strength;Avρ " = , where A v is the area <strong>of</strong> transverse reinforcement in theb sw<strong>di</strong>rection <strong>of</strong> applied shear, b w is the width <strong>of</strong> the columnperpen<strong>di</strong>cular to the applied shear and s is the spacing <strong>of</strong> thetransverse reinforcement;Vν = , where V is the shear demand and d is the effective depth.b dwAs an example, see Figure 2.2.1.2, where parameters a and b for Con<strong>di</strong>tion iproposed by (Elwood et al., 2007) are reported and compared with the previousFEMA 356 prescription. For Con<strong>di</strong>tions iii and iv, parameter a is set equal to 0.


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 69Figure 2.2.1.1. Generalized force-deformation relations for <strong>RC</strong> elements (ASCE/SEI 41)Figure 2.2.1.2. Comparison between parameters a and b for Con<strong>di</strong>tion i and the previous FEMA356 prescription, for columns with conforming (a) and non-conforming (b) transversereinforcement, accor<strong>di</strong>ng to FEMA 356 definition (Elwood et al., 2007)


70 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>Background theoryFirst <strong>of</strong> all, for the purpose <strong>of</strong> determining a values, it was assumed that thispoint corresponds to the plastic rotation at which the lateral resistance hasdegraded to 80% <strong>of</strong> the measured peak shear force, thus assuming the samedefinition employed in EC8 approach.Hence, target probabilities <strong>of</strong> failure were established based on judgementregar<strong>di</strong>ng the consequence <strong>of</strong> each failure mode. Due to the degradation <strong>of</strong> axialcapacity with the development <strong>of</strong> a shear-failure plane, the a values for columnsthat are expected to fail in flexure-shear or shear (Con<strong>di</strong>tions ii and iii,respectively) were selected to achieve a probability <strong>of</strong> failure less than 15%.Because columns experiencing flexural failures are more likely to be able tomaintain axial loads beyond initial loss <strong>of</strong> lateral strength, the target probability<strong>of</strong> failure was relaxed for flexure-controlled columns (Con<strong>di</strong>tion i), with avalues selected to achieve a probability <strong>of</strong> failure less than 35%.Results from laboratory tests compiled by Berry et al. (2004) – on columnswith ribbed bars – were used to assess the adequacy <strong>of</strong> the proposed modellingparameters and check the probabilities <strong>of</strong> failure assuming a lognormal<strong>di</strong>stribution for the plastic rotation. For Con<strong>di</strong>tions i and ii the failureprobabilities based on the assumed a values resulted equal to 30% (instead <strong>of</strong>35%) and 6% (instead <strong>of</strong> 15%), respectively. However, a high <strong>di</strong>spersion <strong>of</strong> theexperimental-to-pre<strong>di</strong>cted capacity ratio is observed.The decrease in deformation capacity due to the absence <strong>of</strong> seismic detailsis reflected, for instance, in the prescription <strong>of</strong> adjusting the Con<strong>di</strong>tion (from ito ii) for columns with 90 degree hooks characterized by Vp /(Vn/ k) ≤ 0. 60 .If experimental data are not available for the determination <strong>of</strong> deformationcapacity (e.g., columns with lap-spliced transverse reinforcement, characterizedby .00 ≥ V /(V / k) 0. 60 ), Con<strong>di</strong>tion is adjusted (from ii to iii) to achieve a1p n>higher conservatism.When the failure Con<strong>di</strong>tion is determined for columns with smooth barsen<strong>di</strong>ng in standard hooks, the development length is taken as twice the values


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 71determined in accordance with ACI 318. This prescription may lead toclassifying a column as “controlled by inadequate development or splicing”(Con<strong>di</strong>tion iv, a=0) even if the column actually has a deformation capacity intoinelastic field. As a matter <strong>of</strong> fact, an anchorage detail <strong>of</strong> a smooth bar – madeup <strong>of</strong> a straight portion <strong>of</strong> bar en<strong>di</strong>ng in a 180 degree hook – can be veryeffective, even allowing the development <strong>of</strong> steel ultimate strength, althoughthe low bond capacities along the straight bar, thank to the load carryingcapacity <strong>of</strong> the hook (Fabbrocino et al., 2005).From this point <strong>of</strong> view, a less conservative but more realistic evaluation <strong>of</strong>the deformation capacity <strong>of</strong> members with smooth bars en<strong>di</strong>ng in standardhooks is provided by EC8 (CEN, 2005).2.2.1.4. Critical reviewThe expressions for the ultimate rotational capacity, as clearly shown in theprevious paragraphs, are necessarily calibrated on experimental data, due to thecomplex nature <strong>of</strong> mechanisms affecting the post-elastic behaviour <strong>of</strong> <strong>RC</strong>members and their interaction.All the approaches presented in literature and in Code are characterized byhigh values <strong>of</strong> the coefficient <strong>of</strong> variation <strong>of</strong> the experimental-to-pre<strong>di</strong>ctedcapacity ratio.The high <strong>di</strong>spersion affecting these models is not only due to the naturalexperimental variability, but also to the <strong>di</strong>fficulty in completely modelling witha simple formulation the interaction between the complex phenomenainfluencing the post-elastic deformation behaviour <strong>of</strong> <strong>RC</strong> element.Panagiotakos and Far<strong>di</strong>s (2001), based on the analysis <strong>of</strong> subgroups <strong>of</strong> tests,homogenous for geometrical and mechanical characteristics and for loa<strong>di</strong>ngcon<strong>di</strong>tions, quantify the CoV associated with the only natural variability in12.5%.The limited pre<strong>di</strong>ction capacity <strong>of</strong> these expressions is also due toimpossibility <strong>of</strong> introducing in the control variables some parameters whichcertainly affect the rotational capacity. The major among these parameters is the


72 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>load path, that is, the energy <strong>di</strong>ssipated in hysteretic cycles. This aspect hasbeen experimentally investigated by (Pujol et al., 2006), who analyzed theinfluence <strong>of</strong> <strong>di</strong>splacement history on the decay <strong>of</strong> element resistance capacity.The experimental tests show that, given equal the geometrical and mechanicalcharacteristics and the applied axial load (that is, all the input parameters <strong>of</strong>code and literature regression formulations), it is possible to predetermine thevalue <strong>of</strong> element chord rotation correspon<strong>di</strong>ng to a conventional drop <strong>of</strong> 20% <strong>of</strong>peak resistance, by imposing a given load path (see Figure 2.2.1.3).Panagiotakos and Far<strong>di</strong>s, in the above mentioned work, try to explicitlyaccount for the effect <strong>of</strong> cyclic loa<strong>di</strong>ng by another regression, where the type <strong>of</strong>loa<strong>di</strong>ng is evaluated with a variable expressing the equivalent number <strong>of</strong>inelastic imposed cycles ( ∑| θ i | θ u ), instead <strong>of</strong> the coefficient ( α cyc ).Nevertheless, contrary to expectations, the inclusion <strong>of</strong> this parameter makesworse the pre<strong>di</strong>ction capacity <strong>of</strong> the formulation. The CoV <strong>of</strong> the ratio betweenthe experimental and the pre<strong>di</strong>cted value, in fact, increases up to 51%. On theother hand, the usual structural modelling approaches do not allow to introducethe <strong>di</strong>ssipated energy in the control variables.A critical analysis <strong>of</strong> expressions (2.3.4.19) and (2.3.4.20), based onmechanical considerations regar<strong>di</strong>ng the absence <strong>of</strong> a <strong>di</strong>rect relationshipbetween the me<strong>di</strong>an estimation <strong>of</strong> the ultimate rotation and some parametersthat certainly influence the member capacity, seems to be without foundation.Due to the purely statistical nature <strong>of</strong> the expression, in fact, the retaining <strong>of</strong>these variables turns out to be not significant because <strong>of</strong> their strong correlationwith other parameters, already present in the formulation (Panagiotakos et al.,2001).It is worth noting that the higher coefficient <strong>of</strong> variation affecting the hybridmechanical-empirical formulation (plastic hinge length) with respect to thepurely empirical one is probably related to the <strong>di</strong>fficulty in expressing theultimate rotation as a function <strong>of</strong> element characteristics based on a statisticalregression analysis restrained to a mechanical relationship.


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 73Figure 2.2.1.3. Influence <strong>of</strong> <strong>di</strong>splacement history on ultimate chord rotation (Pujol et al., 2006)


74 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>2.2.2. A proposal for a new correction coefficient applied to the EC8capacity formulation for <strong>RC</strong> columns with smooth barsSmooth reinforcing bars have been widely used in the construction <strong>of</strong>European <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>. In Italy and in the whole Me<strong>di</strong>terranean area their usewas widely spread up to 1970s, in north-American countries and in NewZealand constructions with smooth bars are present until 1950. The widesprea<strong>di</strong>ng <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with smooth bars among <strong>existing</strong> <strong>buil<strong>di</strong>ngs</strong> can bededuced if it is considered that 50% <strong>of</strong> Italian <strong>existing</strong> <strong>buil<strong>di</strong>ngs</strong> has beenconstructed between earliest 1940s and latest 1970s, when <strong>RC</strong> structures withsmooth bars were the prevailing construction typology.The correct evaluation <strong>of</strong> deformation capacity <strong>of</strong> <strong>RC</strong> elements has toaccount for the effective bond capacities between reinforcing bars and thesurroun<strong>di</strong>ng concrete; for members with smooth bars, low bond capacities<strong>di</strong>rectly influence the three main deformation mechanisms: ben<strong>di</strong>ng, shear andfixed-end rotation.As shown by experimental evidence, the scarce capacities <strong>of</strong> load transferbetween the reinforcing bars and the surroun<strong>di</strong>ng concrete (see Section 2.2.3)makes the deformation contribution associated with the fixed-end rotationeffect very important (see Section 2.2.5). This contribution, in fact, due to thecyclic and post-elastic decay <strong>of</strong> bond capacities, may represent up to (80-90)%<strong>of</strong> overall deformability <strong>of</strong> the element (Verderame et al., 2008a,b).Bond capacities also influence the development <strong>of</strong> cracks along the element.A lower number <strong>of</strong> wider cracks is observed when bond decreases. This greatlyinfluences both shear and ben<strong>di</strong>ng deformability, reducing the former an<strong>di</strong>ncreasing the latter.Therefore, formulations able to provide a reliable assessment <strong>of</strong> ultimatedeformation capacity <strong>of</strong> elements with smooth bars are <strong>of</strong> a particular interestfor assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>.In this Section, referring to the purely empirical formulation proposed in(CEN, 2005), the applicability <strong>of</strong> this formulation to non-conforming elementswith smooth bars is evaluated. In particular, experimental data for the


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 75assessment <strong>of</strong> deformation capacity <strong>of</strong> <strong>RC</strong> elements with smooth bars arepresented in Section 2.3.4.2. Based on these data, in Section 2.3.4.3 correctioncoefficients applied to the EC8 empirical formulation for elements with smoothbars, with or without lapping <strong>of</strong> longitu<strong>di</strong>nal reinforcement, are proposed.2.2.2.1. Deformation capacity <strong>of</strong> <strong>RC</strong> columns with smooth barsThe ultimate rotational capacities for columns with smooth bars, accor<strong>di</strong>ngto the European code (CEN, 2005), as already shown at Section 2.2.1.1, isevaluated by applying a correction coefficient, based on experimental data, tothe capacity formulations calibrated on members with ribbed bars andseismically detailed.Most <strong>of</strong> literature data about the experimental behaviour <strong>of</strong> <strong>RC</strong> elementscomes from test executed on members with ribbed bars. During last years, theneed for a reliable assessment <strong>of</strong> seismic capacity <strong>of</strong> <strong>existing</strong> structures hasproduced an increasing number <strong>of</strong> experimental campaigns aimed at the study<strong>of</strong> behaviour <strong>of</strong> non-conforming elements.In Table 2.2.2.1, experimental results <strong>of</strong> columns with smooth bars (Bousiaset al., 2005; Far<strong>di</strong>s et al., 2006; Faella et al., 2008; Verderame et al., 2008b),inclu<strong>di</strong>ng recent tests (Di Ludovico et al., 2010) carried out in the laboratory <strong>of</strong>the Department <strong>of</strong> Structural Engineering at the University <strong>of</strong> Naples FedericoII, in the research project ReLUIS-DPC 2005-2008 Linea 2, are reported.Based on these data, it will be possible to extend the experimental databasefor the calibration <strong>of</strong> correction coefficients applied to the regressionrelationships for the evaluation <strong>of</strong> ultimate rotational capacity <strong>of</strong> members withsmooth bars.Tested columns with lapping <strong>of</strong> longitu<strong>di</strong>nal reinforcement are included inthis database only if hooks are provided at the end <strong>of</strong> lapped bars. Literature<strong>of</strong>fers experimental data on members without this anchorage detail (Ilki et al.,2004; Yalcin et al., 2008); in these cases, brittle lap splice failures are present.Therefore, in the following these data will not be considered.


76 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>n test Reference loa<strong>di</strong>ng l o /d bL θ u,exp /θ u1 cyclic 15 0.332 cyclic 15 0.623 cyclic 25 0.39Bousias et al., 20054 cyclic 25 0.415 cyclic 100 0.586cyclic 100 0.607 cyclic 100 0.548 cyclic 100 0.74Far<strong>di</strong>s et al., 20069 cyclic 100 0.8310cyclic 100 1.2511 cyclic 43 0.7712 Faella et al., 2008 cyclic 43 0.7913cyclic 43 0.8514 cyclic 40 1.2615 cyclic 40 0.8316 cyclic 40 0.60Verderame et al., 2008b17 cyclic 100 1.2118 cyclic 100 1.1319cyclic 100 0.8120 cyclic 100 1.4121 Di Ludovico et al., 2010 cyclic 100 1.4222cyclic 100 1.76Table 2.2.2.1. Ratios between experimental ultimate rotations and correspon<strong>di</strong>ng theoreticalvalues2.2.2.2. Calibration <strong>of</strong> correction factorThe correction coefficient applied to EC8 expressions for the ultimaterotation <strong>of</strong> members with smooth bars is calibrated, based on experimental datareported in Table 2.2.2.1. The correction coefficient will be calibratedaccor<strong>di</strong>ng to the methodology already illustrated at 2.2.1.1, with regard to thefollowing expression:uypluθ = θ + θ(2.2.2.1)whereplθ u is evaluated accor<strong>di</strong>ng to Eq. (2.2.1.2), with γel=1.The considered database is made up only <strong>of</strong> cyclic tests. As a matter <strong>of</strong> fact,ultimate rotational capacity given by code prescriptions (CEN, 2005) is meantto be cyclic. Monotonic tests could be included in the database for the


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 77calibration <strong>of</strong> correction coefficient only by means <strong>of</strong> a coefficient accountingfor the type <strong>of</strong> loa<strong>di</strong>ng, asαcyc, applied to the expression <strong>of</strong> the ultimaterotation. On the other hand, this would be the same as postulating that thereduction in rotational capacity due to cyclic loa<strong>di</strong>ng, evaluated by thiscoefficient, is, on average, not depen<strong>di</strong>ng on bond capacities. As a matter <strong>of</strong>fact, this coefficient, as previously illustrated, is calibrated on a database madeup <strong>of</strong> members with ribbed bars; therefore, the evaluation <strong>of</strong> the correctioncoefficient should be executed supposing that the reduction given byαcyccanalso be extended to members with smooth bars.Nevertheless, first experimental results highlight that the reduction in rotationalcapacity due to cyclic loa<strong>di</strong>ng is lower for columns with smooth bars comparedto columns with ribbed bars; this is shown, in particular, by test results from theUniversity <strong>of</strong> Naples (Verderame et al., 2008a,b; Di Ludovico et al., 2010).Figure 2.2.2.1 reports the ratio θ / θ ) between cyclic and monotonic( u,cycu, monexperimental ultimate rotations for each possible couple <strong>of</strong> tests, given equalthe axial load level, the longitu<strong>di</strong>nal reinforcement detail (with or withoutlapping) and the geometrical and mechanical characteristics <strong>of</strong> the elements,versus the axial load level ν . The reduction in cyclic rotational capacity clearlyincreases as the axial load level increases.1.00.80.60.4(θ u,cyc / θ u,mon )0.69 smooth bars0.57 ribbed bars(Far<strong>di</strong>s, 2007 )0.2smooth barsribbed barsnormalized axial load, ν0.00.00 0.05 0.10 0.15 0.20 0.25 0.30Figure 2.2.2.1. Ratio between cyclic and monotonic rotational capacities versus the axial loadlevel from Verderame et al. (2008a,b) and Di Ludovico et al. (2010)


78 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>However, the ratio θ / θ ) has a mean equal to 0.69 with a CoV=0.17( u,cycu, monfor columns with smooth bars, independently <strong>of</strong> the axial load level and thelongitu<strong>di</strong>nal reinforcement detail. On the contrary, the average value <strong>of</strong> ratio,for columns with ribbed bars and seismically detailed, is equal to 0.57 asin<strong>di</strong>cated in (Far<strong>di</strong>s, 2007); it is to be noted that this value is confirmed by theonly couple <strong>of</strong> tests characterized by ribbed longitu<strong>di</strong>nal reinforcement.Therefore, due to the uncertainties related to the inclusion <strong>of</strong> monotonic tests,the correction coefficient will now be calibrated based on the only cyclic tests.Table 2.2.2.1 reports the description <strong>of</strong> the database, inclu<strong>di</strong>ng the lap lengthand the ratio between the experimental ultimate rotation and the correspon<strong>di</strong>ngtheoretical value ( θratiou ,exp/ θθ u ,exp / θuversus the lap length o / dbLu), accor<strong>di</strong>ng to (2.2.1.1); Figure 2.2.2.2 shows thel .2.01.81.61.41.21.00.80.60.40.20.0θ u,exp / θ u# 22 testslap length, l o /d bL0 10 20 30 40 50 60 70 80 90 100 110 120Figure 2.2.2.2. Ratio θ exp /θ u versus lap length l o /d bLThe ratio ( θu ,exp/ θu) for members without lapping <strong>of</strong> longitu<strong>di</strong>nal bars(conventionally reported as lo / dbL= 100 ) has mean equal to 1.03 and me<strong>di</strong>anequal to 0.98, with a CoV=0.39. Therefore, based on the experimental tests,


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 79expression (2.2.2.1) shows a very good agreement with the cyclic rotationalcapacity <strong>of</strong> elements with smooth bars without lapping <strong>of</strong> longitu<strong>di</strong>nalreinforcement.The use <strong>of</strong> expression (2.2.2.1) for members with lapping <strong>of</strong> longitu<strong>di</strong>nal barsoverestimates even more the experimental rotational capacity; in fact, the ratio( θ u ,exp / θu) for members with lapping <strong>of</strong> longitu<strong>di</strong>nal bars has mean equal to0.69 and me<strong>di</strong>an equal to 0.69, with a CoV=0.41. With regard to members withlapping <strong>of</strong> longitu<strong>di</strong>nal bars, a linear regression performed on the ratio( θ u ,exp / θu) gives the following expression for the correction coefficient:κ = .020 (l / d )(2.2.2.2)1 0 ⋅ o bLThe ratio has mean equal to 1.07 and me<strong>di</strong>an equal to 0.93, with a CoV=0.38.Based on mean and me<strong>di</strong>an values shown by columns with continuouslongitu<strong>di</strong>nal reinforcement, it is possible to provide one expression for thecorrection coefficient, both for elements with and without lapping <strong>of</strong>longitu<strong>di</strong>nal bars:κ= 0.020 min(50, lo / dbL)(2.2.2.3)The ratio θ u,exp/( κ ⋅ θu) , calculated on all tests in the experimental database,has mean equal to 1.06, me<strong>di</strong>an equal to 0.96 and a CoV=0.38 while formembers without lapping <strong>of</strong> longitu<strong>di</strong>nal bars it has mean equal to 1.03 andme<strong>di</strong>an equal to 0.98, with a CoV=0.39.Figure 2.2.2.3 reports the ratio between the experimental ultimate rotation andthe correspon<strong>di</strong>ng theoretical value ( θu ,expcorrection coefficient given by (2.2.2.3), applied to (2.2.2.1)./ θu), together with the proposed


80 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>2.01.81.61.4θ u,exp / θ u# 22 tests1.21.00.80.60.020·min(50,l o /d bL )0.40.2lap length, l o /d bL0.00 10 20 30 40 50 60 70 80 90 100 110 120Figure 2.2.2.3. Proposed correction factorIt is possible to compare the proposed coefficient, evaluated on 22 tests, withthe coefficient proposed by (Far<strong>di</strong>s, 2006), evaluated on 15 tests, with thecoefficient given by (CEN, 2005), evaluated on 6 tests, and with update to(CEN, 2005) proposed by (CEN, 2009). The correction coefficient suggested in(Far<strong>di</strong>s, 2006) is not far from the proposed coefficient given by (2.2.2.2) formembers with lapping <strong>of</strong> longitu<strong>di</strong>nal reinforcement.On the other hand, the coefficient adopted by (CEN, 2005) shows aconsiderable conservativeness. Accor<strong>di</strong>ng to this prescription, the ultimaterotation <strong>of</strong> members with a lap length equal to l o has to be evaluated based onthe assumption that the ultimate con<strong>di</strong>tion is controlled by the region right afterthe end <strong>of</strong> the lap. Hence, expression (2.2.2.1) should be multiplied byexpression (2.2.1.4). In this coefficient, a further reduction in the ultimaterotation is given by the term ( 1−lo/ LV) , expressing a reduction in the shearspanLVby the lap length ol . Moreover, shear span should be reduced by thelap length also in expressions (2.2.1.2).With regard to members without lapping <strong>of</strong> longitu<strong>di</strong>nal bars, based on theproposed correction coefficient the ultimate rotational capacity <strong>of</strong> members


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 81with smooth bars is equal to that <strong>of</strong> members with ribbed bars and seismicallydetailed. On the contrary, accor<strong>di</strong>ng to the expression proposed in (Far<strong>di</strong>s,2006), the ratio between the former and the latter is equal to 0.75, whilst codeprescriptions (CEN, 2005) suggest 0.575.Expression proposed in (CEN, 2009), as previously noted, is very similar to theexpression given by (Far<strong>di</strong>s, 2006).Figure 2.2.2.4 shows a comparison between <strong>di</strong>fferent correction coefficientsapplied to (2.2.2.1); it is to be noted that the coefficient given by (CEN, 2005)is represented not taking into account the shear span reduction.2.01.81.61.41.21.00.80.60.4θ u,exp / θ u# 22 testsproposed (Eq.23)(CEN, 2005)(CEN, 2009)(Far<strong>di</strong>s, 2006)0.2lap length, l o /d bL0.00 10 20 30 40 50 60 70 80 90 100 110 120Figure 2.2.2.4. Comparison between the proposed correction coefficient and the ones reporte<strong>di</strong>n (CEN, 2005), (Far<strong>di</strong>s, 2006) and (CEN, 2009)2.2.2.3. Discussion <strong>of</strong> resultsThe extension <strong>of</strong> the experimental database allowed to re-calibrate thecorrection coefficients applied to the assessment <strong>of</strong> the ultimate rotationalcapacity <strong>of</strong> elements with smooth bars, with or without lapping <strong>of</strong> longitu<strong>di</strong>nalreinforcement.The expression <strong>of</strong> correction coefficient proposed herein highlights theconservativeness <strong>of</strong> EC8 (CEN, 2005) proposal, which is based on very few


82 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>experimental tests. Moreover, EC8 assumes that, when lapping <strong>of</strong> longitu<strong>di</strong>nalreinforcement is present, the ultimate con<strong>di</strong>tion is controlled by the region rightafter the end <strong>of</strong> the lap, so that the shear span and, therefore, the rotationalcapacity are further reduced. This assumption is not confirmed by theexperimental results reported in (Verderame et al., 2008a,b; Di Ludovico et al.,2010); the highest plastic demand, in fact, always concentrates at the basesection <strong>of</strong> the element.The changes in correction coefficients proposed by (CEN, 2009) – probablybased on the proposal <strong>of</strong> (Far<strong>di</strong>s, 2006) – result in a less conservative and morereliable evaluation <strong>of</strong> ultimate deformation capacity <strong>of</strong> members with smoothbars.Despite the <strong>di</strong>fficulties in the choice <strong>of</strong> the most reliable expression for thecorrection coefficient, recent experimental results (Di Ludovico et al., 2010)clearly highlight the higher rotational capacity <strong>of</strong> members with smooth barswith compared to members with ribbed bars, equal for structural characteristicsand details. As a matter <strong>of</strong> fact, the comparison between the ultimate rotations<strong>of</strong> the elements highlights that the capacity <strong>of</strong> members with smooth bars arehigher, on average, by 35% compared with the correspon<strong>di</strong>ng members withribbed bars.From a mechanical standpoint, the higher ultimate rotational capacity <strong>of</strong>columns with smooth bars may be explained by the comparison between twoopposite mechanisms: the increase in deformability caused by the fixed-endrotation mechanism, particularly exalted due to the low bond capacities; on theother hand, the higher degradation <strong>of</strong> global resistance due to the increase indeformation demand on concrete in compression, localized at the base <strong>of</strong> theelement and associated with the concentrated rotation (rocking effect).Accor<strong>di</strong>ng to experimental evidence, the former seems to prevail on the latter,lea<strong>di</strong>ng to an overall increase <strong>of</strong> ultimate rotational capacity compared withmembers with higher bond capacities.However, it is to be noted that the stirrup spacing in critical region (orbetter, the ratio between stirrup spacing and longitu<strong>di</strong>nal bars <strong>di</strong>ameter) can


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 83highly influence the deformation capacity through the buckling phenomenon.(see Section 2.2.4) This issue can be highlighted, for instance, observing the<strong>di</strong>fferences in ultimate rotation capacity between University <strong>of</strong> Naples databaseand Bousias database.Furthermore, the post-elastic development <strong>of</strong> a high slippage, concentrate<strong>di</strong>n a low number <strong>of</strong> wide cracks, represents not only a source <strong>of</strong> deformabilitybut also a permanent damage for the <strong>RC</strong> element (Verderame et al., 2008b).Moreover, the higher influence <strong>of</strong> fixed-end rotation mechanism on behaviour<strong>of</strong> elements with smooth bars, compared to elements with ribbed bars, alsoleads to a decrease in the energy <strong>di</strong>ssipation capacity. As a matter <strong>of</strong> fact, <strong>RC</strong>members with smooth bars tested under cyclic loa<strong>di</strong>ng reported in (Di Ludovicoet al., 2010), at the same <strong>di</strong>splacement demand, show a <strong>di</strong>ssipated energy about30% lower, on average, than the energy <strong>di</strong>ssipated by the correspon<strong>di</strong>ngmembers with ribbed bars, equal for geometrical characteristics and appliedaxial load. This issue should be carefully considered since it could potentiallylead to an underestimate <strong>of</strong> the seismic demand.Further conservatism should be addressed to the assessment <strong>of</strong> seismiccapacity <strong>of</strong> members with smooth bars because <strong>of</strong> the particularly highuncertainties involved in modelling their deformation mechanisms. This is due,for example, to the <strong>di</strong>fficulties in evaluating the influence <strong>of</strong> rocking effect andto the high variability affecting bond capacities (Verderame et al., 2009a,b),also influenced by possible corrosion (Fang et al., 2006).Finally, the absence <strong>of</strong> an effective anchorage <strong>of</strong> reinforcing bars by means<strong>of</strong> end hooks may limit the deformation capacity (Yalcin et al., 2008) and insome cases the strength (Ilki et al., 2004) <strong>of</strong> the element.


84 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>2.2.3. Bond behaviour <strong>of</strong> smooth bars: experimental and analyticalinvestigationThe development <strong>of</strong> bond stresses between smooth bars and concrete can beexplained by <strong>di</strong>fferent mechanisms: for low values <strong>of</strong> slip, chemical adhesionand micro-interlocking are present, subsequently a purely frictional mechanismis activated.In this Section, results form experimental tests (see Figure 2.2.3.1, Table2.2.3.1) carried out in the laboratory <strong>of</strong> the Department <strong>of</strong> StructuralEngineering (DIST) at the University <strong>of</strong> Naples Federico II are reported. Theresults reported herein were published in (Verderame et al., 2009a). Monotonicand cyclic pullout tests were carried out; in the latter case, <strong>di</strong>fferent values <strong>of</strong>maximum imposed <strong>di</strong>splacements were adopted in order to evaluate theinfluence <strong>of</strong> slip amplitude on the mechanisms <strong>of</strong> bond deterioration. Also, apull-out test was carried out characterized by five cycles for each <strong>of</strong> the targetvalues <strong>of</strong> the slip previously considered.reinforcing barφ=12 mmplastic pipe235 mmL b = 120mm500 mmspecimen30 235 mm(a)Figure 2.2.3.1. Geometry <strong>of</strong> the pull-out specimen (a), test setup (b) (Verderame et al., 2009a)(b)


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 85Specimen Loa<strong>di</strong>ng type Imposed <strong>di</strong>splacement [mm] n° <strong>of</strong> cycles n° <strong>of</strong> testsM_01M_02monotonic - - 2C_0.5_01C_0.5_02cyclic ± 0.5 5 2C_2.0_01C_2.0_02cyclic ± 2.0 5 2C_4.0_01C_4.0_02cyclic ± 4.0 5 2C_8.0_01C_8.0_02cyclic ± 8.0 5 2C_01 cyclic ± 0.5 - ± 2.0± 4.0 - ± 8.0 5 + 5 + 5 +5 1Table 2.2.3.1. Experimental program (Verderame et al., 2009a)Results from pull-out tests show, in monotonic field, a first ascen<strong>di</strong>ng branchwhich in correspondence with very low values <strong>of</strong> the relative slippage reachesmaximum values <strong>of</strong> the bond resistance. With the increase in slippage the bondstrength reduces and tends towards the value <strong>of</strong> minimum friction contribution.The value <strong>of</strong> the friction bond resistance should remain constant or slightlydecrease as the slippage increases. The parameters characterizing the monotonicenvelope <strong>of</strong> the experimental bond–slip relationship are the bond stress and slipat the peak con<strong>di</strong>tion (τ b,max , s max ) and the value <strong>of</strong> minimum frictional bondstress (τ b,f ) (see Figure 2.2.3.2).τ b bond stress [MPa]τb,fτb,maxs maxslip [mm]Figure 2.2.3.2. Characteristic parameters <strong>of</strong> experimental monotonic bond-slip relationship(Verderame et al., 2009a)


86 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>In spite <strong>of</strong> their high variability, values <strong>of</strong> these parameters, in averageterms, seem to reflect well the literature in<strong>di</strong>cations about bond performances <strong>of</strong>plain bars (see Table 2.2.3.2).τ b,max s maxτ b, f/ ττ b,max/ fcτ b,f/ fcb ,f b, maxSpecimen[MPa] [mm] [MPa]M_01 1.64 0.34 0.68 0.41 0.17 0.41M_02 1.58 0.15 0.61 0.40 0.15 0.39C_0.5_01 2.15 0.15 - 0.54 - -C_0.5_02 1.15 0.12 - 0.29 - -C_2.0_01 1.50 0.20 - 0.38 - -C_2.0_02 1.03 0.22 - 0.26 - -C_4.0_01 1.15 0.17 0.49 0.29 0.12 0.43C_4.0_02 0.83 0.14 0.30 0.21 0.08 0.36C_8.0_01 0.61 0.07 0.25 0.15 0.06 0.41C_8.0_02 0.75 0.10 0.43 0.19 0.11 0.57Mean 1.24 0.17 0.46 0.31 0.12 0.43CoV 0.38 0.45 0.37 0.38 0.37 0.18Table 2.2.3.2. Characteristic parameters <strong>of</strong> experimental monotonic bond-slip relationship(Verderame et al., 2009a)τIn cyclic field, experimental results show a significant degradation <strong>of</strong> bondcapacities. Shape <strong>of</strong> hysteretic cycles is characterized by a reloa<strong>di</strong>ng phase, bothin positive and negative field, showing a slight reduction for slip valuesapproaching zero and a subsequent increase in bond stress towards themaximum imposed slip. It is possible to describe this trend by means <strong>of</strong> threecharacteristic parameters: bond values correspon<strong>di</strong>ng to the initial, the me<strong>di</strong>um(that is, zero-slip con<strong>di</strong>tion) and the final point <strong>of</strong> each semi-cycle. Theseparameters show a high variability, represented both by the absence <strong>of</strong>symmetry between positive and negative semi-cycles, in the same test, and bythe variability <strong>of</strong> these values between <strong>di</strong>fferent tests. However, it is generallypossible to recognize a decreasing trend <strong>of</strong> bond stresses both with the number<strong>of</strong> cycles and with the maximum imposed slip.Example results from a cyclic test, together with the schematisation <strong>of</strong> the


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 87typical hysteretic behaviour, are reported in Figure 2.2.3.3.τ b bond stress1.5Pull-out testC_2.0_02τ b bond stress [MPa]first inversion <strong>of</strong> slip1.0τ b,un0.5τ b,rel + (1)τ b,rel + (n)τ b,un - (n)τ b,un - (1)τ b,o + (1)τ b,o + (n)τ b,o - (n)τ b,o - (1)τ b,un + (1)τ + b,un (n)slipτ b,rel - (n)τ b,rel - (1)0.0-0.5slip [mm]-1.0-4 -3 -2 -1 0 1 2 3 4(a)(b)Figure 2.2.3.3. Schematisation <strong>of</strong> the bond-slip relationship <strong>of</strong> the bonded bar subjected tocyclic load (a), characteristic parameters <strong>of</strong> cyclic bond-slip relationship (b) (Verderame et al.,2009a)Based on these experimental results, a bond stress-slip relationship forsmooth bars is proposed, both in monotonic and cyclic field, which waspublished in (Verderame et al., 2009b).The monotonic envelope presents a first ascen<strong>di</strong>ng branch up to a peakstrength value correspon<strong>di</strong>ng to very low values <strong>of</strong> slippage; during this phase,chemical-physical adhesion, mechanical microinterlocking and also the frictioncomponent contribute to the bond strength. Then, a s<strong>of</strong>tening branch related tothe progressive degradation <strong>of</strong> friction mechanism is present; finally, ahorizontal branch is present, correspon<strong>di</strong>ng to a constant value equal to theminimum frictional component value <strong>of</strong> bond resistance. The monotonicenvelope <strong>of</strong> the bond-slip relationship has to be defined through theexperimental evaluation <strong>of</strong> five parameters: parameter α, related to the shape <strong>of</strong>the ascen<strong>di</strong>ng branch; the couple <strong>of</strong> values (τ b,max , s max ), correspon<strong>di</strong>ng to thepeak resistance con<strong>di</strong>tion; parameter p, representing the slope <strong>of</strong> the s<strong>of</strong>teningbranch expressed as a quote <strong>of</strong> the secant stiffness (τ b,max /s max ); and the


88 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>frictional bond strength value τ b,f . The proposed cyclic model is defined throughtwo parameters: cyclic (τ b,c ) and residual (τ b,r ) bond stresses. Under cyclicexcitations the bond stress τ b,c is assumed to be constant and equal to the 35%<strong>of</strong> the monotonic frictional bond resistance, independent <strong>of</strong> the number and themagnitude <strong>of</strong> the cycles. Then, in correspondence with values <strong>of</strong> slip higherthan the maximum one previously attained, τ-slip curve does not reach themonotonic envelope curve, but a reduced value τ b,r , equal to the 68% <strong>of</strong> themonotonic frictional bond resistance. All the characteristic parameters <strong>of</strong> theconstitutive bond-slip relationship are then expressed proportionally to thesquare root <strong>of</strong> the cylindrical compressive strength <strong>of</strong> concrete (see Figure2.2.3.4).τb,maxτ= 0. 31⋅f= 0. 13⋅fb, f ccτ b,maxτ ḇτ b,maxτ b,fτ b,cτ b,rslip- τ b,c-τ b,r-τ b,fττb,rb,c= 0. 09 ⋅ f= 0. 05⋅fccFigure 2.2.3.4. Summary <strong>of</strong> model parameters. (Verderame et al., 2009b)


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 892.2.4. The influence <strong>of</strong> transverse reinforcement anchorage detail onconfined concrete behaviourThe absence <strong>of</strong> a proper anchorage detail in transverse reinforcement canlead to a limitation <strong>of</strong> confinement effect on concrete, thus lea<strong>di</strong>ng to a lowermaterial ductility and, finally, to a lower element ductility. This issue wasexperimentally investigated (Cosenza et al., 2009): monotonic experimentaltests were carried out on column elements (250x250x800 mm) with smoothbars, both for longitu<strong>di</strong>nal and transverse reinforcement. 4φ12 longitu<strong>di</strong>nal barswere present. The transverse reinforcement (8 mm <strong>di</strong>ameter stirrups) wascharacterized by <strong>di</strong>fferent anchorage details, that is, 135 degree hooks (incompliance with modern seismic detailing prescriptions) and 90 degree hooks(reflecting design and constructive practice <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>). Three<strong>di</strong>fferent stirrup spacing values were considered: 100, 200 and 300 mm (seeFigure 2.2.4.1). Steel yield strength was equal to f y =335 MPa and f yw =430 MPafor longitu<strong>di</strong>nal and transverse reinforcement, respectively. Compressivestrength <strong>of</strong> unconfined concrete was equal to f co =27.8 MPa, evaluated on 0-0-#1 Specimen (with no reinforcement). A summary <strong>of</strong> experimental results isshown in Figure 2.2.4.2.Experimental tests highlighted that:- concrete compressive strength increases with the volumetric ratio <strong>of</strong>transverse reinforcement, with no significant influence <strong>of</strong> anchoragedetail;- post-peak s<strong>of</strong>tening response is strongly influenced by buckling <strong>of</strong>longitu<strong>di</strong>nal reinforcement, which in turn is influenced by stirrupspacing (higher the stirrup spacing, earlier this phenomenon takesplace);- progressive opening and loss <strong>of</strong> effectiveness <strong>of</strong> 90 degree anchoragedetail is registered together with the buckling <strong>of</strong> longitu<strong>di</strong>nalreinforcement (see Figure 2.2.4.3);- nevertheless, no significant influence <strong>of</strong> anchorage detail is clearlyshown, neither on post-peak s<strong>of</strong>tening response.


90 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>Longitu<strong>di</strong>nalreinforcementTransversereinforcementSpecimenAnchorage VolumetricA s f y A sw Spacingdetail ratio ρ w[mm 2 ] [MPa] [mm 2 ] [mm] [-] [%]0-0-#1 - - - - - -300-135-#1 452 355 50 300 135° 0.2667300-135-#2 452 355 50 300 135° 0.2667300-135-#3 452 355 50 300 135° 0.2667300-90-#1 452 355 50 300 90° 0.2667300-90-#2 452 355 50 300 90° 0.2667300-90-#3 452 355 50 300 90° 0.2667200-135-#1 452 355 50 200 135° 0.4000200-135-#2 452 355 50 200 135° 0.4000200-135-#3 452 355 50 200 135° 0.4000200-90-#1 452 355 50 200 90° 0.4000200-90-#2 452 355 50 200 90° 0.4000200-90-#3 452 355 50 200 90° 0.4000100-135-#1 452 355 50 100 135° 0.8000100-135-#2 452 355 50 100 135° 0.8000100-135-#3 452 355 50 100 135° 0.8000100-90-#1 452 355 50 100 90° 0.8000100-90-#2 452 355 50 100 90° 0.8000100-90-#3 452 355 50 100 90° 0.8000φ8@300 φ8@200 φ8@100 φ8@300 φ8@200 φ8@100135 degree hooks 90 degree hooksFigure 2.2.4.1. Experimental program (Cosenza et al., 2009)


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 91(a) (b) (c)Figure 2.2.4.2. Summary <strong>of</strong> experimental results for stirrup spacing equal to 100 (a), 200 (b)and 300 (c) mm (Cosenza et al., 2009)100-90° 200-90° 300-90°Figure 2.2.4.3. Evidence <strong>of</strong> longitu<strong>di</strong>nal bar buckling and opening <strong>of</strong> 90 degree anchoragehooks (Cosenza et al., 2009)


92 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>2.2.5. Numerical modelling <strong>of</strong> <strong>RC</strong> members with smooth barsA numerical investigation <strong>of</strong> the deformation mechanism <strong>of</strong> columns withsmooth bars is carried out (Verderame et al., 2008c) through a two-componentmonotonic and cyclic model implemented in FORTRAN®, where (i) theflexural <strong>di</strong>splacement (∆ flex ) is evaluated by means <strong>of</strong> a <strong>di</strong>stributed plasticityfiber model and (ii) the fixed-end rotation contribution (θ base ) is evaluated as therotation given by the slip <strong>of</strong> the anchored bars (see Figure 2.2.5.1). At eachstep, the total lateral <strong>di</strong>splacement is given by ∆ tot =∆ flex +θ base·L, where L is thecolumn height.concreteφ (curvature)steels 1 s 2d-d’θ baseσ 1 σ 2s 1 θ bases 2Figure 2.2.5.1. Two-component column model: flexural <strong>di</strong>splacement is given by a <strong>di</strong>stributedplasticity fiber model, fixed-end rotation is evaluated as depen<strong>di</strong>ng on bar slip from anchorageA typical anchorage detail for smooth bars was represented by a straightportion <strong>of</strong> bar en<strong>di</strong>ng with a 180 degree circular hook. When a strain (that is, astress) value is imposed at the end <strong>of</strong> the hooked bar, a correspon<strong>di</strong>ng slippage<strong>of</strong> reinforcement takes place, given both by the deformability contribution <strong>of</strong>


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 93the straight bar (strongly dependent on bond capacities, both in elastic and inpost-elastic field) and by the concentrated deformability contribution due to theslip <strong>of</strong> the end anchorage detail (hook) (Fabbrocino et al., 2004; Fabbrocino etal., 2005) (see Figure 2.2.5.2a).slip1σ1=f(εs1)θbaseσ2=f(εs2)slip2(a)(b)Figure 2.2.5.2. Two-component model <strong>of</strong> a hooked smooth bar (Fabbrocino et al., 2004) (a);Evaluation <strong>of</strong> fixed-end rotation θ base as a function <strong>of</strong> slip from anchored bars (b)The onset <strong>of</strong> this slippage in longitu<strong>di</strong>nal reinforcement, in correspondencewith the end section <strong>of</strong> the element, leads to the effect <strong>of</strong> deformability increaseknown as “fixed-end rotation”. In order to evaluate this contribution, theanchorage detail is modelled through a two-component finite <strong>di</strong>fference model,where both contributions are taken into account. To this end, hysteretic modelsrepresenting the bond-slip relationship and the steel stress-strain relationshipare needed for the straight bonded bar, together with another hysteretic modelprovi<strong>di</strong>ng the hook as a function <strong>of</strong> the correspon<strong>di</strong>ng stress. Hence, at eachstep, the steel strain values in top and bottom longitu<strong>di</strong>nal reinforcement layers– at the end section <strong>of</strong> the element – are imposed as a boundary con<strong>di</strong>tion forthe models representing the anchorage details. The resulting slip values lead toa rigid rotation at the end <strong>of</strong> the element (see Figure 2.2.5.2b).


94 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>For the hysteretic rules <strong>of</strong> the bond-slip relationship, see Section 2.2.3. Thebond capacities in post-elastic field are based on original and literature(Fabbrocino et al., 2004) experimental stu<strong>di</strong>es.Numerical results show a good agreement with experimental data, both inglobal (overall deformability, pinching effect) and local (base rotation) terms, inmonotonic and cyclic field (see Figures 2.2.5.3 to 5), thus confirming the keyrole played by fixed-end rotation mechanism in determining the deformability<strong>of</strong> <strong>RC</strong> members with smooth bars.force [kN]5045403530252015105experimentalnumerical w/o fixed-end rotationnumerical w/ fixed-end rotation00 20 40 60 80 100 120 140 160 180<strong>di</strong>splacement [mm]Figure 2.2.5.3. Comparison between numerical and experimental (M270-B1 and M270-B2 testsfrom (Verderame et al. 2008a)) monotonic force-<strong>di</strong>splacement relationships, with or withoutconsidering fixed-end rotation contribution


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 95force [kN]50403020100-10-20-30-40-50experimentalnumerical w/o fixed-end rotationnumerical w/ fixed-end rotation120100806040200-20-40-60-80-100-120<strong>di</strong>splacement [mm]Figure 2.2.5.4. Comparison between numerical and experimental (C270-A1 test from(Verderame et al. 2008b)) cyclic force-<strong>di</strong>splacement relationships, with or without consideringfixed-end rotation contributionw exp ,s num [mm]161412108642experimentalnumerical0-2-100 -80 -60 -40 -20 0 20 40 60 80 100<strong>di</strong>splacement [mm]Figure 2.2.5.5. Comparison between the numerical slip values at the end section <strong>of</strong> the elementand the correspon<strong>di</strong>ng experimental crack width values (C270-A1 test from (Verderame et al.2008b))


96 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>2.3 MEMBERS CONTROLLED BY SHEARIn this Section, main truss models for the evaluation <strong>of</strong> shear strength <strong>of</strong> <strong>RC</strong>members are presented.Capacity models for shear strength <strong>of</strong> <strong>RC</strong> members account for <strong>di</strong>fferentcontributions, correspon<strong>di</strong>ng to <strong>di</strong>fferent post-cracking resistance mechanisms:first, the primary contribution (V s ) given by web reinforcement in tension,accor<strong>di</strong>ng to the truss analogy; then, resistance mechanisms developed inconcrete (V c ) are considered, such as dowel action or frictional interlockingbetween cracked interfaces. A <strong>di</strong>stinction can be made between the models thatinclude the contribution <strong>of</strong> axial compression to shear strength in V c and themodels that consider this contribution as a <strong>di</strong>stinct term (V P ).Moreover, capacity models have to take into account the degradation <strong>of</strong>shear strength in members subjected to cyclic inelastic <strong>di</strong>splacement; thisdegradation is usually expressed as a function <strong>of</strong> the maximum ductilitydemand. Hence, assuming V R as shear strength and V flex as flexural strength,V R decreases with the ductility demand increasing. If V R,i is the initial shearstrength (for zero ductility demand) and V R,r is the residual shear strength (thatis, the shear strength correspon<strong>di</strong>ng to the maximum degradation due toductility demand), three <strong>di</strong>fferent con<strong>di</strong>tions can take place (see Figure 2.3.1):• V flex < V R,r : no shear failure occurs, the element deformationcapacity can entirely develop (ductile behaviour, or behaviourcontrolled by flexure);• V R,r < V flex < V R,i : a shear failure may occur before ductile failurebut after flexural yiel<strong>di</strong>ng (limited ductility behaviour, or behaviourcontrolled by shear-flexure interaction);• V R,i < V flex : a shear failure occurs before flexural yiel<strong>di</strong>ng, no ductilemechanism can develop (brittle behaviour, or behaviour controlledby shear).


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 97Figure 2.3.1. Interaction between shear strength and ductility (Priestley et al., 1994)In (Priestley et al., 1994) an empirical-based model is proposed, where theshear strength is given by three contributions:AwfywD'VR = Vs + Vc + VP = cot 30° + k fc ⋅ 0.8Ag+ P tan α (2.3.1)sThe evaluation <strong>of</strong> V s (where A w is the cross-sectional area <strong>of</strong> transversereinforcement, f yw is the yield strength <strong>of</strong> transverse reinforcement, D’ is the<strong>di</strong>stance between the centrelines <strong>of</strong> transverse reinforcement and s is thespacing <strong>of</strong> transverse reinforcement) is based on a truss mechanism assuming a30 degree angle between the <strong>di</strong>agonal compression struts and the columnlongitu<strong>di</strong>nal axis.In the evaluation <strong>of</strong> V c (where f c is the concrete compressive strength and A g isthe gross cross-sectional area) a coefficient k is applied (see Figure 2.3.2) inorder to account for the degradation <strong>of</strong> concrete resistance mechanisms due tothe inelastic flexural demand.Finally, in V P , which is the shear strength contribution given by axialcompression P, α represents the inclination <strong>of</strong> <strong>di</strong>agonal compression struts (dueto P) with member axis (see Figure 2.3.3).


98 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>Figure 2.3.2. Degradation <strong>of</strong> concrete shear strength with ductility (Priestley et al., 1994)(a)Figure 2.3.3. Shear strength contribution given by axial compression P: α angle is <strong>di</strong>fferent inreversed ben<strong>di</strong>ng (a) and in single ben<strong>di</strong>ng (b) (Priestley et al., 1994)(b)In (Sezen and Moehle, 2004) a model is proposed, based on experimentaldata, for the evaluation <strong>of</strong> shear strength in lightly reinforced concrete columns.Shear strength is given by:A f d ⎛ 0.5 f P ⎞V = V + V = k + k 1+0.8As ⎜ a d 0.5 fcA ⎟⎝g ⎠w yw cR s c gwhere d is the effective depth and a is the shear span.(2.3.2)


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 99The concrete contribution V c is evaluated focusing the attention on <strong>di</strong>agonaltension capacity, and assuming that onset <strong>of</strong> <strong>di</strong>agonal tension cracking takesplace when the nominal principal tension stress acting on the element reachesthe nominal tensile strength (evaluated as0.5 fc). Hence, aspect ratio a/d isalso taken into account since elements with increasing a/d show decreasingshear strength.The authors find out that the tra<strong>di</strong>tional expression for V s (that is, based on theassumption <strong>of</strong> 45 degree inclined compressed struts) provides a good estimation<strong>of</strong> experimental data, given the assumed expression for V c .The degradation factor depen<strong>di</strong>ng on inelastic <strong>di</strong>splacement demand (k) isapplied not only to concrete resistance mechanisms but also to transversereinforcement contribution since, from a phenomenological standpoint,concrete degradation also leads to a decrease in V s contribution through loss <strong>of</strong>anchorage and reduction in bond capacity for transverse reinforcement.The contribution <strong>of</strong> axial compression to shear strength is not taken intoaccount in a <strong>di</strong>stinct term.EC8-part 3 (CEN, 2005) adopts the shear capacity model proposed in(Biskinis et al., 2004), based on a dataset <strong>of</strong> 239 experimental tests. For a/dhigher than 2 (slender elements), shear strength is given by:1V = ⎡V + (1 − 0.05min(5; µ )) ⋅ V + V( )plR P ∆ c sγ ⎣elwith⎤⎦(2.3.3)d − xVP= min(P;0.55Acf c)(2.3.4)2aaVc = 0.16 max(0.5;100 ρtot )(1 − 0.16 min(5; ))Ac f(2.3.5)cdVs = ρw ⋅bw ⋅ z ⋅ fyw(2.3.6)where γ el , equal to 1,15 for primary seismic elements and 1,0 for secondary


100 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>seismic elements, is meant to convert mean values <strong>of</strong> shear strength to meanminus-one-standard-deviationones,plµ∆is the plastic part <strong>of</strong> ductility demand, xis the compression zone depth, ρ tot is the total longitu<strong>di</strong>nal reinforcement ratio,ρ w is the transverse reinforcement ratio, b w is the width <strong>of</strong> the cross section andz is the length <strong>of</strong> the internal lever arm.In this model the contribution <strong>of</strong> axial compression is explicitly taken intoaccount, assuming that the inclination <strong>of</strong> <strong>di</strong>agonal compression struts withmember axis is given by (d-x)/2a.In <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> not designed accor<strong>di</strong>ng to the strength hierarchyconcept, no ratio between shear and flexural strength was established a priori.Hence, the onset <strong>of</strong> a shear failure roughly depends on the ratio between theamount <strong>of</strong> longitu<strong>di</strong>nal reinforcement (provi<strong>di</strong>ng flexural strength) and theamount <strong>of</strong> transverse reinforcement (provi<strong>di</strong>ng shear strength). Higher thisratio, higher the probability that the element exhibit a brittle behaviour. Fromthis point <strong>of</strong> view, a shear failure can be even more likely to occur in a oldseismic designed buil<strong>di</strong>ng rather than in a gravity load designed buil<strong>di</strong>ng sincein the former it is likely to have a much higher amount <strong>of</strong> longitu<strong>di</strong>nalreinforcement compared to the latter, but not a much higher amount <strong>of</strong>transverse reinforcement.This is also due to the so-called “threshold-based” design method fortransverse reinforcement: in old technical codes (e.g., RDL 2229/1939, DIN1045/1959, B4200/1953, ACI 318/1951, CP 114/1958) a value <strong>of</strong> allowabletangential stress was assumed (e.g., τ c0 ) and, if the design stress demand <strong>di</strong>d notexceed this value, only a minimum amount <strong>of</strong> transverse reinforcement wasprescribed, thus lea<strong>di</strong>ng to inadequate shear strength.Moreover, some critical issues may affect the development <strong>of</strong> shear strengthin <strong>existing</strong> buil<strong>di</strong>ng without proper seismic details: for instance, the absence <strong>of</strong>a 135 degree hook anchorage in transverse reinforcement can lead to theopening <strong>of</strong> the stirrups under repeated cyclic loa<strong>di</strong>ng, thus resulting in a halfcutting<strong>of</strong> their contributions to shear strength (Biskinis et al., 2004).


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 101Generally speaking, shear capacity in <strong>RC</strong> members is given by twocontributions, correspon<strong>di</strong>ng to two <strong>di</strong>fferent mechanisms: the truss mechanism(to which are referred the capacity models reported herein) and the tied archmechanism. It is to be noted that in members with smooth bars, characterizedby very low bond capacities (see Section 2.2.3) – and, therefore, also by a lowernumber <strong>of</strong> wider cracks, compared to elements with ribbed bars – thecontribution associated with the tied arch mechanism may become prevalentwith respect to the truss mechanism, see Figure 2.3.4.(a)(b)Figure 2.3.4. Variation <strong>of</strong> internal stress flow accor<strong>di</strong>ng to perfect bond (a) or perfect unbond(b) con<strong>di</strong>tion (Pandey and Mutsuyoshi, 2005)


102 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>2.4 BEAM-COLUMN JOINTSIn a beam-column joint with transverse reinforcement, the shear capacity isgiven by two contributions, respectively correspon<strong>di</strong>ng to strut-mechanism(shear is concentrated in a single <strong>di</strong>agonal compressed concrete strut, see Figure2.4.1b) and truss-mechanism (the shear force due to the bond stress along thelongitu<strong>di</strong>nal steel reinforcement inside the joint is in equilibrium with a trussmechanism given by concrete struts and vertical and horizontal tiescorrespon<strong>di</strong>ng to joint panel reinforcement).Nevertheless, transverse reinforcement in beam-column joint panel area, incompliance with Capacity Design principles, has been prescribed only by recentseismic codes (e.g., Circ. M.LL.PP. 65, 1997, see Section 2.5.2). Hence, in thefollowing only capacity models for beam-column joints without transversereinforcement will be reported, thus referring to the strut-mechanism as the onlypossible resistance mechanism.(a)(b)Figure 2.4.1. Mechanism <strong>of</strong> shear transfer at an interior beam-column joint withoutreinforcement: (a) Force from beams and columns acting on joint core; (b) Strut-mechanism(Paulay and Priestley, 1992)


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 103Truss failure may occur by crushing <strong>of</strong> the strut, by splitting <strong>of</strong> the nodalregion, or by bond failure along the anchorage <strong>of</strong> a tie (CEB-FIB, 2003).In Figure 2.4.1a the forces acting on an interior beam-column joint panel arereported. The horizontal shear force V jh is equal to:V = C + C + T − V = T + T − V(2.4.1)''jh s2 c2 1 c 1 2 cbecause the horizontal equilibrium equation referred to the end section <strong>of</strong>the beam yields to:Cs2 + Cc2 = T2(2.4.2)The vertical shear force can be similarly given by an equilibrium equation,but an enough accurate evaluation can be given by:Vhbjv= Vjh(2.4.3)hcwhere h b is the beam depth and h c is the column depth.A first approach to evaluate the shear capacity <strong>of</strong> a beam-column jointwithout transverse reinforcement consists in principal stress limits accor<strong>di</strong>ng toconcrete strength. Direct limits on the shear stress, accor<strong>di</strong>ng to (Hakuto et al.,2000) and reported in many International Codes (ACI 352, 2002; AIJ, 1999) arenot accurate because they do not account for the vertical axial force in thecolumn. The principal stresses p in the joint panel can be given by Mohr’sCircle assuming uniform normal and transverse stresses, f a e v jh respectively,accor<strong>di</strong>ng to the following equation:p2−fa⎛ fa⎞= ± +2⎜2⎟⎝ ⎠v2jh(2.4.4)Equation (2.4.4) allows the horizontal joint shear to be evaluated at the firstdevelopment <strong>of</strong> <strong>di</strong>agonal cracking:ffv = p 1 + ⇒ V = k f 1+ b h(2.4.5)aajh t jh 1 c j jpt k1 fc


104 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>where the tensile limit stress p t is assumed to be proportional to k 1 times thesquare root <strong>of</strong> concrete compressive strength, where k 1 is empirically evaluated.It is clearly shown in (2.4.5) that axial load delays the <strong>di</strong>agonal cracking in thejoint panel. The joint shear causing compressed concrete strut crushing,assuming the compressive limit stress p c to be proportional to k 2 times theconcrete compressive strength, is equal to:ffv = p 1 − ⇒ V = k f 1 − b h(2.4.6)aajh c jh 2 c j jpck2fcwhere k 2 is empirically evaluated.In the case <strong>of</strong> interior joints without transverse reinforcement, the values fork 1 e k 2 (Priestley, 1997) are 0.29 e 0.50, respectively. In the case <strong>of</strong> exteriorjoints, the proposed value for k 1 accor<strong>di</strong>ng to Priestley depends on thelongitu<strong>di</strong>nal bars anchoring details and it is 0.29 if the longitu<strong>di</strong>nal bars are bentat 90° outside the joint or 0.42 if they are anchored inside the joint. In the case<strong>of</strong> exterior joints with smooth bars the value for k 1 equal to 0.20 is suggested(Calvi et al., 2002). In the cited works, deterioration models are provided toaccount for k 1 and k 2 variability based on ductility demand.Accor<strong>di</strong>ng to European Code EC8 (CEN, 2005) the evaluation <strong>of</strong> thehorizontal maximum shear acting in the joint panel (shear demand) can beperformed through the following two expressions, respectively for exterior an<strong>di</strong>nterior joints:Vjhd = γrd ⋅ As1 ⋅fyd − VC(2.4.7)Vjhd= γrd ⋅ (As1 + As1) ⋅fyd − VC(2.4.8)where A s1 is the area <strong>of</strong> the beam top reinforcement, A s2 is the area <strong>of</strong> the beambottom reinforcement, V C is the column shear force, obtained from the analysisin the seismic design situation, γ Rd is a factor to account for overstrength due tosteel strain-hardening and should be not less than 1.2. The EC8 formulation forpre<strong>di</strong>cting the joint shear capacity is made up <strong>of</strong> two separated steps. First, there


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 105is an expression to evaluate the compression capacity <strong>of</strong> the strut that can berecognized in the joint panel under seismic actions and, then, an expressiondevoted to verify the tensile strength <strong>of</strong> the joint in order to avoid <strong>di</strong>agonalcracking. The horizontal shear demand should not exceed a value that couldcause the compression failure <strong>of</strong> the joint:νV = η f 1 − b ⋅ hηdjhd cd j jc(2.4.9)where η = 0.60 (1-f ck /250) for interior joints and η = 0.48 (1-f ck /250) forexterior joints, practically meaning that the strength <strong>of</strong> exterior joints is 0.8(0.48/0.60) times that one <strong>of</strong> interior joints (assuming the same joint materialsand detailing); ν d is the normalised axial force in the column above the joint, f ckis given in MPa, h jc is the <strong>di</strong>stance between the extreme layers <strong>of</strong> columnreinforcement, b j is the effective width <strong>of</strong> the joint.The Italian code (DM 14/1/2008) deals separately with joints belonging tonew and <strong>existing</strong> <strong>buil<strong>di</strong>ngs</strong>, the former ones being evaluated as in EC8. As for<strong>existing</strong> <strong>buil<strong>di</strong>ngs</strong>, IC contains two expressions devoted to verify beam-columnjoint without seismic provisions, that is without hoops in the panel. Theseexpressions allow to calculate the maximum <strong>di</strong>agonal compression (2.4.10) andtensile (2.4.11) stresses in the concrete joint core that must be below givenvalues related to the concrete strength f c :2 2N ⎛ N ⎞ ⎛ V ⎞nσnt= − + ≤ 0,3 fcfcin MPa2A ⎜ g2A ⎟ ⎜ gA ⎟⎝ ⎠ ⎝ g ⎠( )(2.4.10)N2 2⎛ N ⎞ ⎛ V ⎞nσnc= + + ≤2A ⎜ g2A ⎟ ⎜ gA ⎟g⎝ ⎠ ⎝ ⎠0,5fc(2.4.11)where N is the axial force acting on the upper column, A g is the gross area <strong>of</strong>the joint panel horizontal section and V n the horizontal shear acting in the jointpanel evaluated taking into account both the column shear and the shear


106 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>transmitted by the beam reinforcing bars.It is worth noting that a joint failure criterion based on tensile principalstress limit results to be over conservative. As a matter <strong>of</strong> fact, the joint panel isable to transfer noticeable shear forces also in a cracked phase due to the<strong>di</strong>agonal strut mechanism. The joint failure should be always related to thecompressed strut crushing. In the case <strong>of</strong> high axial loads, the compressed strutcrushing can be attained before the joint panel cracking (Paulay and Priestley,1992).The experimental evaluation <strong>of</strong> k 2 coefficient in equation (2.4.6) has toaccount for the real stress field in the joint, that is complex to be evaluated incracked phase, for the compressive strength deterioration due to <strong>di</strong>agonaltensile strains (Collins et al., 1980), and for the detailing <strong>of</strong> steel barsanchorage.The latter is a key aspect in the case <strong>of</strong> exterior joints, to guarantee thedevelopment <strong>of</strong> the compressed strut (Priestley, 1997): when beamreinforcement is anchored by ben<strong>di</strong>ng away from the joint (see Figure 2.4.2a)<strong>di</strong>agonal struts in the joint cannot be stabilized and joint failure occurs at anearly stage.It is to be noted that, in order to allow the truss mechanism to develop,tension ties must be able to develop up to the node <strong>of</strong> the truss, independent <strong>of</strong>bond capacity (i.e., smooth or ribbed reinforcement) (CEB-FIB, 2003).However, some specific issue about smooth reinforcement have to behighlighted, mainly related to the anchorage detail. For instance, when the baris compressed the end hook anchorage mobilizes a pushout cone, potentiallylea<strong>di</strong>ng to a splitting failure (Calvi et al., 2002; CEB-FIB, 2003), see Figure2.4.3.


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 107Figure 2.4.2. Breakdown <strong>of</strong> unreinforced exterior joints (Priestley, 1997)Figure 2.4.3. Cone (wedge) splitting failures in various old-type joints (CEB-FIB, 2003)


108 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>2.5 STRUCTURAL PERFORMANCE OF <strong>RC</strong> BUILDINGS AFTERTHE 6 TH APRIL 2009 L’AQUILA EARTHQUAKE, ITALYOn 6 th April 2009 an earthquake <strong>of</strong> magnitude M w = 6.3 occurred in theAbruzzo region; the epicentre was very close to the city <strong>of</strong> L’Aquila (about 6km away). The event produced casualties and damage to <strong>buil<strong>di</strong>ngs</strong>, lifelines andother infrastructures. An analysis <strong>of</strong> the main damage that <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> showedafter the event is presented in this Section. An analysis <strong>of</strong> the <strong>existing</strong> <strong>RC</strong>buil<strong>di</strong>ng stock in the area is carried out (Section 2.5.1), together with a review<strong>of</strong> the most important seismic codes in force in the last 100 years in Italy(Section 2.5.2). Comparison <strong>of</strong> the current design provisions <strong>of</strong> the Italian andEuropean codes with previous standards allows the main weaknesses <strong>of</strong> the<strong>existing</strong> buil<strong>di</strong>ng stock to be determined (Section 2.5.3). Damage to structuraland elements are finally analyzed thanks to photographic material collected inthe first week after the event (Section 2.5.4). The observations reported in thisSection were published in (Ricci et al., 2010).2.5.1. Reinforced concrete <strong>buil<strong>di</strong>ngs</strong> in L’AquilaThe layout <strong>of</strong> the ancient city <strong>of</strong> L’Aquila is characterized by two majorstreets crossing at right-angles at a place called “Quattro Cantoni”. Thehistorical centre (Figure 2.5.1.1) is situated on a raised hill overlooking thesurroun<strong>di</strong>ng area. It is encircled by me<strong>di</strong>eval walls, which still stand almostcompletely undamaged.The first structures beyond the ancient perimeter were the sports facilities inViale Gran Sasso, built in the 1930s. However, urbanization accelerated afterWorld War II, especially during the 1960s and 1970s, following the opening <strong>of</strong>the highway to Rome. In 1965 and 1975 two urban plans were enacted.Expansion mainly occurred in on the north-western side <strong>of</strong> the city, lea<strong>di</strong>ng in afew years to the complete saturation <strong>of</strong> the urban area bounded by the samehighway (Figure 2.5.1.1). Later expansion ra<strong>di</strong>ated out from the historicalcentre on all sides, except to the south-west, the course <strong>of</strong> the Aterno river(Figure 2.5.1.1).


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 109The current urban structure <strong>of</strong> L’Aquila is that <strong>of</strong> an historical centresurrounded by densely-packed suburbs, comprising the quarters <strong>of</strong> Pettino,Santa Barbara and Torrione, and less densely populated areas in the North-Western, inclu<strong>di</strong>ng Coppito, Sant'Antonio and Torretta quarters. The remainingarea within the city’s administrative boundaries includes several villages in thesurroun<strong>di</strong>ng area.Figure 2.5.1.1. L’Aquila: historical centre (black line), the Aterno river (blue line) and thehighway (yellow line) (Google Earth©)Accor<strong>di</strong>ng to data from the Italian National Institute <strong>of</strong> Statistics (Istitutonazionale <strong>di</strong> statistica, ISTAT), see Figure 2.5.1.2, collected in 2001, whichrepresent the most recent <strong>of</strong>ficial source for information about the <strong>buil<strong>di</strong>ngs</strong>tock in Italy, and hence in the L’Aquila area, 24% <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong> are reinforcedconcrete structures, 68% masonry structures and 8% structures <strong>of</strong> unspecifiedtype (Figure 2.5.1.2b). Data that identify age <strong>of</strong> construction <strong>of</strong> the <strong>buil<strong>di</strong>ngs</strong>(Figure 2.5.1.2a) in<strong>di</strong>cate that 55% <strong>of</strong> the entire stock was built after 1945. Alow overall incidence <strong>of</strong> <strong>RC</strong> structures shows that after 1945 new masonrystructures were still being built and that the number <strong>of</strong> <strong>RC</strong> structures increasedgradually over time. Based on the <strong>di</strong>stribution <strong>of</strong> number <strong>of</strong> storeys (Figure2.5.1.2c), only 5% <strong>of</strong> the <strong>buil<strong>di</strong>ngs</strong> have more than three storeys. Assuming thatall <strong>buil<strong>di</strong>ngs</strong> with more than three storeys are <strong>RC</strong> structures, it may still be


110 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>inferred that the vast majority <strong>of</strong> L’Aquila <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> are no more than threestoreys tall.100%80%60%40%20%0%1991(a)100%80%60%40%20%0%R.C. masonry other1 2 3 ≥ 4(b)(c)Figure 2.5.1.2. 2001 census ISTAT data for L’Aquila: (a) age <strong>of</strong> construction, (b) buil<strong>di</strong>ng type,(c) number <strong>of</strong> storeysIf the interstorey height is considered to vary between 3.0 and 3.5 meters,approximate formulation provided by the Eurocode (CEN, 2003) for <strong>RC</strong> framestructures gives for three-storey <strong>buil<strong>di</strong>ngs</strong> a fundamental period <strong>of</strong> 0.4 seconds.Working hypotheses assumed in this Section, which were useful in definingpoints <strong>of</strong> comparison between codes, are mostly confirmed by representativesamples <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong> employed in other field campaigns carried out for thesame earthquake (e.g., Liel and Lynch, 2009).Accor<strong>di</strong>ng to previous observations, in the following Section 2.5.3, whencomparing <strong>di</strong>fferent Italian Code spectral shapes, the comparison is focused on


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 111period values that range from 0 to 0.4 seconds. The latter assumption allows acomparison between constant acceleration branches <strong>of</strong> the spectra. A generalreview <strong>of</strong> design prescriptions in recent decades is employed to identify themain weaknesses <strong>of</strong> the buil<strong>di</strong>ng stock and to finally compare seismic demandgiven by codes with the demand <strong>of</strong> the earthquake event considered in thisSection.2.5.2. Overview <strong>of</strong> past seismic code provisionsL’Aquila and its neighbourhood were first legally recognized as a seismiczone in 1915. A specific law (RDL 573, 1915) was passed after the catastrophicseismic event occurring in January 1915 that struck Abruzzo (the Marsicaearthquake) killing more than 29,000 people. This law provided that newconstructions would have been designed taking into account seismic loads:horizontal forces were equal to 1/8 and 1/6 <strong>of</strong> gravity loads respectively at thefirst and second level <strong>of</strong> the buil<strong>di</strong>ng.In 1927 (RDL 431, 1927) a more detailed seismic classification wasintroduced; this classification <strong>di</strong>vided the Italian seismic area into two <strong>di</strong>fferentcategories; L’Aquila belonged to the less restricted one (second category).<strong>Seismic</strong> provisions were simply achieved by limiting the number <strong>of</strong> storeys: forthe second category zone the 1927 law allowed construction <strong>of</strong> three-storey<strong>buil<strong>di</strong>ngs</strong>, and for specific situations even four-storey <strong>buil<strong>di</strong>ngs</strong> were accepted.Horizontal forces were equal to 1/10 <strong>of</strong> the storey weight for structures up to 15meters tall or 1/8 for structures higher than this limit. This code gave specificprescriptions for <strong>RC</strong> structures inclu<strong>di</strong>ng prescriptions for <strong>di</strong>mensions <strong>of</strong> beamand column sections and the least amount <strong>of</strong> steel reinforcement required.In the following years, between 1930 and 1937, three seismic codes wereenacted (RDL 682, 1930; RDL 640, 1935; RDL 2105, 1937) and their mainconcern was the evaluation <strong>of</strong> seismic forces. For seismic vertical action thead<strong>di</strong>tional load was determined as equal to 1/3 <strong>of</strong> the structural weight, thusreducing the amount applied in the 1915 regulations. In second category zonesthe ratio between seismic horizontal forces and vertical forces due to gravity


112 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>loads (base shear coefficient) was initially 0.05 (RDL 640, 1935) and then 0.07(RDL 2105, 1937). These prescriptions were confirmed in 1962 (Legge 1684,1962) with less restrictive limits about buil<strong>di</strong>ng height and setting themaximum number <strong>of</strong> storeys at seven. Under this law further areas <strong>of</strong> thecountry were classified as seismic.In 1975 (DM 40, 1975) a fundamental innovation was introduced into theanalytical procedure: for the first time within Italian regulations the dynamicproperties <strong>of</strong> the structures were considered. Starting from this year, seismicaction could be determined by means <strong>of</strong> static and dynamic analyses. In thestatic analysis, the resultant <strong>of</strong> lateral force <strong>di</strong>stribution applied to the buil<strong>di</strong>ngwas given by Eq. 2.5.2.1, where W is the total weight <strong>of</strong> the structural masses;R the response coefficient, assumed as a function <strong>of</strong> the fundamental period <strong>of</strong>the structure; coefficient C represents the seismic action (Eq. 2.5.2.2), and isdefined by means <strong>of</strong> S, the seismic intensity parameter. Coefficients ε and βrespectively express soil compressibility (ε=1.00-1.30) and the possiblepresence <strong>of</strong> structural walls (β =1.00-1.20).Fh= C⋅ R ⋅ε ⋅β⋅ W(2.5.2.1)S − 2C = (2.5.2.2)100Fh= 0.07 ⋅ W(2.5.2.3)For second category zones, S was assumed equal to 9. If coefficients ε and βwere considered equal to 1, respectively correspon<strong>di</strong>ng to stiff soil and absence<strong>of</strong> structural walls, a structure, whose fundamental period was lower than 0.8seconds, was characterized by a base shear coefficient (F h /W) <strong>of</strong> 0.07 and it wasthe same as that adopted up to 1975 (see Eq. 2.5.2.3).The coefficient given by the product <strong>of</strong> C and R should be interpreted as adesign inelastic acceleration demand: it took into account dynamic properties <strong>of</strong>the structure and a strength reduction factor evaluated upon <strong>di</strong>ssipative capacity<strong>of</strong> the structure. Nevertheless, lateral forces applied to the buil<strong>di</strong>ng were


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 113proportional to the height <strong>of</strong> the slab at each storey determined from thefoundation level, assuming a linear <strong>di</strong>stribution with an “inverted triangular”shape that is more suitable to represent the actual dynamic behaviour <strong>of</strong> thestructure, compared with previous code prescriptions.New generation codes explicitly express this kind <strong>of</strong> <strong>di</strong>ssipative capacity <strong>of</strong>the structures; Eurocode 8 (CEN, 2003) does it by means <strong>of</strong> the “behaviourfactor”. Accor<strong>di</strong>ng to the Eurocode 8 definition, the behaviour factor q is anapproximation <strong>of</strong> the ratio <strong>of</strong> the seismic forces that the structure wouldexperience if its response was completely elastic with 5% viscous damping tothe seismic forces that may be used in the design, with a conventional elasticanalysis model, still ensuring a satisfactory response <strong>of</strong> the structure. Thevalues <strong>of</strong> q, which also account for the influence <strong>of</strong> the viscous damping being<strong>di</strong>fferent from 5%, are given for various materials and structural systemsaccor<strong>di</strong>ng to the relevant ductility classes.Regar<strong>di</strong>ng seismic input, even if <strong>di</strong>fferent new seismic design codes wereapproved (DM 24/1/1986; DM 16/1/1996), no changes have been introducedregar<strong>di</strong>ng this aspect since 1975. On the other hand, in this period, the LimitState method was introduced and, for Ultimate Limit State assessment, designacceleration was supposed to be increased by a factor <strong>of</strong> 1.50, thus obtaining anacceleration <strong>of</strong> (1.50×0.07g), equal to 0.105g.Furthermore, it is worth noting that the first prescriptions close to theperformance-based seismic design approach, such as the attainment <strong>of</strong> bothproper local and global ductility capacity, were provided in 1997 with anexplanatory document attached to the 1996 code (Circ. M.LL.PP. 65, 1997). Inthis document there were limits for longitu<strong>di</strong>nal and transverse reinforcement <strong>of</strong>beams and columns with specific prescription in the end zone <strong>of</strong> each structuralelement (critical region). In the 1997 document, ad<strong>di</strong>tional prescriptions wereprovided regar<strong>di</strong>ng proper anchorage <strong>of</strong> bars, and it was prescribed to lengthenlongitu<strong>di</strong>nal and transverse reinforcement <strong>of</strong> the column in beam-column joints.The latter prescription regar<strong>di</strong>ng beam-column joints was aimed at giving aproper local ductility to the element. Although this document (Circ. M.LL.PP.


114 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>65, 1997) represented an important step towards performance-based designcriteria in Italy, lack in prescriptions about regularity criteria in plan andelevation is still recognizable and these criteria remained qualitative, withoutany specific quantitative definition to help in regularity classification.In the 2003 seismic code (OPCM 3274, 2003) and its followingmo<strong>di</strong>fications (OPCM 3431, 2005) an innovative seismic input definition wasintroduced, representing the first real upgrade towards the Eurocode 8approach. In this document an elastic spectrum was provided with a definedshape in which the only value to be changed, considered a function <strong>of</strong> theseismic zone, was the anchorage Peak Ground Acceleration (PGA) on stiff soiltype (ground type A). L’Aquila belonged to the second category and the PGAvalue on ground type A was 0.25g. This spectrum was to be amplifiedconsidering site specific characteristics, taking into account other ground typesand topographic con<strong>di</strong>tions. The elastic acceleration spectrum was to bereduced by the q factor value depen<strong>di</strong>ng on the specific structural type, thusobtaining a design acceleration spectrum. This document explicitly introduce<strong>di</strong>n Italy the strength hierarchy concept, ensuring the development <strong>of</strong> inelasticdeformations in the highest possible number <strong>of</strong> ductile elements and not inelements with lower rotational capacity (that is, in beams and not in columns,due to the <strong>di</strong>fferent axial load), but also provi<strong>di</strong>ng over-strength to brittle failuremechanisms with respect to ductile ones. Furthermore, proper quantitativedefinition <strong>of</strong> regularity criteria in plan and in elevation was introduced, fixingmaximum variation <strong>of</strong> mass, stiffness and strength over buil<strong>di</strong>ng height.The most recent Italian code (DM 14/1/2008) defines maximumacceleration expected at the site no longer with <strong>di</strong>vision in terms <strong>of</strong> seismiczones but as a function <strong>of</strong> geographic coor<strong>di</strong>nates <strong>of</strong> the site. For L’Aquila(latitude 42.38; longitude 13.35), the PGA is 0.261 g on ground type A for a10% probability <strong>of</strong> exceedance in 50 years. In the case <strong>of</strong> L’Aquila, 2003 and2008 PGA values are very close to each other.


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 1152.5.3. Spectral considerations<strong>Seismic</strong> demand defined by previous codes can be considered equal to thelowest seismic capacity <strong>of</strong> structures designed accor<strong>di</strong>ng to them. The seismicdemand <strong>of</strong> old codes can be easily compared with the current code seismicdemand and actual seismic demand registered during the 2009 L’Aquila event.Eurocode 8 (CEN, 2003) and the Italian Code (DM 14/1/2008) provide aNewmark-Hall functional expression for the elastic spectrum. By means <strong>of</strong><strong>of</strong>ficial Italian hazard data, given the specific geographic coor<strong>di</strong>nates andground type, the elastic spectrum may be defined for the considered site.Material, reinforced concrete in this study, and ductility class are necessary todefine the behaviour factor q (see Section 2.5.2); the latter is employed to passfrom the elastic spectrum to the design spectrum.Both Eurocode 8 and the Italian code provide two ductility classesdepen<strong>di</strong>ng on the hysteretic <strong>di</strong>ssipation capacity. Both classes correspond to<strong>buil<strong>di</strong>ngs</strong> designed, <strong>di</strong>mensioned and detailed in accordance with specificearthquake-resistant provisions, enabling the structure to develop stablemechanisms associated with large <strong>di</strong>ssipation <strong>of</strong> hysteretic energy underrepeated reversed loa<strong>di</strong>ng, without suffering brittle failures.Design spectrum defined by the Italian Code (DM 14/1/2008) for the LifeSafety Limit State can be compared with the 1996 Ultimate Limit State spectralshape; the former was evaluated for both ductility classes, namely high ductilityclass (CD “A”) and low ductility class (CD “B”), assuming a behaviour factor qdetermined for new design <strong>RC</strong> frame structures (see Figure 2.5.3.1a).Another interesting comparison can be made between the 1996 inelasticspectral shape and design response spectra evaluated for <strong>existing</strong> <strong>RC</strong> structuresconsidering extreme values <strong>of</strong> q factor (1.5-3.0) accor<strong>di</strong>ng to the current Italianseismic code (Circ. M.LL.PP. 617, 2009), see Figure 2.5.3.1b. Indeed, bothEurocode 8 and the Italian Code provide <strong>di</strong>fferent values <strong>of</strong> behaviour factor qfor new design and <strong>existing</strong> <strong>buil<strong>di</strong>ngs</strong>, presuming that the latter cannot becharacterized by properly high hysteretic <strong>di</strong>ssipation capacity.Accor<strong>di</strong>ng to the Ultimate Limit State spectrum adopted in Italy between


116 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>1975 and 1996, a constant value <strong>of</strong> 0.105g was assumed for spectral or<strong>di</strong>natesbetween 0 and 0.8 seconds. This value for design inelastic acceleration can bereasonably considered representative <strong>of</strong> the minimum base shear coefficient <strong>of</strong>the great majority <strong>of</strong> L’Aquila <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>, if properly designed accor<strong>di</strong>ng tocodes until 2003 and given ISTAT data (see Figure 2.5.1.2a).Comparing constant acceleration branches <strong>of</strong> the various spectra shown inFigure 5a it may be noted that a buil<strong>di</strong>ng designed in CD “A”, and regular inplan and elevation, so characterized by a q factor <strong>of</strong> 5.85, accor<strong>di</strong>ng to thecurrent Italian Code, is designed for the same seismic demand as in the oldcodes. However, it has to be considered that previous codes provided neitherdesign rules nor detailed structural prescriptions able to ensure global and localductility required by the current code, which allows adoption <strong>of</strong> a q factor <strong>of</strong>5.85.Generally, <strong>existing</strong> structures are unable to show a highly ductile behaviourand it is not possible to ensure that the structure develops stable mechanismsassociated with large <strong>di</strong>ssipation <strong>of</strong> hysteretic energy. This is why actual codesconsiderably limit q in such cases, allowing it in the range (1.5-3.0). The choice<strong>of</strong> a value in this range should be made accor<strong>di</strong>ng to regularity criteria and theemployment <strong>of</strong> material properties. Hence, a proper comparison has to becarried out between the current seismic demand spectra provided for <strong>existing</strong>structures and the former code spectrum (see Figure 2.5.3.1b). The lattercomparison leads to a ratio <strong>of</strong> at least 2 between the current seismic demandand the old seismic demand.Design procedures and details accor<strong>di</strong>ng to new generation codes, such asEurocode, (BS EN 1990, 2002), for the Ultimate Limit State, considering thesecond reliability class (<strong>RC</strong>2), accor<strong>di</strong>ng to the same Eurocode definition (BSEN 1990, 2002), lead to an annual failure probability not higher than 1⋅ 10 −6 .A ratio <strong>of</strong> current to old code demands, as calculated above, <strong>of</strong> at least 2,does not mean Life Safety limits are exceeded for all <strong>buil<strong>di</strong>ngs</strong>; on the otherhand, the percentage <strong>of</strong> buil<strong>di</strong>ng failure over the whole population, in this case,would definitely be higher than1⋅ 10 −6 .


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 1170.50a/g0.50a/g0.400.40D.M. 2008 (q=1.50)0.30D.M. 2008 (CD"B")0.300.20(D.M. 1975 - D.M.1996)D.M. 2008 (CD"A")0.20(D.M.1975 - D.M.1996)D.M. 2008 (q=3.00)0.100.10T [sec]0.000.00 0.50 1.00 1.50 2.00 2.50 3.00(a)2.00 a/gAQK-EWAQG-EWAQA-EW1.60AQV-EWAQK-NSAQG-NS1.20AQA-NSAQV-NS0.80D.M. 2008 - TR 475D.M. 2008 - TR 975T [sec]0.000.00 0.50 1.00 1.50 2.00 2.50 3.00(b)2.00 a/gAQK-ZAQG-Z1.60AQA-ZAQV-ZD.M. 2008 - TR 4751.20D.M. 2008 - TR 9750.800.400.40T [sec]0.000.00 0.50 1.00 1.50 2.00 2.50 3.00T [sec]0.000.00 0.50 1.00 1.50 2.00 2.50 3.00(c)(d)Figure 2.5.3.1. Inelastic old code spectra compared with current code spectra for new designstructures (a) and <strong>existing</strong> structures (b). Current elastic code spectra compared with recordedsignal spectra for horizontal (c) and vertical component (d)If the elastic demand spectra <strong>of</strong> the registered signals are compared with thecurrent code’s elastic demand spectra, determined for <strong>di</strong>fferent return periods(T R 475 and 975 years) on ground type A, it may be noted that the spectra <strong>of</strong> theregistered signals exceed code demand in most <strong>of</strong> the frequency rangeconsidered. Figure 2.5.3.1c compares elastic spectra determined fromhorizontal components <strong>of</strong> the registered signals in stations AQK, AQG, AQAand AQV, while Figure 2.5.3.1d compares vertical components <strong>of</strong> the same


118 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>signals with the vertical code spectra.2.5.4. Field survey <strong>of</strong> structural damageIn this Section the main structural damage to <strong>RC</strong> structures after theL’Aquila earthquake is presented. Photographic documentation (Verderame etal., 2009c) was produced on the days imme<strong>di</strong>ately following the 6 th April 2009mainshock. Generally speaking, damage to structural elements is not s<strong>of</strong>requent and it seldom involves the whole structural system.The main structural damage that involved <strong>RC</strong> columns can be easilyrecognized as failure caused by mechanisms that capacity design rules tend toavoid or at least to limit. During an earthquake, columns are characterized byhigh flexural and shear demand; maximum flexural demand combined withaxial force produced by gravity loads and seismic loads are located at the end <strong>of</strong>the element; in these zones (critical regions) rotational ductility demandconcentrates. Therefore, it is necessary to give an adequate rotational capacityand to avoid buckling <strong>of</strong> compressed longitu<strong>di</strong>nal reinforcements.Modern seismic codes, such as Eurocode 8 (CEN, 2003), provideprescriptions to increase rotational capacity <strong>of</strong> the section: the upper limit onthe longitu<strong>di</strong>nal reinforcement percentage leads to a higher ultimate curvature<strong>of</strong> the section; proper hoop spacing and cross-tie presence give, due to a moreefficient confinement action on concrete, an ad<strong>di</strong>tional increase in sectioncurvature capacity; finally, proper spacing between hoops avoids buckling inlongitu<strong>di</strong>nal reinforcement, or at least fixes an acceptable upper bound limit forwhich this phenomenon occurs.However, the prescriptions and structural details presented above are typical<strong>of</strong> modern design concepts that first appeared in Italy in 1997. It is thereforepossible to find <strong>RC</strong> columns with longitu<strong>di</strong>nal reinforcement percentageexcee<strong>di</strong>ng 4% limit or hoops closed with 90 degree hooks, or with insufficientlythick spacing (15-20 cm).


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 119(a)(b)Figure 2.5.4.1. Column with smooth bars and poor transverse reinforcement (a); damage to acolumn due to axial force and ben<strong>di</strong>ng moment (b)Figure 2.5.4.1a presents a corner column <strong>of</strong> an <strong>RC</strong> buil<strong>di</strong>ng in the historicalcentre <strong>of</strong> L’Aquila, probably erected between 1950 and 1960. Damage occurredat the bottom end section <strong>of</strong> the element. The presence <strong>of</strong> smooth bars and asmall hoop <strong>di</strong>ameter (6 mm), closed with 90 degree hooks, can be observed, butthe most significant detail is the absence <strong>of</strong> any transverse reinforcement in thefirst 30–40cm <strong>of</strong> the element imme<strong>di</strong>ately adjacent to the beam-column jointregion. Figure 2.5.4.1b shows a circular column belonging to a buil<strong>di</strong>ng in theresidential zone <strong>of</strong> Pettino, built in the 1980s: typical damage due to axial forceand ben<strong>di</strong>ng moment is recognizable; the concrete cover was crushed due tohigh compression strains and longitu<strong>di</strong>nal bar buckling. In this case hoopspacing is, once again, not thick enough, as in the case <strong>of</strong> Figure 2.5.4.1a, butprobably in this case the column was designed in accordance with codeprescriptions at the time <strong>of</strong> construction.


120 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>(a)(b)(c)(d)Figure 2.5.4.2. Shear failure <strong>of</strong>: (a) rectangular and (b) circular (b) columns, (c) columnadjacent to partial infilling panels, (d) squat column adjacent to basement level concrete walls


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 121High shear demand can produce brittle failures with an outstan<strong>di</strong>ngreduction in column <strong>di</strong>ssipative capacity. In order to prevent brittle failures,shear demand has to be determined accor<strong>di</strong>ng to flexural capacity <strong>of</strong> theelement; applying to shear demand an amplifying coefficient to allow forvariability in steel properties (CEN, 2003) can prevent brittle failureoccurrence. These prescriptions have been laid down since 2003 in the Italiancode; no control <strong>of</strong> the failure mechanism used to be applied before this codewas released. All the above considerations can be confirmed by brittle failure <strong>of</strong>the columns reported in Figure 2.5.4.2.With regard to the rectangular column in Figure 2.5.4.2a, whose section is30×100 cm 2 , belonging to a 1980s’ buil<strong>di</strong>ng, shear failure is evident, involvingthe top end section. Transverse reinforcement has hoop spacing <strong>of</strong>approximately 15-20cm, and is definitely under-designed with respect tocolumn section size, that is, with respect to the inertia <strong>of</strong> the section, thuslea<strong>di</strong>ng to premature shear failure <strong>of</strong> the element. The brittle failure mechanismis highlighted by the crushing <strong>of</strong> the concrete within the reinforcement and thecomplete opening <strong>of</strong> the third and fourth hoops from the top end <strong>of</strong> the element.Figure 2.5.4.2b shows shear failure <strong>of</strong> a 30cm-<strong>di</strong>ameter circular column; inthis case it is possible to recognize insufficient hoop spacing, which leads to thetypical <strong>di</strong>agonal cracking typical <strong>of</strong> shear failure mechanisms and longitu<strong>di</strong>nalbar buckling in the column.In order to stress the non-secondary role played by column – infillinteraction in determining brittle failures in the structural elements, Figure2.5.4.2c shows the damage that columns present in these kinds <strong>of</strong> situation. It ispossible to recognize the brittle failure in the column due to the localinteraction with the concrete infill partially covering the bay frame, reaching1/3 <strong>of</strong> the total column height. Partial infilling that effectively interacts with thecolumn reduces the slenderness <strong>of</strong> the element and consequently produces ahigher shear demand that exceeds column shear capacity. This kind <strong>of</strong>phenomenon involves all the columns interacting with the concrete partialinfilling.


122 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>Figure 2.5.4.2d gives an example <strong>of</strong> a basement that is partially below theground level. Accor<strong>di</strong>ng to common buil<strong>di</strong>ng practice, basement levels arecharacterized by walls, <strong>of</strong>ten realized in concrete, aimed at a retaining function<strong>of</strong> the adjacent embankment; concrete wall height is limited with respect tocolumn height to allow the fitting <strong>of</strong> windows. This structural solution leads toa strict reduction in column slenderness with a consequent increase in sheardemand; moreover, decreasing shear span can mo<strong>di</strong>fy the shear span ratio <strong>of</strong> theelement up to a squat column behaviour. This situation is <strong>of</strong> no secondaryimportance since the shear resistance mechanism <strong>of</strong> a squat column <strong>di</strong>ffers withrespect to the typical behaviour <strong>of</strong> a slender element. Differences between shearcapacity formulations proposed in Eurocode 8 (CEN, 2005) for <strong>existing</strong><strong>buil<strong>di</strong>ngs</strong> for slender and squat columns testify to the <strong>di</strong>fference between shearfailure mechanisms. Hence, if local interaction between the column andconcrete wall is not allowed for, premature brittle failure due to excessiveconcrete compression can <strong>of</strong>ten occur.Figure 2.5.4.3. Shear failure in squat columns <strong>of</strong> the staircaseColumns belonging to staircases can easily show brittle failures as well.Most common staircase types generally possess <strong>di</strong>scontinuity elements in theregular <strong>RC</strong> frame scheme composed by beams and columns. Indeed, on oneside a staircase consists <strong>of</strong> inclined axis elements (beam or slab); on the other,


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 123squat columns are created by the intersection <strong>of</strong> inclined axis elements with thecolumn.Staircase elements lend a considerable lateral stiffness to the wholestructural system, first due to axial stiffness <strong>of</strong> the inclined elements andsecondly to higher lateral stiffness <strong>of</strong> squat columns. These contributions areeasily appreciable via linear analyses. On the other hand, staircase elements canrepresent a weak point because they possess higher shear demand that can leadto brittle failure mechanisms.Figure 2.5.4.3 shows a staircase composed by inclined beams; the squatcolumn in the corner has typical shear failure. Poor transverse reinforcement,both in terms <strong>of</strong> hoop spacing and <strong>di</strong>ameter, can be recognized.Figure 2.5.4.4. Failure in reinforced concrete wallsShear failures were found in reinforced concrete as well. As an example, inFigure 2.5.4.4 two reinforced concrete walls, respectively with two <strong>di</strong>fferentshape factors, are shown; damage consists <strong>of</strong> a spread <strong>di</strong>agonal cracking. Lowlongitu<strong>di</strong>nal and transverse reinforcement percentages can be recognized,


124 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>especially compared with minimum values prescribed by design codes based oncapacity design approach.(a)(b)(c)(d)Figure 2.5.4.5. Joint failure with evidence <strong>of</strong> (a) longitu<strong>di</strong>nal bar buckling and (b) <strong>di</strong>agonalcracking failure in concrete joint panel; (c) (d) failure mechanisms at joint – column interfacesurface


Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 125Beam-column joints can completely change the structural behaviour <strong>of</strong> thewhole buil<strong>di</strong>ng and their failure should necessarily be avoided in a properseismic design approach: such elements possess brittle failure mechanisms. Ingeometrically very small beam-column joints, demand coming from beams andcolumns is concentrated and both the concrete panel and longitu<strong>di</strong>nal bars aresubjected to high gra<strong>di</strong>ents <strong>of</strong> shear and flexural demand.Joint failure mechanisms are mainly governed by shear and bondmechanisms; force <strong>di</strong>stribution, which allows shear and moment transfer,produces <strong>di</strong>agonal cracking and hence joint failure due to <strong>di</strong>agonal compressionin the concrete is quite likely to occur, thus producing a reduction in strengthand stiffness in the connection.Generally speaking, joint design is limited by concrete compressive stress;the <strong>di</strong>agonal stress induced by the elements meeting in the joint cannot exceedconcrete compressive stress. In order to keep structural continuity whenconcrete cracking occurs, a proper transverse reinforcement along the wholeelement should be provided. The presence <strong>of</strong> transverse reinforcement allowsstresses to be transferred by means <strong>of</strong> a strut and tie mechanism, even if thecracking phase has passed in the concrete. The latter mechanism can bedeveloped if longitu<strong>di</strong>nal reinforcement, transverse reinforcement and concretestruts contribute to truss formation. If capacity design prescriptions arefollowed, preventing brittle failure in joints gives the chance to develop moreductile mechanisms in the other structural elements.Specific design rules for beam-column joints appeared in the Italian designprescriptions only in 2003 (OPCM 3274, 2003). Indeed, in the explanatorydocument to the 1996 code (Circ. M.LL.PP. 65, 1997) the transversereinforcement in the joints was simply required to be at least equal to the hoopspacing in the columns.Damage from the 6 th April 2009 earthquake clearly shows how hazardousfailure <strong>of</strong> joints can be. Figure 2.5.4.5a shows an external beam-column joint,characterized by an extensive cracking in the joint panel. The absence <strong>of</strong>transverse reinforcement leads to local buckling <strong>of</strong> the longitu<strong>di</strong>nal bars that


126 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>consequently results in concrete cover spalling. Interestingly, the absence <strong>of</strong>proper transverse reinforcement in the joint also leads to a loss <strong>of</strong> anchorage inbeam longitu<strong>di</strong>nal reinforcement.Figure 2.5.4.5b shows typical <strong>di</strong>agonal cracking failure in a concrete panelbelonging to an external joint. Cracking begins at the intersection between thejoint and upper column and ends at the intersection between the joint and lowercolumn, producing the loss <strong>of</strong> monolithic connection. Absence <strong>of</strong> hoops, in thissituation too, leads to buckling in the external longitu<strong>di</strong>nal bars and involveslower column bars without transverse reinforcement in the first 30–40cm.Another noteworthy aspect in <strong>RC</strong> damage after the L’Aquila earthquake is apeculiar loss <strong>of</strong> connection at the lower joint-column interface; this aspect isemphasized and becomes a critical issue when there is insufficient longitu<strong>di</strong>naland transverse reinforcement both within the joint and at the column end.Generally speaking, the presence <strong>of</strong> a separation (previously present orotherwise) at the interface between the column and beam-column joint, if bothelements – column and joint – are well designed, complying with modernseismic prescriptions, should not prevent the development <strong>of</strong> a ductile failuremechanism in the column. Accor<strong>di</strong>ng to current code prescriptions, (i) aminimum amount <strong>of</strong> longitu<strong>di</strong>nal reinforcement, evenly <strong>di</strong>stributed around theperiphery <strong>of</strong> the section, and (ii) an adequate, effectively anchored transversereinforcement, both in the beam-column joint and at the column end, have to beadopted, thus avoi<strong>di</strong>ng brittle failure along the interface section betweencolumn and joint (Paulay and Priestley, 1992).Figure 2.5.4.5c reports a brittle failure mechanism due to the lack <strong>of</strong> transverseand longitu<strong>di</strong>nal reinforcement that led to loss <strong>of</strong> continuity at the intersectionbetween the joint and lower column, being the probable final cause <strong>of</strong> thefailure. Figure 2.5.4.5d shows a clear separation in concrete at the joint-columninterface; in this case, due to a complete spalling <strong>of</strong> the concrete cover, thereinforcement in the element may be recognized and it may be noted that thefirst hoop in the column is partially open. The lack <strong>of</strong> transverse reinforcementin the element made the separation at the joint-column interface critical.


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Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 135− Verderame G.M., Fabbrocino G., Manfre<strong>di</strong> G., 2008b. <strong>Seismic</strong> response<strong>of</strong> <strong>RC</strong> columns with smooth reinforcement. Part II: Cyclic tests.Engineering Structures, 30(9), 2289-2300.− Verderame G.M., Ricci P., Manfre<strong>di</strong> G., Cosenza E. 2008c. La capacitàdeformativa <strong>di</strong> elementi in c.a. con barre lisce: modellazione monotonae ciclica, Atti del convegno ReLUIS “Valutazione e riduzione dellavulnerabilità sismica <strong>di</strong> e<strong>di</strong>fici esistenti in c.a.”, Rome, Italy, May 29-30. Pp. 589-600.− Verderame G.M., Ricci P., De Carlo G., Manfre<strong>di</strong> G., 2009a. Cyclic bondbehaviour <strong>of</strong> plain bars. Part I: Experimental investigation. Constructionand Buil<strong>di</strong>ng Materials, 23(12), 3499-3511.− Verderame G.M., De Carlo G., Ricci P., Fabbrocino G., 2009b. Cyclicbond behaviour <strong>of</strong> plain bars. Part II: Analytical investigation.Construction and Buil<strong>di</strong>ng Materials, 23(12), 3512-3522.− Verderame G.M., Iervolino I., Ricci P,. 2009c. Report on the damages on<strong>buil<strong>di</strong>ngs</strong> following the seismic event <strong>of</strong> 6th <strong>of</strong> April 2009 time 1.32(UTC) – L’Aquila M=5.8, V1.20. http://www.reluis.it/− Verderame G.M., Ricci P., Manfre<strong>di</strong> G., Cosenza E., 2010. Ultimatechord rotation <strong>of</strong> <strong>RC</strong> columns with smooth bars: some considerationsabout EC8 prescriptions. Bulletin <strong>of</strong> Earthquake Engineering. DOI:10.1007/s10518-010-9190-x− Yalcin C., Kaya O., Sinangil M., 2008. <strong>Seismic</strong> retr<strong>of</strong>itting <strong>of</strong> R/Ccolumns having plain rebars using CFRP sheets for improved strengthand ductility. Construction and Buil<strong>di</strong>ng Materials, 22(3), 295-307.− Zhu L., Elwood K.J., Haukaas T., 2007. Classification and seismic safetyevaluation <strong>of</strong> <strong>existing</strong> reinforced concrete columns. ASCE Journal <strong>of</strong>Structural Engineering, 133(9), 1316-1330.


136 Chapter II – <strong>Seismic</strong> behaviour <strong>of</strong> <strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 137Chapter IIIInfluence <strong>of</strong> infills on seismic behaviour <strong>of</strong>reinforced concrete <strong>buil<strong>di</strong>ngs</strong>3.1 INTRODUCTIONInfill walls are usually employed in reinforced concrete <strong>buil<strong>di</strong>ngs</strong> forpartition use and for thermal/acoustic insulation. Hence, they are considered asnon-structural elements; nevertheless, post-earthquake damage observation,experimental and numerical research have shown that their influence on seismicbehaviour <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> can be not negligible at all. Modern seismic codes(e.g. FEMA 356, 2000; CEN, 2004a; DM 16/1/1996; DM 14/1/2008) prescribeto account for the possible influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> <strong>RC</strong>frames, both at local and global level. Even though the awareness about thisissue in earthquake engineering is not very recent, it is likely to state thatpractically no <strong>existing</strong> <strong>RC</strong> buil<strong>di</strong>ng was designed accounting for the presence <strong>of</strong>these elements.Generally speaking, infill walls can provide a considerable contribution to a<strong>RC</strong> structure in terms <strong>of</strong> strength and stiffness. However, their post-peakresponse is usually quite brittle. Moreover, many uncertainties affect theevaluation <strong>of</strong> their behaviour; the first (and obvious) reason is that this kind <strong>of</strong>elements are not designed to have a specific behaviour under seismic action.Different collapse modes are possible, both in-plane and out-<strong>of</strong>-plane. Also,


138 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>many <strong>di</strong>fferences in materials and constructive methods are observed.The interaction between infill panels and <strong>RC</strong> structural elements underseismic action develops at global level, lea<strong>di</strong>ng to an increase in lateral stiffnessand base shear capacity, but also at local level, potentially lea<strong>di</strong>ng to brittlefailure mechanisms in surroun<strong>di</strong>ng elements such as columns or beam-columnjoints.It is not easy to determine whether infill influence on seismic behaviour <strong>of</strong><strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> is beneficial or not, on the whole. Probably, the best syntheticdescription <strong>of</strong> this issue can be drawn from the conclusions reported in (Dolšekand Fajfar, 2001): the infill walls can have a beneficial effect on the structuralresponse, provided that they are placed regularly throughout the structure, andthat they do not cause shear failures <strong>of</strong> columns.In this Chapter, main issues about the influence <strong>of</strong> infills on seismicbehaviour <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> are <strong>di</strong>scussed. To this end, the behaviour <strong>of</strong> an infillpanel and its local interaction with the surroun<strong>di</strong>ng <strong>RC</strong> members are <strong>di</strong>scussedfirst (Section 3.2). Hence, the influence <strong>of</strong> infills on global behaviour <strong>of</strong> <strong>RC</strong>structures is illustrated, also through experimental results from literature(Section 3.3). Finally, an analytical study on the influence <strong>of</strong> infills on period <strong>of</strong>vibration <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> is presented (Section 3.4).3.2 BEHAVIOUR OF <strong>RC</strong> FRAMES WITH MASONRY INFILLSFundamental issues about the behaviour <strong>of</strong> <strong>RC</strong> frames with masonry infillsare reported herein. Very extensive and comprehensive reviews can be found in(Crisafulli, 1997; Shing and Mehrabi, 2002).The in-plane lateral response <strong>of</strong> an infill panel can be described through thetypical behaviour shown by experimental tests on one bay-one storey infilled<strong>RC</strong> frames (e.g., Styliani<strong>di</strong>s, 1985; Pires, 1990; Mehrabi et al., 1996; Mosalamet al., 1997; Colangelo, 2003).


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 139(a)(b)(c)Figure 3.2.1. Cyclic lateral load-<strong>di</strong>splacement response <strong>of</strong> “weak” (a) or “strong” (b) infilled<strong>RC</strong> frames; Monotonic lateral load-<strong>di</strong>splacement response <strong>of</strong> bare, “weak” infilled or “strong”infilled <strong>RC</strong> frames (c) (Mehrabi et al., 1996)First, the response <strong>of</strong> the infilled <strong>RC</strong> frame is influenced, obviously, by thematerial characteristics <strong>of</strong> the infill panel (see Figure 3.2.1). Thesecharacteristics are influenced both by mortar and masonry unit properties;nevertheless, when evaluating the behaviour <strong>of</strong> an infilled <strong>RC</strong> frame thematerial mechanical characteristics are usually referred to the equivalenthomogeneous material, and are expressed through <strong>di</strong>fferent parameters such asthe Young’s elastic modulus, the shear elastic modulus, the compressivestrength or the shear cracking stress. These parameters are usually determinedfrom vertical or <strong>di</strong>agonal (i.e., with <strong>di</strong>fferent angles between the bed joint


140 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong><strong>di</strong>rection and the applied load) tests on masonry specimens. However, materialtypes and constructive methods can vary greatly in infill panels. Hence, highuncertainties and <strong>di</strong>spersion affect the determination <strong>of</strong> these characteristicswhen they have to be evaluated in order to model the influence <strong>of</strong> infill panelson structural behaviour (see Section 3.2.4).Behaviour <strong>of</strong> an infilled <strong>RC</strong> frame is also strongly influenced by theinteraction between the masonry panel and the surroun<strong>di</strong>ng <strong>RC</strong> structure, bothin terms <strong>of</strong> stiffness and strength.Generally, some <strong>di</strong>stinct phases in the response <strong>of</strong> an infilled frame can be<strong>di</strong>stinguished, focusing the attention on the monotonic envelope <strong>of</strong> a typicallateral force-<strong>di</strong>splacement curve.In a first phase, for very low values <strong>of</strong> lateral <strong>di</strong>splacement, the response <strong>of</strong>the infilled frame strictly depends on interface con<strong>di</strong>tions between the panel andthe surroun<strong>di</strong>ng elements. In non-integral infilled frames, due to shrinkage <strong>of</strong>the mortar or to constructive problems, there is a lack <strong>of</strong> contact between thetwo elements, thus lea<strong>di</strong>ng to high reduction in the initial stiffness (Crisafulli,1997). On the contrary, in integral infilled frames the initial response is givenby a monolithic behaviour <strong>of</strong> the whole composite system, ensured by bondcapacities at the interface between the panel and the frame (see Figure 3.2.2).Figure 3.2.2. Force-<strong>di</strong>splacement response <strong>of</strong> integral and non-integral infilled frames(Crisafulli, 1997)


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 141As far as integral infilled frames are concerned, with increase in lateral load<strong>di</strong>fferences in deformational characteristics between the panel and the <strong>RC</strong>frame cause cracking and separation at the interface between the two materials,lea<strong>di</strong>ng to a first stiffness decrease in the force-<strong>di</strong>splacement response. Thisseparation occurs for variable load levels, depen<strong>di</strong>ng also on the interfacecon<strong>di</strong>tions; however, it is expected to take place for very low drift values.Afterwards, an increase in the stress state narrowed in the opposite compressionangles and along the <strong>di</strong>agonal <strong>of</strong> the panel takes place, together with a <strong>di</strong>agonalcracking; contact areas between the frame and the panel further decrease (seeFigure 3.2.3).(a)(b)Figure 3.2.3. Normal and shear stresses acting on a loaded corner (a); increase in the stress statealong the <strong>di</strong>agonal <strong>of</strong> the panel (b) (Crisafulli, 1997)As the lateral load further increases, cracking and damage in the panelgradually increase up to the attainment <strong>of</strong> the maximum lateral strength <strong>of</strong> theinfilled frame. This mechanism is usually referred to as “truss mechanism”, dueto the clear analogy between the <strong>di</strong>agonal <strong>of</strong> the panel, along whichcompression stresses concentrates, and a compressed <strong>di</strong>agonal truss. Theinteraction between the compressed truss and the surroun<strong>di</strong>ng <strong>RC</strong> membersdevelops in corner contact areas whose <strong>di</strong>mensions are mainly influenced by theratio between the stiffness <strong>of</strong> the panel and the stiffness <strong>of</strong> the <strong>RC</strong> frame. Thisinteraction strictly influences the <strong>di</strong>stribution <strong>of</strong> forces in <strong>RC</strong> members (see


142 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>Figure 3.2.4). Shear and axial force variation in columns are <strong>of</strong> particularimportance.Figure 3.2.4. Ben<strong>di</strong>ng moment, shear and axial force <strong>di</strong>agrams for a typical infilled <strong>RC</strong> frame(Crisafulli, 1997)After the peak, the experimental curve shows a <strong>di</strong>fferent s<strong>of</strong>tening behaviourdepen<strong>di</strong>ng on the type <strong>of</strong> the panel failure and on the post-elastic response <strong>of</strong>the frame.Nevertheless, the above described truss mechanism – which initiallydevelops after the separation between the infill panel and the <strong>RC</strong> frame – mayor may not evolve into a primary load-resistance mechanism, mainly depen<strong>di</strong>ngon the interaction between the panel and the surroun<strong>di</strong>ng <strong>RC</strong> frame. Differentfailure modes may take place, <strong>di</strong>fferent from <strong>di</strong>agonal cracking <strong>of</strong> the panel,such as corner crushing or horizontal shear sli<strong>di</strong>ng. The failure mechanism <strong>of</strong>the infill panel may also influence the failure mechanism <strong>of</strong> the surroun<strong>di</strong>ng <strong>RC</strong>frame, for instance, by determining the location <strong>of</strong> plastic hinge in columns (seeFigure 3.2.5).


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 143Figure 3.2.5. Failure mechanisms <strong>of</strong> infilled frames (Shing and Mehrabi, 2002)


144 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>3.2.1. Influence <strong>of</strong> openingsPresence <strong>of</strong> openings is another issue which should be carefully consideredwhen evaluating the behaviour <strong>of</strong> an infilled <strong>RC</strong> frame, although it is not easyat all to be modelled. Numerical (e.g., Mosalam, 1996; Asteris, 2003) andexperimental (e.g., Mosalam et al., 1997; Kakaletsis and Karayannis, 2009)stu<strong>di</strong>es were carried out to investigate the influence <strong>of</strong> openings on the lateralforce-<strong>di</strong>splacement behaviour <strong>of</strong> an infilled <strong>RC</strong> frame. A general reduction instiffness and strength is observed, mainly depen<strong>di</strong>ng on the opening percentage(expressed as the ratio between the opening area and the total panel area), butalso on the opening position (Asteris, 2003). However, the evaluation <strong>of</strong> thisreduction can <strong>di</strong>ffer greatly from one model to another. Presence <strong>of</strong> openingscan also influence the developments <strong>of</strong> stress flows in the panel, lea<strong>di</strong>ng to theformation <strong>of</strong> resistance mechanism <strong>di</strong>fferent from the standard single truss (seeFigure 3.2.1.1).Figure 3.2.1.1. Single- (a) and multi- (b) <strong>di</strong>agonal truss formation (Mondal and Jain, 2008)


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 1453.2.2. Brittle failure in <strong>RC</strong> members due to local interaction with infillsThe local interaction between the panel and the adjacent beam and columnelements consists in a normal and shear stress transfer – developed in a contactarea (see Figure 3.2.3) whose <strong>di</strong>mensions are influenced by several factors –lea<strong>di</strong>ng to a severe force variation in <strong>RC</strong> members (see Figure 3.2.4). Asalready highlighted, this interaction can lead to brittle failure mechanisms, bothin columns and in beam-column joints. In particular, the resulting shear forceacting on a column may be significantly larger than the expected value resultingfrom section flexural strength, given by equilibrium <strong>of</strong> the element. Hence,even a column expected to have a ductile behaviour (see Section 2.3) mayexperience a shear failure. Moreover, a detrimental decrease in axial load takesplace. It is to be noted that the column shear span to be considered whenevaluating the behaviour resulting from interaction with an infill panel issignificantly lower than the column height, thus lea<strong>di</strong>ng to a squat-elementbehaviour.Figure 3.2.2.1. Shear failure in a column adjacent to partial infilling panels (see Section 2.5.4)


146 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>Moreover, a shear failure mechanism can take place in the squat columnresulting from the interaction with a partial infill (see Figure 3.2.2.1).(a)(b)Figure 3.2.2.2. Diagonal cracking failure in a beam-column joint due to shear forces and“opening” moment due to interaction with the infill panel (Crisafulli, 1997) (a); observed failure<strong>of</strong> an unreinforced external joint after the 2009 L’Aquila earthquake (see Section 2.5.4) (b)In beam-column joints, the interaction with the infill panel can lead to<strong>di</strong>agonal cracking failure <strong>of</strong> the joint panel even before cracking <strong>of</strong> the adjacentbeam section (see Figure 3.2.2.2). Sli<strong>di</strong>ng shear failure may also take place atthe interface between column element and joint panel (Verderame et al.,2010a).It is to be noted that all <strong>of</strong> these brittle failure mechanisms may be avoided,or at least significantly limited, adopting the seismic details prescribed bymodern seismic codes accor<strong>di</strong>ng to Capacity Design principles, such astransverse reinforcement (i) in beam-column joints and (ii) at the ends <strong>of</strong> thecolumns (with proper spacing). Although these prescriptions are aimed (i) atavoi<strong>di</strong>ng joint failure due to flexural forces from beams and columns and (ii) atprovi<strong>di</strong>ng higher ductility in critical (plastic hinge) region, respectively, theycan also avoid brittle failure mechanisms due to forces from local interaction


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 147with infill panels.However, modern seismic code also provide specific prescriptions aimed atavoi<strong>di</strong>ng brittle failure mechanisms due to interaction between <strong>RC</strong> columns an<strong>di</strong>nfill panels. For instance, EC8-part I (CEN, 2004a), at Section 5.9, prescribesto consider the shear force acting on the column as the smaller <strong>of</strong> (i) thehorizontal component <strong>of</strong> the strut force <strong>of</strong> the infill, assumed to be equal to thehorizontal shear strength <strong>of</strong> the panel, and (ii) the shear force determinedaccor<strong>di</strong>ng to the Capacity Design rule – that is, on the basis <strong>of</strong> the equilibrium<strong>of</strong> the column under end moment resistances – assuming that the plastic hingesdevelop at the two ends <strong>of</strong> the contact length, which is assumed to be equal tothe full vertical width <strong>of</strong> the <strong>di</strong>agonal strut <strong>of</strong> the infill.Moreover, if the height <strong>of</strong> the infill is smaller than the clear length <strong>of</strong> theadjacent columns, the same code prescribes to consider the entire length <strong>of</strong> thecolumns as critical region, thus provi<strong>di</strong>ng a proper amount <strong>of</strong> transversereinforcement, and to assume that the plastic hinges develop at the two ends <strong>of</strong>the length <strong>of</strong> the column not in contact with the infill when evaluating the shearforce from the equilibrium <strong>of</strong> the column under moment resistances (see Figure3.2.2.3).Figure 3.2.2.3. Partial masonry infill in concrete frame (Paulay and Priestley, 1992)


148 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>3.2.3. Out-<strong>of</strong>-plane behaviourSo far, in-plane behaviour <strong>of</strong> infill panels has been described, since itproduces relevant interaction mechanisms with surroun<strong>di</strong>ng <strong>RC</strong> elements;nevertheless, out-<strong>of</strong>-plane failure mechanisms are <strong>of</strong> importance, too, since theysignificantly influence the own damage <strong>vulnerability</strong> <strong>of</strong> infill elements (seeFigure 3.2.3.1).Out-<strong>of</strong>-plane resistance is mainly due to the formation <strong>of</strong> an archingmechanism, which is highly influenced by panel slenderness (Shing andMehrabi, 2002). Moreover, experimental tests showed that the interactionbetween in-plane and out-<strong>of</strong>-plane resistance has no significant influence(Flanagan and Bennett, 1999).(a)(b)Figure 3.2.3.1. In-plane and out-<strong>of</strong>-plane forces acting on an infill panel (Crisafulli, 1997) (a);observed out-<strong>of</strong>-plane failure <strong>of</strong> an external infill layer after the 2009 L’Aquila earthquake (b)3.2.4. Models for the analysis <strong>of</strong> infilled <strong>RC</strong> framesModels reproducing the in-plane lateral force-<strong>di</strong>splacement behaviour <strong>of</strong>infill panels are used to evaluate the influence <strong>of</strong> these elements on structuralresponse. They can be <strong>di</strong>vided in two categories: micro-models and macromodels.


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 149Micro-models are essentially based on Finite Element (FE) method. Theinfill panel is <strong>di</strong>scretized in a number <strong>of</strong> sub-elements, representing anequivalent homogeneous material or a two-phase (mortar and masonry units)material. Contact element are also employed to model the boundary interactionbetween infill panel and reinforced concrete. By means <strong>of</strong> these models, localeffects such as cracking, crushing and contact interaction can be evaluated. FEanalyses are usually employed to investigate numerically the influence <strong>of</strong><strong>di</strong>fferent parameters (e.g., presence <strong>of</strong> openings) on the response <strong>of</strong> singleinfilled frames with a relatively low number <strong>of</strong> elements (Mosalam, 1996;Asteris, 2003).Nevertheless, the computational effort and the refined modelling required bythis approach do not fit the needs <strong>of</strong> a structural analysis aimed at evaluatingthe global behaviour <strong>of</strong> a <strong>RC</strong> buil<strong>di</strong>ng with infill walls. To this aim, macromodelsare employed. Most <strong>of</strong> them are based on the equivalent strut concept,due to the mechanical behaviour usually shown by an infill panel after theseparation from the surroun<strong>di</strong>ng <strong>RC</strong> frame, as already illustrated. Equivalentstrut concept was first introduced by Polyakov (1956); first models based onthis concept were aimed at evaluating the increase in the stiffness <strong>of</strong> a framedue to the presence <strong>of</strong> a masonry infill panel by experimentally calibrating thewidth <strong>of</strong> the equivalent strut, which was usually assumed to have the samethickness and the same compressive elastic modulus <strong>of</strong> the panel (e.g., Holmes,1961; Stafford Smith, 1966; Mainstone, 1971).However, equivalent strut models allow to simulate the lateral force<strong>di</strong>splacementbehaviour <strong>of</strong> an infilled frame in a wide range <strong>of</strong> loa<strong>di</strong>ng, bymeans <strong>of</strong> an appropriate characterization <strong>of</strong> the strut force-<strong>di</strong>splacementrelationship (usually implicitly referring to a <strong>di</strong>agonal cracking failuremechanisms). Several models were proposed, provi<strong>di</strong>ng not only the monotonicenvelop <strong>of</strong> the strut force-<strong>di</strong>splacement relationship, but also the rulesdescribing the hysteretic behaviour.


150 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>Figure 3.2.4.1. Single-strut model for infilled frames (Crisafulli, 1997)Once the strut force-<strong>di</strong>splacement relationship has been determined, it isassigned to <strong>di</strong>agonal truss elements (carrying load in compression) thatrepresent the infill panels in the numerical structural model. The most simpleway to model an infill panel by means <strong>of</strong> an equivalent strut is the use <strong>of</strong> asingle-strut model (see Figure 3.2.4.1). This approach allows to account for theaxial force variation in <strong>RC</strong> columns due to the interaction with the adjacentpanel.Nevertheless, a single-strut model is not able to fully capture the localinteraction between the panel and the adjacent <strong>RC</strong> elements, lea<strong>di</strong>ng, forinstance, to an increase in shear demand in columns. To this aim, multi-strutmodels were proposed, where the <strong>di</strong>agonal elements representing the infillpanel (i) connect points <strong>di</strong>fferent from the opposite corners, thus modelling theactual extension <strong>of</strong> the contact area, and (ii) are placed not only concentrically(i.e., parallel to the <strong>di</strong>agonal <strong>of</strong> the panel) but also eccentrically, thus effectivelyrepresenting the force demand in adjacent beams and columns (FEMA 356,2000).In spite <strong>of</strong> a not very higher computational and modelling effort, thesemodels allow to account for the influence <strong>of</strong> infills on the seismic behaviour <strong>of</strong>infilled <strong>RC</strong> structures in a quite more realistic way, not only at local but also atglobal level.


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 151In the following, main macro-models for the evaluation <strong>of</strong> behaviour <strong>of</strong>infilled <strong>RC</strong> frames are presented. The adequacy <strong>of</strong> <strong>di</strong>fferent models to pre<strong>di</strong>ctthe response <strong>of</strong> an infilled frame – depen<strong>di</strong>ng, for instance, on the stage <strong>of</strong>behaviour and the failure mechanism – is <strong>di</strong>scussed.Klingner and Bertero (1976)In (Klingner and Bertero, 1976), a simple single-strut model is proposed (seeFigure 3.2.4.2) based on experimental tests on 1/3 scale <strong>RC</strong> frames infilled withreinforced masonry units. However, in authors’ opinion, some <strong>of</strong> the results areapplicable to other panel materials as well.In this model, the monotonic envelop is represented by a linear elasticbranch up to the maximum strength followed by an exponential degra<strong>di</strong>ngcurve where the strength is proportional to e γv , where v is the axial deformationin the strut (compression is negative) and γ is a parameter expressing therapi<strong>di</strong>ty in strength deterioration; a tensile force <strong>di</strong>fferent from zero can beconsidered in tension, too.In cyclic field, no degradation <strong>of</strong> the skeleton curve is modelled. Theunloa<strong>di</strong>ng stiffness is constant, too, and equal to the elastic stiffness. Adegradation <strong>of</strong> the reloa<strong>di</strong>ng stiffness is modelled by assuming that the force<strong>di</strong>splacementreloa<strong>di</strong>ng joints the skeleton curve for a <strong>di</strong>splacement equal to themaximum <strong>di</strong>splacement previously attained, in compression or in tension.


152 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>Figure 3.2.4.2. Equivalent strut model proposed in (Klingner and Bertero, 1976)Panagiotakos and Far<strong>di</strong>s (1996)In the infill model proposed by Panagiotakos and Far<strong>di</strong>s (Panagiotakos andFar<strong>di</strong>s, 1996; Far<strong>di</strong>s, 1997) the monotonic envelope <strong>of</strong> the lateral force<strong>di</strong>splacementcurve is given by four branches:- the first branch corresponds to the linear elastic behaviour up to the firstcracking, and the stiffness is given byKG Aw wel= (3.2.4.1)hwwhere A w is the cross-sectional area <strong>of</strong> the infill panel, G w is the elasticshear modulus <strong>of</strong> the infill material and h w is the clear height <strong>of</strong> theinfill panel. Accor<strong>di</strong>ng to the authors, this assumption gives the bestagreement with experimental initial stiffness values reported byStyliani<strong>di</strong>s (1985) and Pires (1990).The shear cracking strength is given byF= τ A(3.2.4.2)cr cr wwhere τ cr is the shear cracking stress;


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 153- the second branch follows the first cracking, up to the point <strong>of</strong>maximum strength. The maximum strength is given byFmax= 1.30⋅ F(3.2.4.3)crand the correspon<strong>di</strong>ng <strong>di</strong>splacement is evaluated assuming that thesecant stiffness up to this point is given by Mainstone’s formula(Mainstone, 1971), that is, assuming an equivalent strut width given by:( ) 0.4−b = 0.175 λ h d(3.2.4.4)w h w wwhere d w is the clear <strong>di</strong>agonal length <strong>of</strong> the infill panel and λ h is thewell-known coefficient accounting for the ratio between stiffness <strong>of</strong>masonry panel and <strong>RC</strong> frame (Stafford Smith, 1966; Stafford Smith andCarter, 1969), given by:E t sin 2θw wλh= 4(3.2.4.5)4EcIphwwhere E w is the Young’s elastic modulus <strong>of</strong> the infill material, t w is thethickness infill panel, θ is the slope <strong>of</strong> <strong>di</strong>agonal <strong>of</strong> infill to horizontaland E c I p is the flexural stiffness <strong>of</strong> <strong>RC</strong> columns adjacent to the infillpanel.Similar to initial elastic stiffness, this assumption is based on thecomparison with experimental secant-to-maximum stiffness valuesreported in Styliani<strong>di</strong>s (1985) and Pires (1990).The authors also say that a representative value for the post-crackingtangent stiffness could be Kpost− cracking= 0.03⋅ Kel(Panagiotakos andFar<strong>di</strong>s, 1996);- the third branch is the post-capping degra<strong>di</strong>ng branch, up to the residualstrength. Its stiffness depends on the elastic stiffness through theparameter α:Ks<strong>of</strong>t= −α K(3.2.4.6)el


154 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>the value <strong>of</strong> this parameter has to be arbitrarily assumed. However, theauthors give some in<strong>di</strong>cation (Panagiotakos and Far<strong>di</strong>s, 1996): the range<strong>of</strong> values for a should be between 0.005 and 0.1, although a value <strong>of</strong> 0.1is unrealistically high (very brittle infill), while a value <strong>of</strong> 0.01 may bemore realistic yet still conservative (well constructed infill);- the fourth branch is the horizontal branch correspon<strong>di</strong>ng to the residualstrength. This strength is given byFres= β F(3.2.4.7)maxwith β between 0.05 and 0.1.In cyclic field, a degradation <strong>of</strong> the strength envelope (depen<strong>di</strong>ng oncumulated <strong>di</strong>splacement) and <strong>of</strong> unloa<strong>di</strong>ng and reloa<strong>di</strong>ng stiffness is modelled,through <strong>di</strong>fferent experimentally-calibrated parameters, allowing to model thepinching effect too.Figure 3.2.4.3. Lateral force-<strong>di</strong>splacement relationship <strong>of</strong> an infill panel, as proposed in (Far<strong>di</strong>s,1997)Authors provide a lateral force-<strong>di</strong>splacement relationship for the infill panel(see Figure 3.2.4.3) that may be employed in infill modelling through theequivalent strut concept, by simply projecting this relationship on the axis <strong>of</strong>the inclined strut.


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 155However, it is to be noted that in authors’ opinion (Far<strong>di</strong>s, 1997) it is notphysically appealing to adopt an equivalent strut approach for the calculation <strong>of</strong>the stiffness before cracking. At this stage, that is, for very low values <strong>of</strong> thelateral drift, the response <strong>of</strong> the infilled frame is not affected by non-linearitydue to the separation at the interface between the masonry panel and thesurroun<strong>di</strong>ng frame, which has not occurred yet. The behaviour <strong>of</strong> the infilledframe can be still considered as monolithic (Fiorato, 1970), and no trussmechanism has taken place yet. Hence, for instance, no significant variation <strong>of</strong>the axial load in adjacent <strong>RC</strong> columns (given by the presence <strong>of</strong> an equivalent<strong>di</strong>agonal strut) should be modelled.As a matter <strong>of</strong> fact, the simple expression assumed in this model for theevaluation <strong>of</strong> the elastic stiffness is based on the assumption that, under thelateral load, the panel deformation follows a pure shear behaviour.Crisafulli (1997)In (Crisafulli, 1997), two strut models with <strong>di</strong>fferent degree <strong>of</strong> refinementare proposed.A single strut model is proposed first, suitable for the evaluation <strong>of</strong> theglobal response <strong>of</strong> an infilled structure. In this model the strut resistance alsodepends on the expected failure mode <strong>of</strong> the panel. The hysteretic behaviour ismodelled through <strong>di</strong>fferent parameters influencing, for instance, the slope <strong>of</strong>unloa<strong>di</strong>ng or reloa<strong>di</strong>ng curves.Hence, a more refined multi-strut model is proposed, in order to achieve abetter representation <strong>of</strong> the effect <strong>of</strong> the masonry panel on the surroun<strong>di</strong>ngframe, depen<strong>di</strong>ng on the type <strong>of</strong> failure. When a <strong>di</strong>agonal tension cracking isexpected (usually followed by the compressive failure <strong>of</strong> the <strong>di</strong>agonal strut), seeFigure 3.2.4.4a, a model with three concentric struts is proposed.


156 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>(a)(b)(c)(d)Figure 3.2.4.4. Failure modes and correspon<strong>di</strong>ng multi-strut models: <strong>di</strong>agonal tension cracking(a), corner crushing (b), stepped shear sli<strong>di</strong>ng (c) and horizontal shear sli<strong>di</strong>ng (d) (Crisafulli,1997)


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 157In this model, the <strong>di</strong>stance h z is evaluated as z/2, where the contact length z,in turn, is evaluated accor<strong>di</strong>ng to (Stafford Smith 1966; Stafford Smith andCarter, 1969):πz = (3.2.4.8)2 ⋅λhIf a corner crushing is expected, see Figure 3.2.4.4b, the author proposes toadopt a model where the central strut is <strong>di</strong>vided into two parts with <strong>di</strong>fferentarea, in order to consider approximately the increase <strong>of</strong> axial stresses occurringin the corners <strong>of</strong> the panels. If a shear failure <strong>of</strong> the masonry panel by steppeddebon<strong>di</strong>ng <strong>of</strong> the mortar joint is expected, see Figure 3.2.4.4c, a model isproposed accounting separately for the compressive and shear behaviour <strong>of</strong>masonry using a double truss mechanism and a shear spring in each <strong>di</strong>rection.In this case h z is between z/2 and z/3. If a horizontal sli<strong>di</strong>ng shear failure isexpected the same model can be adopted mo<strong>di</strong>fying h z in h/2, see Figure3.2.4.4d.Of course, the definition <strong>of</strong> further parameters, compared with the previouslyillustrated single-strut model, is needed for the application <strong>of</strong> this kind <strong>of</strong>models.Chrysostomou et al., (2002)Chrysostomou et al. (2002) propose a multi-strut model with threeconcentric struts per <strong>di</strong>rection. The proposed force-<strong>di</strong>splacement relationshipdepends on parameters that have physical meaning and can be adapted toexperimental data. The effects <strong>of</strong> openings, lack <strong>of</strong> fit and interface con<strong>di</strong>tionscan also be modelled by assigning proper values to the model parameters. Incyclic field, strength and stiffness degradation is modelled.The position <strong>of</strong> the <strong>of</strong>f-<strong>di</strong>agonal struts depends on the contact length, whichis given as a function <strong>of</strong> parameter α (see Figure 3.2.4.5). Actually, accor<strong>di</strong>ngto authors, contact length should not have a unique and constant value duringthe analysis. Hence, the chosen value should best represent the final position <strong>of</strong>


158 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>plastic hinge formation in <strong>RC</strong> members due to interaction with the infill panel.Figure 3.2.4.5. Six-strut idealization <strong>of</strong> infill walls (Chrysostomou et al., 2002)Lateral force-<strong>di</strong>splacement relationships and stiffness for infill panel areprovided first. Hence, axial force-<strong>di</strong>splacement relationships and stiffness forthe central strut and for the <strong>of</strong>f-<strong>di</strong>agonal struts are evaluated. Obviously, thesum <strong>of</strong> the forces and stiffnesses <strong>of</strong> the three struts adds to the force andstiffness <strong>of</strong> the panel.The definition <strong>of</strong> axial force-<strong>di</strong>splacement relationships and stiffness for thecentral strut is aimed at reproducing the faster deterioration <strong>of</strong> the central<strong>di</strong>agonal part <strong>of</strong> the panel, either due to corner crushing or due to tensioncracking along the <strong>di</strong>agonal; following the deterioration <strong>of</strong> the compression<strong>di</strong>agonal, more load is carried by the <strong>of</strong>f-<strong>di</strong>agonal part <strong>of</strong> the panel. Therefore,parameters are defined that influence the force and stiffness <strong>di</strong>stributionbetween the central and lateral struts, thus allowing to model, for example, thecrushing <strong>of</strong> the central strut when the peak load <strong>of</strong> the infill panel is reached,which is usually the case for non-integral infilled frames (Liauw and Kwan,1984).Hence, axial force-<strong>di</strong>splacement relationships and stiffness for the <strong>of</strong>f<strong>di</strong>agonalstruts are evaluated. To this aim, the principle <strong>of</strong> virtual <strong>di</strong>splacementsis applied to evaluate the <strong>di</strong>stribution <strong>of</strong> forces between the central strut and the<strong>of</strong>f-struts, for each <strong>di</strong>splacement value


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 1593.3 EXPERIMENTAL BEHAVIOUR OF INFILLED <strong>RC</strong>STRUCTURESGlobal structural behaviour <strong>of</strong> a <strong>RC</strong> buil<strong>di</strong>ng is influenced by the presence <strong>of</strong>infill walls in <strong>di</strong>fferent ways: roughly, an increase in lateral stiffness and in baseshear capacity are observed. It is to be noted that, when describing the influence<strong>of</strong> infills on the lateral force-<strong>di</strong>splacement global response, the influence <strong>of</strong> theabove illustrated shear failure mechanisms in columns or beam-column jointswill be neglected, because considered as the result <strong>of</strong> a local interaction.The increase in lateral stiffness leads to a mo<strong>di</strong>fication <strong>of</strong> the dynamicproperties, resulting in a lower period <strong>of</strong> vibration (see Section 3.4).The increase in lateral strength should reasonably have a beneficial effect onseismic capacity, but the brittle post-peak behaviour generally shown by infillpanels is reflected in a brittle global lateral force-<strong>di</strong>splacement response. Ageneral reduction in global <strong>di</strong>splacement demand is observed, even though thisdemand tends to concentrate at the bottom <strong>of</strong> the structure.These considerations are valid if the infill panels are regularly placedthroughout the structure, in plan and in elevation. Otherwise, the presence <strong>of</strong>infill walls may lead to a detrimental localization <strong>of</strong> inelastic <strong>di</strong>splacementdemand (see Figures 3.3.1, 3.3.2), resulting in less ductile (less energy<strong>di</strong>ssipating)and potentially catastrophic collapse mechanisms.This is reflected by modern seismic code (e.g., EC8-part I (CEN, 2004a) atSection 4.3.6), which prescribe to avoid strong irregularities in <strong>di</strong>stribution <strong>of</strong>infills, both in plan and elevation, or – if such irregularities are present – toaccount for them by conventionally increasing the seismic demand (e.g.,increasing the seismic action effects in the vertical elements <strong>of</strong> the storey wherea drastic reduction <strong>of</strong> infills is present, compared to the others).Moreover, the own damage <strong>vulnerability</strong> <strong>of</strong> infill elements is also consideredwhen assessing seismic safety. To this aim, for Damage Limitation Limit Statethe interstorey drift ratio is limited to 0.005 if “non-structural elements <strong>of</strong> brittlematerials attached to the structure” are present.However, it is worth noting that the influence <strong>of</strong> infills on structural


160 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>behaviour cannot be analyzed without considering the seismic behaviour thatthe correspon<strong>di</strong>ng bare structure would show, that is, the design procedure.Figure 3.3.1. Torsional collapse mechanism due to an irregular infill <strong>di</strong>stribution in plan (Bragaand Petrangeli, 1976)


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 161Figure 3.3.2. S<strong>of</strong>t-storey collapse mechanism due to an irregular infill <strong>di</strong>stribution in elevation(Braga and Petrangeli, 1976)Literature does not <strong>of</strong>fer many experimental results showing the behaviour<strong>of</strong> <strong>RC</strong> structures with infill panels. In this Section, main stu<strong>di</strong>es from literatureare reported, illustrating the influence <strong>of</strong> infills on stiffness, strength andcollapse mechanism <strong>of</strong> <strong>RC</strong> structures.


162 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>Negro and Verzeletti (1996)Negro and Verzeletti (1996) carried out pseudo-dynamic tests on a full-scalefour-storey <strong>RC</strong> buil<strong>di</strong>ng (see Figure 3.3.3) designed accor<strong>di</strong>ng to Eurocodes 2and 8, in ductility class High – complying the weak beam/strong columnprinciple – for a PGA equal to 0.3g. Three tests were carried out, withoutinfills, with uniformly <strong>di</strong>stributed infills and with infills in all storey but thefirst, respectively.(a)(b)Figure 3.3.3. Layout <strong>of</strong> the tested frame (Negro and Verzeletti, 1996)An artificially generated earthquake derived from the 1976 Friuli earthquakewas employed in the tests, with nominal acceleration 50% larger than the valueadopted in design (PGA=1.5x0.3=0.45g).During the first test carried on the bare frame the structure performed asexpected, respecting the weak beam/strong column mechanism. The damagewas limited and uniformly <strong>di</strong>stributed. A decrease in frequency <strong>of</strong> vibrationbefore and after the test was observed (from 1.78 to 0.82 Hz).


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 163Figure 3.3.4. Uniformly infilled frame (Negro and Verzeletti, 1996)After the first test, infill walls were uniformly placed throughout thestructure (see Figure 3.3.4). The fundamental frequency changed to 3.34 Hz.During the test, the masonry panels at the first and second storeys werecompletely destroyed, while the panels at the third storey suffered extensivedamage, and the ones at the upper storey remained almost intact, thushighlighting a non-uniform interstorey <strong>di</strong>splacement demand <strong>di</strong>stribution.After the second test, the masonry panels were demolished and replacedwith new ones, leaving the first storey bare (see Figure 3.3.5). The fundamentalfrequency was 1.6 Hz. The test resulted in s<strong>of</strong>t-storey mechanism, characterizedby a concentration <strong>of</strong> drift at the first storey, with some damage suffered by thepanels <strong>of</strong> the second storey only.


164 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>Figure 3.3.5. S<strong>of</strong>t-storey infilled frame (Negro and Verzeletti, 1996)If maximum base share values from the three tests are compared, it isobserved that the maximum base shear for the s<strong>of</strong>t-storey structure is onlyslightly larger than that <strong>of</strong> the bare frame, while the maximum base shear forthe uniformly infilled frame was almost 50% than that <strong>of</strong> the bare frame, thushighlighting the noticeable contribution <strong>of</strong> infills to the lateral strength <strong>of</strong> thestructure.The <strong>di</strong>stribution <strong>of</strong> <strong>di</strong>splacement demand along the height <strong>of</strong> the structure inthe three tests can be observed from the interstorey drift pr<strong>of</strong>iles (see Figure3.3.6).If compared with the bare structure, presence <strong>of</strong> uniformly <strong>di</strong>stributed infillsleads to a decrease in <strong>di</strong>splacement demand, but also to a concentration <strong>of</strong> thisdemand in lower storeys. The worst behaviour is shown by the s<strong>of</strong>t-storeystructure, where the highest <strong>di</strong>splacement demand at the first storey and themost irregular demand <strong>di</strong>stribution are observed, compared with other tests.


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 165Figure 3.3.6. Maximum interstorey drift pr<strong>of</strong>iles (Negro and Verzeletti, 1996)Pinto et al. (2002)Pseudo-dynamic tests were carried out within the ICONS project on planefour-storey three-bay <strong>RC</strong> frames, with and without infills. The frames wererepresentative <strong>of</strong> <strong>existing</strong> European <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>; they were designed for abase shear coefficient equal to 0.08, with no compliance with Capacity Designprinciples. In the infilled frame, masonry panels were uniformly <strong>di</strong>stributedalong the height <strong>of</strong> the structure and openings were present in two <strong>of</strong> the threebays (see Figure 3.3.7).


166 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>Figure 3.3.7. Plan and elevation view <strong>of</strong> the infilled <strong>RC</strong> frame


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 167100010004 th storey800[kN]4 th storey800[kN]600600400400200200[mm]0-80 -60 -40 -20 0 20 40 60 80-200[mm]0-80 -60 -40 -20 0 20 40 60 80-200-400-400-600-600-800-800-1000-1000100010003 rd storey800[kN]3 rd storey800[kN]600600400400200200[mm]0-80 -60 -40 -20 0 20 40 60 80-200[mm]0-80 -60 -40 -20 0 20 40 60 80-200-400-400-600-600-800-800-1000-1000100010002 nd storey800[kN]2 nd storey800[kN]600600400400200200[mm]0-80 -60 -40 -20 0 20 40 60 80-200[mm]0-80 -60 -40 -20 0 20 40 60 80-200-400-400-600-600-800-800-1000-1000100010001 st storey800[kN]1 st storey800[kN]600600400400200200[mm]0-80 -60 -40 -20 0 20 40 60 80-200[mm]0-80 -60 -40 -20 0 20 40 60 80-200-400-400-600-600-800-800-1000(a)(b)Figure 3.3.8. Comparison between interstorey <strong>di</strong>splacement-shear experimental relationships forbare (a) and infilled (b) <strong>RC</strong> frames-1000


168 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>Input signals for pseudo-dynamic tests were artificial accelerogramscharacterized by PGA values correspon<strong>di</strong>ng to <strong>di</strong>fferent return periods.In Figure 3.3.8 interstorey <strong>di</strong>splacement-shear experimental relationships forbare and infilled frames for the same seismic intensity (given by a PGAcorrespon<strong>di</strong>ng to a 975 years return period) are reported.The bare frame collapsed under a column-sway mechanism at the thirdstorey, where the maximum <strong>di</strong>splacement demand can be observed.The infilled frame showed a noticeable increase in stiffness and strength,compared with the bare one, resulting in a severe decrease in <strong>di</strong>splacementdemand, which was higher at lower storeys.Dolce et al. (2005)Dolce et al. (2005) carried out shake table tests on 1/3.3-scale plane <strong>RC</strong>frames (see Figure 3.3.9), designed accor<strong>di</strong>ng to the European seismic code(EC8–part I) for low-ductility and 0.15 g PGA seismic intensity, in order tostudy their behaviour with or without <strong>di</strong>fferent kinds <strong>of</strong> energy <strong>di</strong>ssipating andre-centring bracing systems. Two unretr<strong>of</strong>itted specimens were tested: a bareframe and a masonry infilled frame.Figure 3.3.9. Geometrical characteristic <strong>of</strong> 1/3.3 scale <strong>RC</strong> structural models (Dolce et al., 2005)


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 169Both models were subjected to two alternate series <strong>of</strong> tests, namely seismictests and random tests. <strong>Seismic</strong> tests were aimed at evaluating the structuralresponse under seismic motion, represented by an artificially generatedaccelerogram <strong>of</strong> increasing intensity (PGA). Random tests were aimed atevaluating the frequency <strong>of</strong> vibration. Hence, both the equivalent (during theseismic excitation) and the fundamental (after the seismic excitation, under lowintensity) frequencies <strong>of</strong> vibration were evaluated. The latter providesinformation about the damage suffered by the structure during the seismicevent, but the former is <strong>of</strong> importance for <strong>di</strong>splacement-based methods.Structural collapse occurred for 0.48 and 0.9g PGA for bare and infilledmodel, respectively, thus highlighting the beneficial role <strong>of</strong> infill elements, ifuniformly <strong>di</strong>stributed and accurately realized.Figure 3.3.10. Frequency <strong>of</strong> vibration due to seismic tests with increasing intensity for bareframe and masonry infilled frame (Dolce et al., 2005)


170 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>Figure 3.3.10 shows the changes in the frequency <strong>of</strong> vibration due to seismictests with increasing intensity for both models. Comparing the frequencies <strong>of</strong>vibration <strong>of</strong> the two models the stiffness increase due to infill presence isclearly shown by an initial fundamental frequency about 2.5 times higher (9.03and 3.65 Hz, respectively). The decrease in frequency <strong>of</strong> vibration was almostlinear for the bare model, up to collapse. For the infilled model, the decreasewas linear at lower seismic intensities but followed a power law after asignificant damage in infill panels occurred. For both models the gap betweenequivalent and fundamental frequency <strong>of</strong> vibration tends to increase during thetests, due to the progression <strong>of</strong> structural and non-structural damage.Figure 3.3.11 shows the pr<strong>of</strong>iles <strong>of</strong> maximum absolute <strong>di</strong>splacements andmaximum interstorey drifts. Comparing the maximum <strong>di</strong>splacement an<strong>di</strong>nterstorey drift demand for each seismic intensity level, two main conclusionscan be drawn:- the ro<strong>of</strong> drift at collapse was greater than 3% for the bare model andabout equal to 2.5% for the infilled model. Hence, the <strong>di</strong>splacementcapacity <strong>of</strong> the infilled structure was substantially lower;- an evident damage concentration at the first storey, with increasingseismic intensity, was observed. Authors highlighted that thisconcentration is a consequence <strong>of</strong> the constant resistance <strong>of</strong> the infilledframe along the height.


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 171Figure 3.3.11. Pr<strong>of</strong>iles <strong>of</strong> maximum absolute <strong>di</strong>splacements and maximum interstorey drifts forbare frame and masonry infilled frame (Dolce et al., 2005)


172 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>Shing et al. (2009)Shing et al. (2009) carried out shake-table tests on two 2/3-scale, three-story,two-bay, infilled <strong>RC</strong> frames (see Figure 3.3.12). One was tested without retr<strong>of</strong>itmeasures and the other had infill strengthened in the first and second stories.Results from the test on the unreinforced specimen are reported herein.The structure was designed as an exterior frame <strong>of</strong> a <strong>RC</strong> buil<strong>di</strong>ng designedfor gravity loads only, accor<strong>di</strong>ng to obsolete code prescriptions. Infills wereuniformly <strong>di</strong>stributed along the height, and in one bay openings were present.(a)(b)Figure 3.3.12. Elevation view <strong>of</strong> tested frame (a) and shake table test setup (b) (Shing et al.,2009)In the shake-table tests, the specimen was subjected to a sequence <strong>of</strong> scaledground motion records (Gilroy from the 1989 Loma Prieta earthquake and theNS component <strong>of</strong> the 1940 El Centro earthquake) , see Figure 3.3.13.Damage was localized at the bottom storey. The weak first storey isolatedthe second storey from severe seismic force. Shear failure developed in themiddle column during the 120% Gilroy, see Figure 3.3.14b. Severe damagewith shear failures developed in the exterior columns occurred when thespecimen was subjected to the 250% El Centro, see Figure 3.3.14d.


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 173Figure 3.3.13. First storey interstorey drift-shear demand for <strong>di</strong>fferent ground motion intensities(Shing et al., 2009)Figure 3.3.14. First storey damage for <strong>di</strong>fferent ground motion intensities (Shing et al., 2009)


174 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>Pujol and Fick (2010)Pujol and Fick (2010) carried out experimental tests on a full scale threestorey<strong>RC</strong> structure designed for gravity loads only. The structure had two baysin the <strong>di</strong>rection <strong>of</strong> loa<strong>di</strong>ng and one bay in the opposite <strong>di</strong>rection. Tests were firstcarried out on the bare structures. Hence, brick infill walls were added to thedamaged structure, which was tested again. The load was applied in<strong>di</strong>splacement control at the top slab. Hence, loads at the other two levels wereadjusted to 2/3 (at the floor <strong>of</strong> the third storey) and 1/3 (at the floor <strong>of</strong> thesecond storey) <strong>of</strong> the load applied at the top level, thus imposing step by step afixed linear shape <strong>of</strong> the lateral load pattern. Following this procedure,<strong>di</strong>splacement cycles with increasing amplitude were applied to the structure.The bare structure initially had a fundamental period <strong>of</strong> vibration equal to0.5 s. The test on this structure was stopped at a ro<strong>of</strong> drift <strong>of</strong> 3%. For a ro<strong>of</strong>drift equal to 2.8% a punching shear failure took place at the connectionbetween a column and the slab at the second storey, where the largestinterstorey drift demand was observed.Hence, the structure was mo<strong>di</strong>fied ad<strong>di</strong>ng unreinforced brick walls. Thefundamental period <strong>of</strong> vibration <strong>of</strong> the (partially) infilled structure was equal to0.2 s, thus highlighting the higher stiffness due to the ad<strong>di</strong>tion <strong>of</strong> infill walls.Then another experimental test was carried out, imposing <strong>di</strong>splacement cycleswith increasing amplitude. Also in this case the largest interstorey drift demandwas observed at the second storey.Results from both tests are compared in Figure 3.3.15. The increase instrength due to the ad<strong>di</strong>tion <strong>of</strong> infill walls is clearly shown. Authors highlightthat this noticeable increase remains effective up to 1.5% <strong>of</strong> ro<strong>of</strong> drift.An image <strong>of</strong> the tested structure is reported in Figure 3.3.16.


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 175Figure 3.3.15. Comparison <strong>of</strong> results from first and second test (Pujol and Fick, 2010)Figure 3.3.16. Tested structure after the second test (Pujol and Fick, 2010)


176 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>3.4 ANALYTICAL INVESTIGATION OF ELASTIC PERIOD OFINFILLED <strong>RC</strong> MRF BUILDINGSIt has been highlighted how the presence <strong>of</strong> infill walls leads to a higherlateral stiffness <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>, resulting in a mo<strong>di</strong>fication <strong>of</strong> dynamicproperties, that is, in a lower period <strong>of</strong> vibration.In this Section, this issue is investigated from a numerical standpoint, bymeans <strong>of</strong> modal analyses carried out on 3D numerical <strong>RC</strong> Moment ResistingFrame (MRF) buil<strong>di</strong>ng models, varying structure morphology (height, surfacearea, ratio between plan <strong>di</strong>mensions) and infill characteristics. Simplifiedformulas based on regression analysis <strong>of</strong> obtained numerical data are presentedand <strong>di</strong>scussed. These relationships are also compared with similar literaturenumerical expressions and empirical data from experimental measurements on<strong>existing</strong> <strong>buil<strong>di</strong>ngs</strong>.The results illustrated in this Section were published in (Ricci et al., 2010).3.4.1. The period <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>In an equivalent static approach, the evaluation <strong>of</strong> seismic forces is based onthe period <strong>of</strong> vibration <strong>of</strong> the structure. However, the period <strong>of</strong> vibration is notan unique and constant characteristic. The stiffness degradation experienced bythe structure during the response to a seismic event causes the “lengthening” <strong>of</strong>the period: as the degree <strong>of</strong> damage (both structural and non-structural)increases, the period increases too. In order to obtain a realistic estimate <strong>of</strong>seismic demand, many authors propose to evaluate the period <strong>of</strong> vibrationbased on empirical data from <strong>existing</strong> <strong>buil<strong>di</strong>ngs</strong> subjected to earthquakes.<strong>Seismic</strong> codes <strong>of</strong>ten adopt formulas obtained in this way.Moreover, during last years numerical and experimental efforts were madein order to evaluate period-height relationships for <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> accounting forthe stiffness contribution <strong>of</strong> infill walls.In this Section, empirical-based expressions for evaluating the period <strong>of</strong>vibration <strong>of</strong> <strong>RC</strong> MRF SW <strong>buil<strong>di</strong>ngs</strong> are illustrated; moreover, the description <strong>of</strong>literature experimental campaigns and numerical models aimed at the


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 177assessment <strong>of</strong> dynamic behaviour <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infill walls is reported.3.4.1.1 Empirical estimate <strong>of</strong> period <strong>of</strong> <strong>RC</strong> MRF <strong>buil<strong>di</strong>ngs</strong>Expression proposed by Eurocode 8 (CEN, 2004a) and first appeared inATC3-06 (ATC, 1978):T0.75= CtH(3.4.1.1)is derived from Rayleigh’s method, and C t is calibrated in order to achieve thebest fit to experimental data. ATC3-06, based on Gates and Foth’s study(1978), proposed for this coefficient the value 0.025 as a lower limit forevaluating the period <strong>of</strong> vibration <strong>of</strong> <strong>RC</strong> MRF <strong>buil<strong>di</strong>ngs</strong>. The evaluation <strong>of</strong> thisvalue was based on periods computed from motions recorded in 14 <strong>buil<strong>di</strong>ngs</strong>during the San Fernando earthquake in 1971. The value <strong>of</strong> C t was subsequentlychanged into 0.030, that is, 0.074 if the height is expressed in metres, verysimilar to the value 0.075 adopted by EC8:0.75T = 0.075H(3.4.1.2)In (Bertero et al., 1988), starting from an accurate analysis <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong>stu<strong>di</strong>ed by Gates and Foth, the authors partially mo<strong>di</strong>fy their database andpropose to assume C t equal to 0.035, as a lower bound for period <strong>of</strong> vibration <strong>of</strong>the only structural components <strong>of</strong> the buil<strong>di</strong>ng, correspon<strong>di</strong>ng to the stage whenthe stiffness contribution <strong>of</strong> non-structural elements can be considered to benegligible due to their damage level.In (Goel and Chopra, 1997a) the authors calibrate numerical values <strong>of</strong>coefficients α and β in the expression:T= α H β(3.4.1.3)based on strong motion accelerograms from 27 <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> recorded during<strong>di</strong>fferent seismic events. The best agreement with all experimental data, inaverage terms, is given by:0.90T = 0.053H(3.4.1.4)


178 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>3.4.1.2 Empirical estimate <strong>of</strong> period <strong>of</strong> <strong>RC</strong> SW <strong>buil<strong>di</strong>ngs</strong>In <strong>RC</strong> SW <strong>buil<strong>di</strong>ngs</strong> the lateral load resistance is mainly provided by shearwalls. Hence, a significant contribute to the overall lateral stiffness, too, isgiven by walls. The period <strong>of</strong> vibration <strong>of</strong> these <strong>buil<strong>di</strong>ngs</strong> can be evaluated withgood approximation as the period <strong>of</strong> an equivalent cantilever (Goel and Chopra,1998). If the only shear deformability is accounted for, this period is equal to:T = 4mHκ ⋅GHAS(3.4.1.5)where m H is the uniformly <strong>di</strong>stributed mass per unit height, κ is a factoraccounting for the shape <strong>of</strong> the transverse section (equal to 5/6 for a rectangularsection), G is the shear elastic modulus and A S is the area <strong>of</strong> the transversesection (Goel and Chopra, 1997b). The area A S can be expressed as the product<strong>of</strong> the thickness t by L x(y) , that is the plan <strong>di</strong>mension <strong>of</strong> the equivalent cantileverparallel to the considered <strong>di</strong>rection along which the fundamental period isevaluated:T 4m H Hκ⋅G t ⋅ L LHx(y)= = αx(y)x(y)(3.4.1.6)Different codes adopt this kind <strong>of</strong> formula, with an experimentally calibratedvalue for α. In (ATC, 1978) it is proposed to assume α equal to 0.05 for<strong>di</strong>mensions expressed in feet, that is, 0.09 for <strong>di</strong>mensions in metres. In (Goeland Chopra, 1998) the authors propose the following expression:ρ H HTx(y)= 40= ακ⋅G A Ae,x(y)e,x(y)(3.4.1.7)where ρ is the average mass density, defined as the ratio between the totalbuil<strong>di</strong>ng mass and the total buil<strong>di</strong>ng volume, andAeis the equivalent sheararea, defined as the percentage on the total plan area <strong>of</strong> A e , which accounts forthe presence <strong>of</strong> several uncoupled shear walls, considering also their flexural


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 179deformability (Goel and Chopra, 1997b). Based on Eq. (3.4.1.7), the authorscarry out a regression analysis on 17 measured period values from 9 <strong>RC</strong> SW<strong>buil<strong>di</strong>ngs</strong> subjected to seismic excitations. The best agreement with allexperimental data, independent <strong>of</strong> the peak ground acceleration experienced bythe <strong>buil<strong>di</strong>ngs</strong>, is given by:T = 0.0077H(3.4.1.8)AeMoreover, the authors point out the poor correlation between H / D and themeasured period, where D is the plan <strong>di</strong>mension parallel to the <strong>di</strong>rection alongwhich the period is evaluated.3.4.1.3 Empirical estimate <strong>of</strong> period <strong>of</strong> infilled <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>The above illustrated formulas for estimating the fundamental period <strong>of</strong> <strong>RC</strong><strong>buil<strong>di</strong>ngs</strong> are based on experimental data from USA structures subjected toearthquakes <strong>of</strong> <strong>di</strong>fferent intensity. Generally speaking, European <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>are significantly <strong>di</strong>fferent from USA <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>, both in terms <strong>of</strong> structuralsystem and non-structural elements (such as internal and external infills).During last years, experimental stu<strong>di</strong>es were carried out aimed at theassessment <strong>of</strong> dynamic properties <strong>of</strong> this type <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong>, especially inMe<strong>di</strong>terranean area. Measurement techniques used in these stu<strong>di</strong>es were mainlybased on low amplitude motion, that is, microtremors or ambient noise.Therefore, due to low intensity <strong>of</strong> the source <strong>of</strong> excitation, measured periodsrepresent with good approximation the linear dynamic properties <strong>of</strong> thestructures, since phenomenon <strong>of</strong> period lengthening – caused by non-linearity inbehaviour <strong>of</strong> structural and non-structural materials and components (such asinfill walls, too) – should not have occurred during the experimentalmeasurements. Empirical relationships proposed in these stu<strong>di</strong>es highlight agood agreement with each other.These relationships provide period values much lower than previouslyillustrated works (e.g. Gates and Foth 1978; Goel and Chopra, 1997a; Goel and


180 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>Chopra, 1998; Bertero et al., 1988). Moreover, experimental data show the highinfluence <strong>of</strong> infill presence on period <strong>of</strong> vibration (Oliveira and Navarro, 2010).In (Oliveira, 2004) a database is presented, made up <strong>of</strong> measured periods <strong>of</strong>vibration from Portuguese <strong>buil<strong>di</strong>ngs</strong>, evaluated by means <strong>of</strong> microtremors. Themajority <strong>of</strong> these <strong>buil<strong>di</strong>ngs</strong> are located on firm soil types. Among them, theauthors select 130 <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infill brick walls, obtaining that the bestfit to experimental period data is given byTx= 0.012H and Ty= 0.013H , inlongitu<strong>di</strong>nal and transversal <strong>di</strong>rections respectively. If an interstorey heightequal to 3 meters is assumed, these relationships change into Tx= 0.037N andTy= 0.039N , where N is the total number <strong>of</strong> storeys.Although on a smaller number <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong>, the same authors also show thatthe absence <strong>of</strong> infill walls leads to a period <strong>of</strong> vibration at least double, for thesame height, compared with <strong>buil<strong>di</strong>ngs</strong> where infill walls are present.In (Navarro and Oliveira, 2006), based on a subset <strong>of</strong> 37 <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> withinfill walls from the same database, monitored with very sensitive sensors, theauthors evaluate the period <strong>of</strong> vibration as T = ( 0.043 ± 0.001)N .In (Gallipoli et al., 2010) empirical data for periods <strong>of</strong> vibration <strong>of</strong> 244 <strong>RC</strong><strong>buil<strong>di</strong>ngs</strong> located in Italy and in Balkan area, evaluated by means <strong>of</strong> ambientnoise measurements, are presented. The period-height relationship is given byT 0.016H = .In (Oliveira and Navarro, 2010) further expressions proposed by <strong>di</strong>fferentauthors for evaluating the fundamental period are presented, based onexperimental data from <strong>buil<strong>di</strong>ngs</strong> located in Me<strong>di</strong>terranean area (France andSpain), having in common a <strong>RC</strong> structural system with infill wall panels.Accor<strong>di</strong>ng to these expressions – also evaluated by means <strong>of</strong> low amplitudemotion measurement techniques – fundamental period is included, again,between 0.015H and 0.017H .


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 1813.4.1.4 Numerical estimate <strong>of</strong> period <strong>of</strong> infilled <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>In (Crowley and Pinho, 2006) the authors propose period-heightrelationships for <strong>RC</strong> MRF <strong>buil<strong>di</strong>ngs</strong> with infill walls, considering both grossand yield stiffness <strong>of</strong> <strong>RC</strong> sections. These equations are obtained as linearregressions <strong>of</strong> period values evaluated by modelling eleven case-study <strong>buil<strong>di</strong>ngs</strong>designed only for vertical loads or accor<strong>di</strong>ng to obsolete seismic codes. Thepresence <strong>of</strong> infills is accounted for by means <strong>of</strong> equivalent <strong>di</strong>agonal struts,accor<strong>di</strong>ng to (Liauw and Kwan, 1984). The presence <strong>of</strong> openings is taken intoaccount, too, by means <strong>of</strong> the expressions proposed in (Bertol<strong>di</strong> et al., 1994).For uncracked infilled <strong>buil<strong>di</strong>ngs</strong>, if a gross stiffness for <strong>RC</strong> element sections isconsidered, the following expression is obtained:Te= 0.038H(3.4.1.9)For cracked <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>, the yield period – evaluated assuming a crackedstiffness for <strong>RC</strong> element sections – is given by:Ty= 0.055H(3.4.1.10)Masi and Vona (2008), by means <strong>of</strong> a simulated design procedure, elaboratestructural models <strong>of</strong> a class <strong>of</strong> infilled <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>. The design procedure isdefined for gravity loads only. The stiffness reduction due to the cracking <strong>of</strong>member sections is evaluated by adopting <strong>di</strong>fferent values <strong>of</strong> the effectiveinertia. Infills are represented by equivalent <strong>di</strong>agonal struts accor<strong>di</strong>ng to(Mainstone, 1974); presence <strong>of</strong> openings is not taken into account. Thevariability in the <strong>di</strong>stribution <strong>of</strong> infill elements is considered too. A totalnumber <strong>of</strong> 648 analyses is performed. For infilled <strong>buil<strong>di</strong>ngs</strong> with gross oryielded inertia <strong>of</strong> <strong>RC</strong> members, respectively, the period (along the transversal<strong>di</strong>rection) is given by:Te= 0.050H(3.4.1.11)andTy= 0.055H(3.4.1.12)


182 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>Kose (2009), through a sensitivity analysis, finds out that the mainparameters affecting the period <strong>of</strong> vibration <strong>of</strong> an infilled <strong>RC</strong> buil<strong>di</strong>ng,accounting also for the presence <strong>of</strong> shear walls, are the percentage <strong>of</strong> shearwalls on the total floor area, the percentage <strong>of</strong> infill walls on the total panel areaand the number <strong>of</strong> bays (in order <strong>of</strong> importance). Amanat and Hoque (2006)also perform a sensitivity analysis on the period <strong>of</strong> vibration <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>with infills, conclu<strong>di</strong>ng that the main parameters affecting the period, besidesthe height, are the number and the length <strong>of</strong> bays and the amount <strong>of</strong> infills,while the stiffness <strong>of</strong> <strong>RC</strong> members does not have a great influence.3.4.2. Modelling <strong>of</strong> infill stiffnessBased on the consideration that in integral infilled <strong>RC</strong> frames, in a firstphase, for very low values <strong>of</strong> lateral <strong>di</strong>splacement, the initial response is givenby a monolithic behaviour <strong>of</strong> the whole composite system, ensured by bondcapacities at the interface between the panel and the frame (see Section 3.2), in(Fiorato et al., 1970) the evaluation <strong>of</strong> the initial stiffness <strong>of</strong> the infilled frame isbased on the linear elastic response <strong>of</strong> the equivalent composite cantileverbeam. This response results from the interaction between the two elements, andthe applied lateral load is <strong>di</strong>stributed between them based on the ratio betweentheir stiffness. Authors evaluate the overall <strong>di</strong>splacement assuming that theflexural deformability is due to the monolithic response <strong>of</strong> the compositesystem, while the shear deformability contribution is only due to the infillpanel. Therefore, the resulting stiffness is given by:K =11 1+GwAw3EI3h hw(3.4.2.1)where A w is the cross-sectional area <strong>of</strong> the infill panel, G w is the elastic shearmodulus <strong>of</strong> the infill material, h w is the clear height <strong>of</strong> the infill panel, E is theelastic Young’s modulus <strong>of</strong> the frame-panel composite material, I is the


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 183moment <strong>of</strong> inertia <strong>of</strong> the total frame-panel cross section and h is the <strong>di</strong>stancefrom top <strong>of</strong> base beam to mid-height <strong>of</strong> the first-storey beam. The theoreticalvalue <strong>of</strong> the initial stiffness evaluated accor<strong>di</strong>ng to Eq. (3.4.2.1) seems to wellapproximate, in the early range <strong>of</strong> loa<strong>di</strong>ng, the lateral load-deflection curves <strong>of</strong>infilled frames tested by the authors (Fiorato et al., 1970).The approach proposed in (Far<strong>di</strong>s, 1997), see Eq. 3.2.4.1 at Section 3.2.4, isquite similar, from a theoretical standpoint. In this case it is assumed that, underthe lateral load, the panel deformation follows a pure shear behaviour, and nointeraction between the panel and the surroun<strong>di</strong>ng elements is taken intoaccount. The infill is modelled as a system in parallel with the <strong>RC</strong> frame.Many other models for the evaluation <strong>of</strong> the infill stiffness, based on theequivalent strut approach (see Section 3.2.4), are proposed in literature.Holmes (1961) arbitrary proposes to assume this width equal to 1/3 <strong>of</strong> the<strong>di</strong>agonal length. In (Mainstone, 1971), the author, based on experimental data,proposes <strong>di</strong>fferent formulas expressing the width <strong>of</strong> the equivalent strutcorrespon<strong>di</strong>ng to secant stiffness at first cracking and ultimate strengthcon<strong>di</strong>tions. In particular, the equivalent strut width for the evaluation <strong>of</strong> thesecant stiffness to the first cracking is given by Eq. 3.2.4.4 at Section 3.2.4.In (Paulay and Priestley, 1992) the authors assume that the width <strong>of</strong> theequivalent strut is equal to 0.25 times the <strong>di</strong>agonal length <strong>of</strong> the panel. Thisvalue is proposed in order to estimate the secant stiffness correspon<strong>di</strong>ng to alateral load equal to 50% <strong>of</strong> the maximum load capacity <strong>of</strong> the infilled frame,that is, after separation between masonry panel and <strong>RC</strong> frame has occurred. Asa matter <strong>of</strong> fact, in authors’ opinion the evaluation <strong>of</strong> the period in a seismicdemand assessment should be based on the structural stiffness correspon<strong>di</strong>ng tothis stage.Liauw and Kwan (1984) build up numerical models <strong>of</strong> non-integral infilledframes, thus deducing that the width <strong>of</strong> the equivalent strut has to be expressedas a function <strong>of</strong>hwcos θ. Then, based on experimental stiffness values given in(Barua and Mallick, 1977), the authors find out the following expression:


184 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>bw0.95hwcos θ=λhw(3.4.2.2)The experimental data fitted by Eq. (3.4.2.2) are evaluated accor<strong>di</strong>ng to theprocedure proposed in (Stafford Smith, 1967). In this work the author describesa typical load-<strong>di</strong>splacement curve <strong>of</strong> an infilled frame. In particular, heidentifies two zones: a first one characterized by an irregular behaviour, wherethe stiffness is considered to be unpre<strong>di</strong>ctable, and a second one where theresponse is quasi-linear (see Figure 3.4.2.1). First phase is essentially due to theinitial lack <strong>of</strong> fit between the panel and the frame, while during the secondphase a firm bearing develops between the two elements. Stiffness <strong>of</strong> theinfilled frame, accor<strong>di</strong>ng to author’s proposal, is evaluated in the latter range <strong>of</strong>loa<strong>di</strong>ng. The considerations reported by the author clearly refer to the behaviour<strong>of</strong> non-integral infilled frames. The value calculated by means <strong>of</strong> the abovedescribed procedure can be reasonably considered to be lower than the initialstiffness shown by an integral infilled frame.Figure 3.4.2.1. Schematic representation <strong>of</strong> load-deflection curves recorded in tests (Baruaand Mallick, 1977)Above described models are compared in Figure 3.4.2.2. A one-bay one-storeyinfilled frame is considered, with (300×300)mm columns and a (300×500)mmbeam, and a (4.00×3.00)m infill; panel thickness is assumed equal to 200 mm.Elastic Young’s modulus <strong>of</strong> concrete is given equal to E c =30000 MPa. Lateralstiffness <strong>of</strong> the infilled frame is reported, accor<strong>di</strong>ng to the illustrated formulas,


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 185depen<strong>di</strong>ng on the shear elastic modulus <strong>of</strong> the infill G w . The ratio G w /E w isgiven equal to 0.30.Expressions proposed in (Far<strong>di</strong>s, 1997) and in (Fiorato et al., 1970) clearlyprovide higher stiffness values compared with remaining ones. As a matter <strong>of</strong>fact, the expression given in (Fiorato et al., 1970) is aimed at the assessment <strong>of</strong>the infilled frame stiffness in the earliest range <strong>of</strong> loa<strong>di</strong>ng, when cracking <strong>of</strong> thepanel and separation at the interface between panel and surroun<strong>di</strong>ng frame havenot taken place yet. The expression proposed by Far<strong>di</strong>s (1997), even if in asimplified way, evaluates the infill stiffness in a pre-cracking phase, too.On the contrary, the other described formulas evaluate a secant stiffness value,up to first cracking (Mainstone, 1971) or to 50% <strong>of</strong> the maximum load (Paulayand Priestley, 1992) con<strong>di</strong>tions, or a not properly initial stiffness value referredto non-integral infilled frames (Liauw and Kwan, 1984).Hence, in this study, in order to evaluate the infill stiffness in a pre-crackingphase, the expression proposed by Far<strong>di</strong>s (Eq. 3.2.4.1) is adopted.800700600K [kN/mm]F∆Far<strong>di</strong>s, 1997Fiorato et al., 1970Paulay and Priestley, 1992Liauw and Kwan, 1984Mainstone, 1971500K=F/∆400300200100G w [MPa]0600 800 1000 1200 1400 1600 1800 2000Figure 3.4.2.2. Comparison <strong>of</strong> infilled frame stiffness accor<strong>di</strong>ng to <strong>di</strong>fferent literature models


186 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>3.4.3. Numerical estimate <strong>of</strong> period <strong>of</strong> infilled <strong>RC</strong> MRF <strong>buil<strong>di</strong>ngs</strong>A numerical investigation <strong>of</strong> period <strong>of</strong> vibration <strong>of</strong> infilled <strong>RC</strong> MRF<strong>buil<strong>di</strong>ngs</strong> is carried out through a parametric study on a class <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong>. Eachbuil<strong>di</strong>ng is generated accor<strong>di</strong>ng to a series <strong>of</strong> geometrical and mechanicalparameters. The considered <strong>buil<strong>di</strong>ngs</strong> are designed for gravity loads only; thistypology represents a wide part <strong>of</strong> the <strong>existing</strong> <strong>RC</strong> buil<strong>di</strong>ng stock. As a matter<strong>of</strong> fact, the 43% <strong>of</strong> the Italian territory is classified as exposed to seismic riskand, within this portion, only the 40% <strong>of</strong> structures have been designedaccor<strong>di</strong>ng to seismic guidelines (De Marco et al., 2000). The structural model isdefined by means <strong>of</strong> a simulated design procedure, carried out accor<strong>di</strong>ng tocode prescriptions and design practices at the age <strong>of</strong> construction, that is,between 1950s and 1970s (RDL 2229, 1939). The presence <strong>of</strong> uniformly<strong>di</strong>stributed external infill panels is taken into account.3.4.3.1 Buil<strong>di</strong>ng populationModelled <strong>buil<strong>di</strong>ngs</strong> have a rectangular shape in plan, defined by a surfacearea (A b ) equal to 200, 400 or 600 square meters. This range is based on in-situsurveys carried out during last years in <strong>di</strong>fferent Italian cities, in order to collectdata for the assessment <strong>of</strong> seismic <strong>vulnerability</strong> <strong>of</strong> the <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>tock (Cosenza et al., 2003; Pecce et al., 2004; Polese et al., 2008). For eachvalue <strong>of</strong> A b , longitu<strong>di</strong>nal and transversal <strong>di</strong>mensions (L x and L y respectively)are evaluated from the ratio (L x /L y ), assumed equal to 1, 3/2, 2 and 5/2. Figure3.4.3.1 shows plan <strong>di</strong>mensions L x and L y depen<strong>di</strong>ng on surface area A b , for eachvalue <strong>of</strong> the ratio (L x /L y ).


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 187L x /L y =1 L x /L y =3/224.5020.0014.1420.0016.3311.5514.1420.0024.5017.3224.5030.00A b200m 2400m 2L x /L y =2 L x /L y =5/2600m 217.3214.1410.0015.4912.658.9420.0028.2834.6422.3631.6238.73Figure 3.4.3.1. Morphology and plan <strong>di</strong>mensions <strong>of</strong> analyzed <strong>buil<strong>di</strong>ngs</strong>Starting from the global <strong>di</strong>mensions in plan L x and L y , all possiblecombinations <strong>of</strong> number <strong>of</strong> bays in longitu<strong>di</strong>nal and transversal <strong>di</strong>rections (n x ,n y ) are determined assuming a bay length (a x , a y ) between 3.5 and 6.0 meters(Simurai, 2010). A staircase is present, centred respect to the longitu<strong>di</strong>nal<strong>di</strong>mension and 3 meters wide; inclined axis beams parallel to the transversal<strong>di</strong>rection are present in the staircase. The number <strong>of</strong> storeys is between two andeight; the interstorey height is equal to a z =3.0 meters.The concrete compressive strength f c is assumed equal to 20 MPa; Young’smodulus E c is given by 22.000 (f c /10) 0.3 (CEN, 2004b).Given the illustrated parameters, the structural model <strong>of</strong> the buil<strong>di</strong>ng is definedby means <strong>of</strong> a simulated gravity loads design procedure (Cosenza et al., 2005;Verderame et al., 2010c). The structural configuration follows the parallelplane frames system: frames in longitu<strong>di</strong>nal <strong>di</strong>rection resist to gravity loadsfrom slabs, and in transversal <strong>di</strong>rection only two frames at the two ends arepresent (see Figure 3.4.3.2a). Slab way is always parallel to the transversal<strong>di</strong>rection. Element <strong>di</strong>mensions are calculated accor<strong>di</strong>ng to the allowable


188 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>stresses method; the design value for maximum concrete compressive stress isassumed equal to 5.0 and 7.5 MPa for axial load and axial load combined withben<strong>di</strong>ng respectively. Design values <strong>of</strong> dead and live gravity loads areevaluated. Column <strong>di</strong>mensions are calculated accor<strong>di</strong>ng only to the axial load,beam <strong>di</strong>mensions are determined from ben<strong>di</strong>ng due to loads from slabs.Infills are considered as uniformly <strong>di</strong>stributed in external frames <strong>of</strong> eachbuil<strong>di</strong>ng, see Figure 3.4.3.2b. Clear <strong>di</strong>mensions <strong>of</strong> infill panels – height h w andlength l w – are evaluated taking into account beam and column <strong>di</strong>mensionsrespectively. The panel thickness s w is assumed equal to 200 mm,correspon<strong>di</strong>ng to a double layer brick infill (120+80)mm thick, which can beconsidered as typical <strong>of</strong> a non-structural infill masonry wall (Bal et al., 2007).Elastic shear modulus G w is equal to 1350, 1080 or 1620 MPa, which can beassumed, respectively, as the me<strong>di</strong>an value and the me<strong>di</strong>an value minus andplus one time the standard deviation for hollow clay brick panels (with hollowpercentage lower than 45%), accor<strong>di</strong>ng to the actual Italian seismic code(Circolare 617, 2009). The assumed range <strong>of</strong> values for G w is also consistentwith the value <strong>of</strong> 1240 MPa provided in (Far<strong>di</strong>s, 1997), based on wallette testscarried out at the University <strong>of</strong> Pavia on specimens made up <strong>of</strong> hollow claybricks with a void ratio <strong>of</strong> 42%, selected as representative <strong>of</strong> typical light nonstructuralmasonry.Stiffness <strong>of</strong> infills is evaluated accor<strong>di</strong>ng to two hypotheses:(i) uncracked infills, adopting Eq. (3.2.4.1) proposed in (Far<strong>di</strong>s, 1997),similar to the expression proposed in (Fiorato et al., 1970). Theperiod values are compared with the empirical formulas for <strong>existing</strong>infilled <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>, based on in-situ experimental results obtainedby means <strong>of</strong> microtremors (Section 3.4.1.3);(ii) cracked infills, adopting Eq. (3.2.4.4) proposed in (Mainstone, 1971)for the evaluation <strong>of</strong> the secant stiffness to the first cracking. Theperiod values are compared with literature formulas based on similarnumerical analyses (Section 3.4.1.4).


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 189Period is evaluated both with and without presence <strong>of</strong> openings. The openingpercentage is assumed equal to 20%, which can be considered as representative,on average, <strong>of</strong> window presence (Bal et al., 2007). For uncracked infills (case i)the stiffness is reduced by 25%; this reduction is evaluated accor<strong>di</strong>ng to thesimple method proposed in (Fiorato et al., 1970) for the initial elastic stiffness<strong>of</strong> masonry infilled panels with openings. For cracked infills (case ii) areduction factor equal to 0.38 is applied to Mainstone’s formula, accor<strong>di</strong>ng to(Asteris, 2003).The total number <strong>of</strong> considered <strong>buil<strong>di</strong>ngs</strong>, given by the variation <strong>of</strong> morphology(L x /L y ), surface area (A b ), plan <strong>di</strong>mensions (L x , L y ), bay length (a x , a y ), number<strong>of</strong> storeys (N) and infill mechanical characteristics (G w ), is equal to 672.infill wallL y a ya ycolumnbeamslab waya ystairstairinfill walla x a x 3.00a x a xl w l w l w l wL xL x(a)(b)Figure 3.4.3.2. Plan buil<strong>di</strong>ng model: structural configuration (a), external infill configuration(b)3.4.3.2 Evaluation <strong>of</strong> periodFor each buil<strong>di</strong>ng, a modal analysis was performed on a three-<strong>di</strong>mensionalnumerical model <strong>of</strong> the structure and fundamental periods <strong>of</strong> vibration inlongitu<strong>di</strong>nal (X) and transversal (Y) <strong>di</strong>rections were calculated.Masses were evaluated from a load analysis carried out on every buil<strong>di</strong>ng. Ateach floor level a master joint was defined, correspon<strong>di</strong>ng to the position <strong>of</strong> thecentre <strong>of</strong> masses; the total floor mass was attributed to this joint, both in terms<strong>of</strong> translational and rotational Degree Of Freedom (DOF), in longitu<strong>di</strong>nal and


190 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>transversal <strong>di</strong>rections and around the vertical axis respectively. Hence, the3N×3N mass <strong>di</strong>agonal matrix ([M]) <strong>of</strong> the entire structure relative to theseDOFs was defined, where N is the number <strong>of</strong> storeys.A three-<strong>di</strong>mensional numerical model <strong>of</strong> the structure was built up by means <strong>of</strong>OpenSees s<strong>of</strong>tware (McKenna et al., 2004). Infill panels were represented byshear links connecting the opposite joints <strong>of</strong> each bay in the external frames.These links were characterized by the elastic stiffness calculated by means <strong>of</strong>Eq. (14) (uncracked infills) or Eq. (15) (cracked infills), based on the clear<strong>di</strong>mensions <strong>of</strong> the panel and its parametric mechanical characteristics. Grossstiffness was attributed to <strong>RC</strong> element sections.A rigid <strong>di</strong>aphragm constraint was assigned to joints <strong>of</strong> each floor slab and the3N×3N stiffness matrix ([K]) related to the same DOFs was defined, imposingunit generalized <strong>di</strong>splacements at the N previously defined master joints.An eigenvalue analysis was performed by means <strong>of</strong> MATLAB ® s<strong>of</strong>tware, inorder to evaluate the 3N natural vibration frequencies (ω i ) <strong>of</strong> the structure andthe related modal <strong>di</strong>splacement vectors ({Ψ} i ), solving the following equation:2[ ] [ ] { } { }( K − ω M ) Ψ = 0(3.4.3.1)The i th period <strong>of</strong> vibration was given by:Ti2π= (3.4.3.2)ωiHence, the fundamental periods <strong>of</strong> vibration T x and T y were evaluated as theperiods characterized by the higher participating mass ratios in longitu<strong>di</strong>nal andtransversal <strong>di</strong>rections respectively.3.4.4. Analysis <strong>of</strong> resultsIn this Section, results <strong>of</strong> modal analyses carried out on <strong>buil<strong>di</strong>ngs</strong> defined inSection 3.4.3.1 are presented and <strong>di</strong>scussed. Numerical expressions obtained byregression <strong>of</strong> analytical data are presented and compared with main literatureformulas, previously illustrated in Section 3.4.1.


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 191Results for <strong>buil<strong>di</strong>ngs</strong> with uncracked external infills (case i), based on thestiffness model proposed in (Far<strong>di</strong>s, 1997), both with and without the presence<strong>of</strong> openings, are analyzed first.The influence <strong>of</strong> internal infills is also considered. The period <strong>of</strong> a buil<strong>di</strong>ngwith internal infills is evaluated depen<strong>di</strong>ng on the period <strong>of</strong> the correspon<strong>di</strong>ngbuil<strong>di</strong>ng without internal infills.Then, numerical results for <strong>buil<strong>di</strong>ngs</strong> with cracked external infills (case ii),based on the secant stiffness model proposed in (Mainstone, 1971), are<strong>di</strong>scussed.3.4.4.1. Uncracked infillsFigures 3.4.4.1a and 3.4.4.1b report the fundamental period <strong>of</strong> vibration Tversus the height H for longitu<strong>di</strong>nal (X) and transversal (Y) <strong>di</strong>rectionsrespectively, for <strong>buil<strong>di</strong>ngs</strong> with uncracked infills without openings.First <strong>of</strong> all, numerical values <strong>of</strong> period – for the same height – vary even by100%, in both considered <strong>di</strong>rections.The period in longitu<strong>di</strong>nal <strong>di</strong>rection (T x ) is clearly lower than in transversal<strong>di</strong>rection (T y ). This is certainly due to the <strong>di</strong>fference in <strong>di</strong>mensions L x and L y :unless the case (L x /L y =1), the longitu<strong>di</strong>nal <strong>di</strong>mension L x is higher than thetransversal <strong>di</strong>mension L y , up to (L x /L y =5/2).1.0Period T x [sec]1.0Period T y [sec]0.80.80.60.60.40.40.20.2H [m]0.00 5 10 15 20 25 30H [m]0.00 5 10 15 20 25 30Figure 3.4.4.1. Period-height relationship for <strong>buil<strong>di</strong>ngs</strong> with uncracked infills without openings:longitu<strong>di</strong>nal (a) and transversal (b) <strong>di</strong>rections


192 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>Generally speaking, in infilled <strong>buil<strong>di</strong>ngs</strong> a significant contribution to theoverall lateral stiffness is given by infills along the considered <strong>di</strong>rection. If theonly plan <strong>di</strong>mension opposite to the considered <strong>di</strong>rection changes, the buil<strong>di</strong>ngarea changes too, lea<strong>di</strong>ng to a <strong>di</strong>fferent total mass, while the lateral stiffness <strong>of</strong>the buil<strong>di</strong>ng does not change significantly because the stiffness contribution <strong>of</strong>infills along the considered <strong>di</strong>rection remains constant. Therefore, a variation inperiod valuevariation inTx(y)is expected, roughly proportional to the square root <strong>of</strong> theLy(x). On the contrary, if the only plan <strong>di</strong>mension along theconsidered <strong>di</strong>rection changes, the total mass and the infill contribution to lateralstiffness change in the same way, not lea<strong>di</strong>ng to a significant variation in periodvalue. The latter consideration, in particular, is consistent with (Goel andChopra, 1998), where a poor correlation between H L x(y ) and Tx(y)ispointed out by the authors.In the present buil<strong>di</strong>ng population, for <strong>buil<strong>di</strong>ngs</strong> with equal surface area, asthe ratio (L x /L y ) increases, the former <strong>di</strong>mension increases and the latterdecreases, respectively lea<strong>di</strong>ng to an increase in lateral stiffness in longitu<strong>di</strong>nal<strong>di</strong>rection and to a decrease in lateral stiffness in transversal <strong>di</strong>rection, while thetotal buil<strong>di</strong>ng mass remains about constant. Then, given equal the surface area,as (L x /L y ) increases, a decrease in T x and an increase in T y are expectedcompared with the case (L x /L y =1).As a matter <strong>of</strong> fact, the lateral stiffness for <strong>buil<strong>di</strong>ngs</strong> with (L x /L y =1) is verysimilar in both <strong>di</strong>rections, thus lea<strong>di</strong>ng to a ratio (T x /T y ) close to 1. The perio<strong>di</strong>n transversal <strong>di</strong>rection T y is almost linear with the period in longitu<strong>di</strong>nal<strong>di</strong>rection T x , given equal the ratio (L x /L y ), and increases with (L x /L y ), see Figure3.4.4.2a.These considerations are consistent with Eq. (3.4.1.7), adopted by severalseismic codes (e.g. ATC, 1978) for the evaluation <strong>of</strong> fundamental period <strong>of</strong> <strong>RC</strong>SW <strong>buil<strong>di</strong>ngs</strong>. This expression can be applied to the present numerical data. Ifspecific values are assumed for coefficient α in longitu<strong>di</strong>nal and transversal<strong>di</strong>rections, the following expressions are obtained:


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 193TxH= α x(3.4.4.1)LxTyH= α y(3.4.4.2)Lylea<strong>di</strong>ng to:TyαLy x= Tx(3.4.4.3)α x LyAccor<strong>di</strong>ng to Eq. (3.4.4.3), T y is proportional to T x , given equal the ratio(L x /L y ), and increases with this value.The value <strong>of</strong> ratio2y Tx)α α can be observed from Figure 3.4.4.2b, whereyx( T versus (L x /L y ) is reported. Unless a moderate variability, α y α x is,on average, equal to 1 for each <strong>of</strong> the considered values <strong>of</strong> the ratio between L xand L y . Based on this result, an unique value α = α = α can be assumed,independent <strong>of</strong> the considered <strong>di</strong>rection. This is consistent with literatureproposals for <strong>RC</strong> SW <strong>buil<strong>di</strong>ngs</strong>, as reported in Eq. (3.4.1.7).yx0.70.60.50.40.30.2T y [sec]5/223/2(L x /L y )0.1T x [sec]00 0.1 0.2 0.3 0.4 0.5 0.6 0.713.02.52.01.51.0(T y /T x ) 2y = 1.00xR 2 = 0.9900.5(L x /L y )0.00.0 0.5 1.0 1.5 2.0 2.5 3.0Figure 3.4.4.2. Comparison between longitu<strong>di</strong>nal (T x ) and transversal (T y ) periods for <strong>di</strong>fferentvalues <strong>of</strong> the ratio (L x /L y ) (a); value <strong>of</strong> ratio α y α x (b)


194 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>These considerations highlight a similarity between the elastic dynamicresponse <strong>of</strong> infilled <strong>RC</strong> MRF <strong>buil<strong>di</strong>ngs</strong> and <strong>RC</strong> SW <strong>buil<strong>di</strong>ngs</strong>. As a matter <strong>of</strong>fact, some geometric parameters – such as height (H) and plan <strong>di</strong>mensions (L x ,L y ) – seem to influence in a similar way the period <strong>of</strong> vibration for these twostructural typologies. In both cases, a significant contribution to the lateralstiffness <strong>of</strong> the buil<strong>di</strong>ng is given by walls; hence, the period is wellapproximated by the period <strong>of</strong> an equivalent cantilever, see Section 3.4.1. Thisis also consistent with the assumption made in (Fiorato et al., 1970), where theinitial stiffness <strong>of</strong> an infilled frame is evaluated by modelling the frame as anequivalent composite cantilever, see Section 3.4.2.Hence, a regression analysis is carried out on numerical data accor<strong>di</strong>ng toexpression (3.4.1.7). Evaluation <strong>of</strong> coefficient α is based on all data,independent <strong>of</strong> the considered <strong>di</strong>rection ( α = αy= αx); to this end, for eachbuil<strong>di</strong>ng the period T x(y)is reported depen<strong>di</strong>ng on the ratio H L x(y ), seeFigure 3.4.4.3. Then, α is estimated via or<strong>di</strong>nary least square regression,obtaining:HT x(y) = 0.063(3.4.4.4)Lx(y)with H and L x(y)expressed in meters.In Figure 3.4.4.3 the numerical data are reported and expression (3.4.4.4) isplotted, versus the ratio H L x(y ) . The low pre<strong>di</strong>ction capacity <strong>of</strong> Eq. (3.4.4.4)is clearly shown. Given a value <strong>of</strong> H L x(y )noticeably variable, even by 100%., the analytical period values are


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 1951.00.80.6Period T x(y) [sec]y = 0.063xR 2 = 0.7120.40.2H/(L x(y) ) 1/20.00 2 4 6 8 10Figure 3.4.4.3. Simplified formula for period <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong> with uncracked infills versusHL x(y)As above mentioned, the scarce pre<strong>di</strong>ction capacity <strong>of</strong> the ratio H L x(y ) isalso highlighted in (Goel and Chopra, 1998) for the period <strong>of</strong> <strong>RC</strong> SW <strong>buil<strong>di</strong>ngs</strong>.The authors, based on analytical procedures, propose Eq. (3.4.1.7) as a moreadequate expression to pre<strong>di</strong>ct the period value. Eq. (3.4.1.7) is a rearrangement<strong>of</strong> Eq. (3.4.1.5), because it considers not only the shear deformability but alsothe flexural deformability.In this study, consistently with the purely shear nature <strong>of</strong> the stiffness modeladopted for uncracked infills (Far<strong>di</strong>s, 1997), the contribution <strong>of</strong> flexuraldeformability considered in Eq. (3.4.1.7) is not taken into account.Therefore, the following expression is assumed as alternative to Eq. (3.4.4.4):Tx(y)H= α(3.4.4.5)Ax(y)where A x(y)is the ratio (in percentage) between the infill area (roughlyevaluated inclu<strong>di</strong>ng column <strong>di</strong>mensions) along the considered <strong>di</strong>rection x(y)and the buil<strong>di</strong>ng area. Based on infill <strong>di</strong>stribution in considered <strong>buil<strong>di</strong>ngs</strong> (seeFigure 3.4.3.2b), this ratio can be expressed as( )Ax(y) = ⎡⎣2⋅sw ⋅ Lx(y)( Lx ⋅ Ly) ⎤⎦ ⋅ 100 = 2⋅sw Ly(x)⋅100. Then, Eq. (3.4.4.5)


196 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>becomes:HTx(y)= 0.020(3.4.4.6)Ax(y)where H is the buil<strong>di</strong>ng height expressed in meters. Eq. (3.4.4.6), given theexpression <strong>of</strong>Ax(y), highlights a <strong>di</strong>rect dependence between Tx(y)and Ly(x),consistently with the considerations reported at the beginning <strong>of</strong> the presentSection. Figure 3.4.4.4a reports the numerical data and the plot <strong>of</strong> Eq. (3.4.4.6),versus the ratio H A x(y ). The high pre<strong>di</strong>ction capacity <strong>of</strong> Eq. (3.4.4.6) isclearly shown. The higher estimate capacity <strong>of</strong> Eq. (3.4.4.6) compared with Eq.(21) is due to the parameter A x(y), accounting for the variability in floor massand storey stiffness. As a matter <strong>of</strong> fact, both the surface area ( L x ⋅ L y ) –proportional to the floor mass by unit area mass m S – and the infill area –proportional to the storey infill stiffness by shear modulus G w and height h w –are included in A x(y). The low variability <strong>of</strong> analytical period, given equalH A x(y) , is mainly due to the specific stiffness <strong>of</strong> infills, that is, to G w ,which is not included in A x(y).If the periodTx(y)is expressed as depen<strong>di</strong>ng on H GwA x(y)(see Figure3.4.4.4b), the pre<strong>di</strong>ction capacity further increases, thus demonstrating theinfluence <strong>of</strong> shear modulus G w . Therefore, it is likely to assume that theremaining variability can be explained by the variability in bay length.Moreover, it is to be noted that coefficient α in Eq. (3.4.4.6) is equal to 0.020,while in Eq. (3.4.1.8) it is equal to 0.0077 for <strong>RC</strong> SW <strong>buil<strong>di</strong>ngs</strong>. The <strong>di</strong>fferencein the order <strong>of</strong> magnitude between these values can be explained by the<strong>di</strong>fference in shear modulus between concrete ( G ) and infills ( Gin coefficients α . If an elastic moduluscw), includedE c =25000 MPa is assumed, withν=0.20, the shear modulus is equal to G = E 2(1 + ν)= 10400 MPa. Ifcc


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 197Gw=1350 MPa, the ratio(0.020/0.0077)=2.60.G G is equal to 2.78, not far fromcw1.0Period T x(y) [sec]1.0Period T x(y) [sec]y = 0.713x0.8y = 0.020x0.8H/(A x(y) ) 1/2 H/(G w A x(y) ) 1/2R 2 = 0.940R 2 = 0.9810.60.60.40.40.20.20.00.00 5 10 15 20 25 30 0 0.2 0.4 0.6 0.8 1Figure 3.4.4.4: Simplified formula for period <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong> with uncracked infills versusH Ax(y)(a) and versusw x(y)H G A (b)Based on the analyzed data, the lateral stiffness <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong> with uniformly<strong>di</strong>stributed uncracked infills is mainly due to the only infill contribution, andthe contribution <strong>of</strong> the <strong>RC</strong> structure (frames and stairs) can be considered asnegligible.Further regression analyses are carried out on numerical data, in order to makea comparison with literature formulas. In particular, the period is assumed asdepen<strong>di</strong>ng on the power <strong>of</strong> the height ( T = αH), as linearly depen<strong>di</strong>ng on theheight ( T = αH) and on the number <strong>of</strong> storeys ( T = αN).Evaluation <strong>of</strong> coefficients α and β is based on all data, independent <strong>of</strong> theconsidered <strong>di</strong>rection. The obtained period-height relationships – with H inmeters – are respectively:0.85T = 0.022H(3.4.4.7)T = 0.014H(3.4.4.8)T = 0.043N(3.4.4.9)β


198 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>The pre<strong>di</strong>ction capacity <strong>of</strong> Eqs. (3.4.4.7), (3.4.4.8) and (3.4.4.9) is clearly low,if compared with Eq. (3.4.4.6), see Figure 3.4.4.5. The high variability <strong>of</strong>periods, given a value <strong>of</strong> height, is due to the dependence <strong>of</strong> period ongeometrical parameters not included in these expressions. Nevertheless, it is tobe noted that their pre<strong>di</strong>ction capacity is not lower than the pre<strong>di</strong>ction capacity<strong>of</strong> Eq. (3.4.4.4).1.0Period T [sec]1.0Period T [sec]0.80.60.4y = 0.014xR 2 = 0.731y = 0.022x 0.85R 2 = 0.8040.80.60.4y = 0.043xR 2 = 0.7310.20.2H [m]0.00 5 10 15 20 25 30Number <strong>of</strong> storeys, N0.00 2 4 6 8 10Figure 3.4.4.5. Simplified formulas for period <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong> with uncracked infills depen<strong>di</strong>ng onheight H (a) and number <strong>of</strong> storeys N (b)If coefficient α in ( T = αH) is evaluated separately for longitu<strong>di</strong>nal (X) andtransversal (Y) <strong>di</strong>rection, Eq. (3.4.4.8) changes into:T x = 0.012H(3.4.4.10)T y = 0.016H(3.4.4.11)Expressions proposed up to here are based on period <strong>of</strong> infilled <strong>RC</strong> MRF<strong>buil<strong>di</strong>ngs</strong> without openings. The presence <strong>of</strong> openings, assumed to be uniformly<strong>di</strong>stributed and correspon<strong>di</strong>ng to an opening percentage <strong>of</strong> 20%, leads to adecrease in stiffness <strong>of</strong> infills by 25%, thus increasing the period <strong>of</strong> vibration <strong>of</strong><strong>buil<strong>di</strong>ngs</strong>.If presence <strong>of</strong> openings is taken into account, Eq. (3.4.4.6) – expressing theperiod as depen<strong>di</strong>ng on the infill percentage area A x(y)– changes into the


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 199following:HT x(y) = 0.023(3.4.4.12)Ax(y)The increase in the value <strong>of</strong> period is, on average, <strong>of</strong> 15%, technicallycorrespon<strong>di</strong>ng to the square root <strong>of</strong> the ratio between the infill stiffness withand without openings. Hence, even if openings are present and uniformly<strong>di</strong>stributed, the lateral stiffness <strong>of</strong> the buil<strong>di</strong>ng is well represented by the onlystiffness contribution <strong>of</strong> infills.Period-height relationships can be obtained again, by new numericalregressions on period values accounting for the presence <strong>of</strong> openings. Anincrease in coefficient α can be noted.If Eqs. (3.4.4.7), (3.4.4.8) and (3.4.4.9) are evaluated independent <strong>of</strong> the<strong>di</strong>rection, the following expressions are obtained:0.85T = 0.025H(3.4.4.13)T = 0.016H(3.4.4.14)T = 0.049N(3.4.4.15)while Eqs. (3.4.4.10) and (3.4.4.11), depen<strong>di</strong>ng on the considered <strong>di</strong>rection, are:T x = 0.014H(3.4.4.16)T y = 0.019H(3.4.4.17)Influence <strong>of</strong> internal infillsAbove illustrated results show that the lateral stiffness <strong>of</strong> infilled <strong>buil<strong>di</strong>ngs</strong>,with or without openings, is well represented by the stiffness contribution <strong>of</strong>infills, since the stiffness contribution <strong>of</strong> <strong>RC</strong> structure can be considered asnegligible. Stiffness <strong>of</strong> infills is well represented by the infill area, given equalthe height h w and the shear modulus G w .


200 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>In the following, based on these considerations, the influence <strong>of</strong> internal infillson the fundamental period <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong> is approximately evaluated. Internalinfills, as well as external infills, increase lateral stiffness <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong>; this isevaluated by the increase in infill area, that is, in parameter A x(y).Internal infills are assumed as symmetrically <strong>di</strong>stributed in plan, along both<strong>di</strong>rections. Shear modulus G w and height h w are assumed equal to externalinfills. The thickness is assumed equal to s w =100 mm. The reduction in thevalue <strong>of</strong> period, compared with the case when only external infills are present,can be estimated as proportional to the square root <strong>of</strong> the increase in stiffness,that is, in infill area due to the presence <strong>of</strong> internal infills. In both <strong>di</strong>rections, itis assumed that the overall linear <strong>di</strong>mension <strong>of</strong> internal infills is equal toexternal infills (Crowley and Pinho, 2010). Based on this assumption, given thelower thickness <strong>of</strong> internal infills, due to their presence the total infill areaincreases by 50%.Therefore, the period <strong>of</strong> both internally and externally infilled <strong>buil<strong>di</strong>ngs</strong> is equalto 2 /3 = 0. 82 times the period <strong>of</strong> only externally infilled <strong>buil<strong>di</strong>ngs</strong>. Inparticular, if the presence <strong>of</strong> openings is not taken into account:T = 0.011H(3.4.4.18)or:T = 0.035N(3.4.4.19)while, if openings are present:T = 0.013H(3.4.4.20)or:T = 0.040N(3.4.4.21)3.4.4.2. Cracked infillsIn this Section, results <strong>of</strong> modal analyses carried out accor<strong>di</strong>ng to the hypothesis<strong>of</strong> cracked infills – by means <strong>of</strong> the secant stiffness model proposed in


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 201(Mainstone, 1971) – are presented. Cracking <strong>of</strong> infills leads to a severe decreasein their stiffness, that is, to an increase in the fundamental period in both<strong>di</strong>rections, compared with the uncracked con<strong>di</strong>tion.If the presence <strong>of</strong> openings is not considered, the period increases, on average,by 120%. If openings are present, the period increases even by 160%. Thepresence <strong>of</strong> openings leads to a higher increase in values <strong>of</strong> period, because thedecrease in infill stiffness due to their presence is more severe for crackedcon<strong>di</strong>tion than for uncracked con<strong>di</strong>tion.A regression analysis is carried out accor<strong>di</strong>ng to the expression T = αH, inorder to make a comparison with similar formulas, see Section 3.4.1.4.Simplified expressions for period <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong> with cracked infills withoutopenings, in longitu<strong>di</strong>nal and transversal <strong>di</strong>rections, are respectively given by:T x= 0.026H(3.4.4.22)T y= 0.036H(3.4.4.23)If presence <strong>of</strong> openings is considered, period is given by:T x= 0.034H(3.4.4.24)T y= 0.048H(3.4.4.25)Simplified formulas for period <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong> with cracked infills, independent <strong>of</strong>the considered <strong>di</strong>rection, are provided, without openings (Figure 3.4.4.6a):T = 0.031H(3.4.4.26)and with openings (Figure 3.4.4.6b):T = 0.041H(3.4.4.27)


202 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>1.81.51.2Period T [sec]y = 0.031xR 2 = 0.6911.81.51.2Period T [sec]y = 0.041xR 2 = 0.6530.90.90.60.60.3H [m]0.00 5 10 15 20 25 300.3H [m]0.00 5 10 15 20 25 30Figure 3.4.4.6. Simplified formulas for period <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong> with cracked infills without (a) andwith (b) openingsExpressions for period <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong> with cracked infills, with and withoutopenings, provide an upper and a lower bound, respectively, for the expressiongiven in (Crowley and Pinho, 2006) for uncracked infilled <strong>buil<strong>di</strong>ngs</strong> (Eq.(3.4.1.9)).This is probably due to the infill stiffness assumed by the authors: the value <strong>of</strong>secant stiffness given by the model proposed in (Liauw and Kwan, 1984) forE w =1500 MPa (Crowley and Pinho, 2006) is quite similar to the infill stiffnessgiven by (Mainstone, 1971) in the assumed range <strong>of</strong> variation for G w .Moreover, the authors do not build three-<strong>di</strong>mensional models <strong>of</strong> considered<strong>buil<strong>di</strong>ngs</strong>, but only two-<strong>di</strong>mensional models <strong>of</strong> representative frames (bare,fully infilled or infilled with openings). The dynamic response <strong>of</strong> the buil<strong>di</strong>ng,in terms <strong>of</strong> fundamental period <strong>of</strong> vibration, is obtained as a weighted average<strong>of</strong> the two-<strong>di</strong>mensional response <strong>of</strong> modelled frames, based on the meanfrequency <strong>of</strong> occurrence <strong>of</strong> each type <strong>of</strong> frame within a typical buil<strong>di</strong>ng,provided by (Bal et al., 2007).Finally, Eq. (3.4.1.11), proposed in (Masi and Vona, 2008), is <strong>di</strong>fferent aboutby 40% from the expression for transversal period <strong>of</strong> infilled <strong>buil<strong>di</strong>ngs</strong> withoutopenings. This is probably due to a <strong>di</strong>fference in the assumed value <strong>of</strong> infillshear modulus G w .


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 2033.4.5. Comparison with literature formulasIn this Section, proposed expressions for fundamental period <strong>of</strong> infilled<strong>buil<strong>di</strong>ngs</strong> are compared with literature empirical and numerical expressions.Comparison is carried out accor<strong>di</strong>ng to two main issues: structural typology an<strong>di</strong>ntensity <strong>of</strong> excitation used for the experimental measurement <strong>of</strong> period.Therefore, numerical formulas proposed herein for period <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong> withuncracked infills are compared with literature regressions <strong>of</strong> experimental dataobtained by means <strong>of</strong> techniques based on low amplitude motion –microtremors or ambient noise – previously introduced in Section 3.4.1.3.These experimental stu<strong>di</strong>es were carried out on infilled <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> inMe<strong>di</strong>terranean area, similar to analyzed <strong>buil<strong>di</strong>ngs</strong> in structural typology an<strong>di</strong>nfill characteristics. Due to the nature <strong>of</strong> the applied measurement techniques,it is likely to assume that these relationships provide a not lengthened value <strong>of</strong>the period, correspon<strong>di</strong>ng to a linear behaviour <strong>of</strong> structural materials andcomponents.Main considered period-height relationships are reported in (Oliveira, 2004;Navarro and Oliveira, 2006; Gallipoli et al., 2010). Moreover, expressionsprovided by (Kobayashi et al., 1996; Dunand et al., 2002), reported in (Oliveiraand Navarro, 2010), respectively concerning Spanish and French <strong>buil<strong>di</strong>ngs</strong>, areconsidered.These relationships express period value depen<strong>di</strong>ng on height or number <strong>of</strong>storeys, usually independent <strong>of</strong> the buil<strong>di</strong>ng plan <strong>di</strong>rection. Therefore, in thefollowing, a numerical-experimental comparison will be carried out accor<strong>di</strong>ngboth to height and to number <strong>of</strong> storeys.Figure 3.4.5.1 reports proposed linear relationships for <strong>buil<strong>di</strong>ngs</strong> withuncracked infills and literature experimental relationships. Only highest andlowest experimental period values are reported and the area between thesebounds is painted in grey for an easier understan<strong>di</strong>ng. Proposed analyticalexpressions include only externally infilled <strong>buil<strong>di</strong>ngs</strong> (in red), with or withoutopenings, and both internally and externally infilled <strong>buil<strong>di</strong>ngs</strong> (in blue), with or


204 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>without openings. A very good agreement between numerical and experimentalrelationships is shown.Numerical relationships for both internally and externally infilled <strong>buil<strong>di</strong>ngs</strong>(in blue) fully fit the range <strong>of</strong> experimental values. The assumption <strong>of</strong> presence<strong>of</strong> only externally infills (in red) leads to higher values <strong>of</strong> period.1.00.80.6Period T [sec]with int.infills - w/o openingswith int.infills - with openingsw/o int.infills - w/o openingsw/o int.infills - with openingsDunand et al., 2002Oliveira, 2004 - long.1.00.80.6Period T [sec]with int.infills - w/o openingswith int.infills - with openingsw/o int.infills - w/o openingsw/o int.infills - with openingsOliveira, 2004 - transv.Kobayashi et al., 19960.40.40.20.2H [m]0.00 5 10 15 20 25 30 35 40number <strong>of</strong> storeys, N0.00 2 4 6 8 10 12 14Figure 3.4.5.1. Comparison between proposed and experimental period-height (a) andperiod-number <strong>of</strong> storeys (b) relationships (area between highest and lowest experimentalperiod values is painted in grey)It is to be noted that modelled <strong>RC</strong> MRF <strong>buil<strong>di</strong>ngs</strong> were designed for gravityloads only. For these <strong>buil<strong>di</strong>ngs</strong>, it was shown that the contribution <strong>of</strong> the <strong>RC</strong>structure to the overall lateral stiffness is negligible, if infills are present.However, empirical data were evaluated both on <strong>buil<strong>di</strong>ngs</strong> designed for gravityloads only and on <strong>buil<strong>di</strong>ngs</strong> designed for seismic loads, even if accor<strong>di</strong>ng toobsolete code prescriptions.In (Gallipoli et al., 2008) the period database <strong>of</strong> 65 Italian <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> isprovided (a first subset <strong>of</strong> the data set presented in (Gallipoli et al., 2010)),reporting the town and the age <strong>of</strong> construction <strong>of</strong> each buil<strong>di</strong>ng. The authorsin<strong>di</strong>cate that the town <strong>of</strong> Potenza was classified for the first time as a seismiczone after the 1980 Irpinia earthquake; hence, pre-1981 <strong>buil<strong>di</strong>ngs</strong> weredesigned for gravity loads only. Two separated regressions were carried out on


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 205pre- and post-1980 buil<strong>di</strong>ng data from this town, lea<strong>di</strong>ng to period-heightrelationships respectively given by T = 0.015Hand T = 0.014H, see Figure3.4.5.2.The design procedure <strong>of</strong> the <strong>RC</strong> structure does not seem to influencesignificantly the experimental data. As a matter <strong>of</strong> fact, seismic designed <strong>RC</strong>structures have a higher lateral stiffness – that is, a lower period <strong>of</strong> vibration(Verderame et al., 2010b) – compared with gravity loads designed structures,due to higher element section <strong>di</strong>mensions; nevertheless, in infilled <strong>buil<strong>di</strong>ngs</strong>,this effect <strong>of</strong> stiffness increase is strongly reduced by presence <strong>of</strong> infills. In(Angel, 2007) the author carries out eigenvalue analyses on <strong>existing</strong> and newinfilled <strong>RC</strong> MRF <strong>buil<strong>di</strong>ngs</strong>, obtaining much lower values for the period <strong>of</strong>vibration in the latter case. Nevertheless, a so large scatter is probably due tothe mechanical characteristics assumed for infill panels: the author supposesthat in <strong>existing</strong> <strong>buil<strong>di</strong>ngs</strong> the panels are made <strong>of</strong> light non-structural masonry,and that in new <strong>buil<strong>di</strong>ngs</strong> the same panels are made up <strong>of</strong> perforated concreteblocks, characterized by a <strong>di</strong>agonal compressive strength eight times higher.1.0Period T [sec]0.80.6pre-1980post-1980y = 0.015xy = 0.014x0.40.2H [m]0.00 10 20 30 40 50Figure 3.4.5.2. Periods <strong>of</strong> gravity load designed (pre-1980) and seismic designed (post-1980) <strong>buil<strong>di</strong>ngs</strong> in the town <strong>of</strong> Potenza, from (Gallipoli et al., 2008)


206 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>The good numerical-experimental agreement demonstrates that thehypothesis <strong>of</strong> uncracked infill stiffness is consistent with the <strong>di</strong>splacementcon<strong>di</strong>tion <strong>of</strong> infills under low amplitude motion sources <strong>of</strong> excitation.Furthermore, it is worth noting that the analytical value <strong>of</strong> period shouldrepresent a lower bound for the empirical value, since experimentalmeasurements are influenced by soil flexibility, lea<strong>di</strong>ng to an increase in period(Muriá-Vila and González, 1995). On the contrary, rigid-base hypothesis leadsa stiffer system, that is, to a lower period.Despite the good numerical-experimental agreement – in average terms – itis to be noted that the period <strong>of</strong> an infilled buil<strong>di</strong>ng depends not only on heightbut also on percentage <strong>of</strong> infill area, opening percentage and <strong>di</strong>stribution, an<strong>di</strong>nfill mechanical characteristics. This is shown by the high variability, givenequal the height, <strong>of</strong> experimental values <strong>of</strong> period (Oliveira and Navarro, 2010;Gallipoli et al., 2008), see Figure 3.4.5.2, but also by the high variability <strong>of</strong>numerical values <strong>of</strong> period, see Figure 3.4.4.1, due to the dependence on theabove mentioned parameters.Analytical evaluation <strong>of</strong> elastic period <strong>of</strong> infilled <strong>buil<strong>di</strong>ngs</strong> has to be basedon uncracked infill stiffness hypothesis. If a non-initial infill stiffness value isassumed, obtained numerical formulas (Crowley and Pinho, 2006; Masi andVona, 2008) overestimate, even by 200%, empirical data, see Figure 3.4.5.3.1.81.51.2Period T [sec]proposedCrowley and PinhoMasi and Vona0.90.60.3H [m]0.00 5 10 15 20 25 30 35 40Figure 3.4.5.3. Comparison between proposed, experimental and numerical literatureperiod-height relationships (area between highest and lowest experimental period values ispainted in grey)


Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 207This is probably the main reason <strong>of</strong> the large numerical-experimental scatterpointed out in (Masi and Vona, 2008), where a ratio about equal to 3 isregistered between the theoretical values provided by the proposed formulationand empirical values <strong>of</strong> period.Furthermore, a period calculated by assuming a cracked (secant) stiffness ateach storey does not represent the actual dynamic properties <strong>of</strong> a damage<strong>di</strong>nfilled <strong>RC</strong> buil<strong>di</strong>ng, neither in a simplified way, and it can not be employed inthe seismic assessment <strong>of</strong> this kind <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong> (Crowley and Pinho, 2006).As a matter <strong>of</strong> fact, the <strong>di</strong>stribution <strong>of</strong> damage in infills (that is, the <strong>di</strong>stribution<strong>of</strong> infill secant stiffness) is not uniform along the height <strong>of</strong> the buil<strong>di</strong>ng, as it isconsidered in these formulations, but tends to concentrate in one storey at thebottom <strong>of</strong> the buil<strong>di</strong>ng, especially if the buil<strong>di</strong>ng is seismically under-designedand strongly influenced, also in non-linear field, by the presence on infillpanels, as already highlighted in literature by means <strong>of</strong> experimental tests (Pintoet al., 2002) and numerical non-linear analyses (Dolšek and Fajfar, 2001) oninfilled <strong>RC</strong> frames or <strong>buil<strong>di</strong>ngs</strong>.The overcoming <strong>of</strong> the elastic limit, both in infill and <strong>RC</strong> elements, leads to alengthening in the period <strong>of</strong> vibration, as much as the amplitude <strong>of</strong> motionincreases. Nevertheless, these effects become much more complex in MDOFsystems (Oliveira and Navarro, 2010).


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Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong> 215− Simurai, 2010. Technical report to the SIMURAI project – StrumentiIintegrati per il MUlti Risk Assessment territoriale in ambienti urbaniantropizzatI (Integrated instruments for large scale multi risk assessmentin urban anthropic environment), supported by the Italian Ministry <strong>of</strong>Education, University and Research, scientific coor<strong>di</strong>nator Pr<strong>of</strong>.Gaetano Manfre<strong>di</strong>.− Stafford Smith B., 1966. Behaviour <strong>of</strong> square infilled frames. ASCEJournal <strong>of</strong> Structural Division, 92(1), 381-403.− Stafford Smith B., 1967. Methods for pre<strong>di</strong>cting the lateral stiffness andstrength <strong>of</strong> multi-storey infilled frames. Buil<strong>di</strong>ng Science, 2(3), 247-257.− Stafford Smith B., Carter C., 1969. A method <strong>of</strong> analysis for infilledframes. Procee<strong>di</strong>ngs <strong>of</strong> the Institution <strong>of</strong> Civil Engineering, 44, 31-48.− Styliani<strong>di</strong>s K.C., 1985. Experimental investigation <strong>of</strong> the behaviour <strong>of</strong> thesingle-story infilled R.C. frames under cyclic quasi-static horizontalloa<strong>di</strong>ng (parametric analysis). Ph.D. Thesis, University <strong>of</strong> Thessaloniki,Thessaloniki, Greece.− Verderame G.M., De Luca F., Ricci P., Manfre<strong>di</strong> G., 2010a. Preliminaryanalysis <strong>of</strong> a s<strong>of</strong>t storey mechanism after the 2009 L’Aquila earthquake,Earthquake Engineering and Structural Dynamics. DOI:10.1002/eqe.1069− Verderame G.M., Iervolino I., Manfre<strong>di</strong> G., 2010b. Elastic period <strong>of</strong> substandardreinforced concrete moment resisting frame <strong>buil<strong>di</strong>ngs</strong>. Bulletin<strong>of</strong> Earthquake Engineering, 8(4), 955-972.− Verderame G.M., Polese M, Mariniello C., Manfre<strong>di</strong> G., 2010c. Asimulated design procedure for the assessment <strong>of</strong> seismic capacity <strong>of</strong><strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>. Advances in EngineeringS<strong>of</strong>tware, 41(2), 323-335.


216 Chapter III – Influence <strong>of</strong> infills on seismic behaviour <strong>of</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 217Chapter IVNumerical investigation <strong>of</strong> seismic capacity <strong>of</strong>reinforced concrete <strong>buil<strong>di</strong>ngs</strong> with infills4.1 INTRODUCTIONDuring last decades, a growing attention has been addressed to the influence<strong>of</strong> infills on the seismic behaviour <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>, also supported by theobservation <strong>of</strong> damage to <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills after severe earthquakes(e.g., Kocaeli 1999 (EERI, 2000)). The importance <strong>of</strong> this issue was widelyrecognized by earthquake engineering researchers, lea<strong>di</strong>ng to first full-scaleexperimental tests on infilled <strong>RC</strong> frames (e.g., Negro and Verzeletti, 1996) andcode prescriptions about the consideration <strong>of</strong> infills in seismic design (e.g.,CEN, 1995). As a result, from the second half <strong>of</strong> 1990s on, several valuablenumerical efforts have been made to investigate the seismic behaviour <strong>of</strong> <strong>RC</strong>frames with infills through nonlinear analyses.In this Chapter, a review <strong>of</strong> main numerical stu<strong>di</strong>es from literature ispresented first. Hence, a numerical investigation on the influence <strong>of</strong> infills onthe seismic behaviour <strong>of</strong> a case-study Gravity Load Designed buil<strong>di</strong>ng is carriedout by means <strong>of</strong> Static Push-Over analyses, within the N2 spectral assessmentframework. Different infill configurations are considered (Bare, Uniformlyinfilled and S<strong>of</strong>t-storey infilled), and a sensitivity analysis is carried out, thusevaluating the influence <strong>of</strong> main material and capacity parameters on seismic


218 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infillsresponse for <strong>di</strong>fferent Limit States. Fragility curves are obtained, through theapplication <strong>of</strong> a Response Surface Method. Finally, a comparison between theseismic capacity assessment based on “exact” models and on correspon<strong>di</strong>ngShear Type models is carried out, in view <strong>of</strong> the simplified approach develope<strong>di</strong>n Chapter V.4.2 NUMERICAL INVESTIGATION OF SEISMIC BEHAVIOUR OFINFILLED <strong>RC</strong> BUILDINGS: STATE-OF-THE-ARTIt is to be noted that, when evaluating the influence <strong>of</strong> infills on the seismicresponse <strong>of</strong> infilled <strong>RC</strong> structures by means <strong>of</strong> nonlinear analyses, the possibleinfluence <strong>of</strong> brittle failure mechanisms – especially due to local interactionbetween infill panels and surroun<strong>di</strong>ng <strong>RC</strong> members, see Section 3.2 – is usuallynot considered, rather focusing the attention on the flexure-controlled behaviour<strong>of</strong> <strong>RC</strong> members. Sometimes, for specific case-study structures, this is justifiedby the observation <strong>of</strong> experimental behaviour (e.g., Dolšek and Fajfar,2008a,b).Far<strong>di</strong>s and Panagiotakos (1997b) presented a comprehensive study based onnonlinear dynamic analyses carried out (i) on idealized SDOF infilled frames,(ii) on the numerical model <strong>of</strong> an infilled four-storey <strong>RC</strong> structureexperimentally tested ((Negro and Verzeletti, 1996), see Section 3.3) and (iii)on <strong>RC</strong> structures with <strong>di</strong>fferent number <strong>of</strong> storeys (4, 8 or 12) (Far<strong>di</strong>s andPanagiotakos, 1997a) and infill configuration (Bare, Fully infilled or Pilotis). Itis worth noting that structures were designed for seismic loads accor<strong>di</strong>ng toEurocode 8, complying with the weak beam/strong column principle. Inparticular, based on numerical results from (iii), infill influence was deemedbeneficial on seismic response, except for very brittle or irregularly <strong>di</strong>stribute<strong>di</strong>nfills. However, the detrimental effect <strong>of</strong> an irregular infill <strong>di</strong>stribution wasmore pronounced at ground motion intensities much higher than that <strong>of</strong> thedesign motion. In me<strong>di</strong>um-high rise reinforced concrete frame <strong>buil<strong>di</strong>ngs</strong>, the


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 219presence <strong>of</strong> infills and even irregularities in their arrangement in elevation had avery small effect on the global and local seismic response, also due to the lowshear strength <strong>of</strong> the infills in comparison to the total strength and base shear <strong>of</strong>the buil<strong>di</strong>ng. The influence <strong>of</strong> code prescriptions accounting for the presence <strong>of</strong>an irregular <strong>di</strong>stribution <strong>of</strong> infills (increasing design seismic demand in s<strong>of</strong>tstoreys)was analyzed, too, and authors even came to the conclusion that theseprescriptions were too conservative.Kappos (1998) carried out nonlinear dynamic analyses on a case study tenstoreyinfilled <strong>RC</strong> frame considering <strong>di</strong>fferent infill configurations (Bare, Fullyinfilled and Pilotis) and <strong>di</strong>fferent strength values for infill material (Low andHigh). Frames were designed accor<strong>di</strong>ng to Eurocode 8, in interme<strong>di</strong>ate ductilityclass and for a PGA equal to 0.25g (without applying the specific codeprescriptions accounting for the infill presence). Hence, nonlinear dynamicanalyses were carried out assuming as input motions <strong>di</strong>fferent accelerogramsnormalized to the code design spectrum. Results highlighted a rather uniform<strong>di</strong>stribution <strong>of</strong> interstorey drift demand in the bare frame, a tendency <strong>of</strong>decreasing drift demand with the height in the fully infilled frame and a verylarge demand at the first (s<strong>of</strong>t-) storey, drastically reducing at upper storey, inthe Pilotis frame, as expected. Hence, under the same seismic action, the bestperformance (in terms <strong>of</strong> lowest interstorey drift demand) was shown by theFully infilled frame. This was also reflected by the large amount <strong>of</strong> energy<strong>di</strong>ssipated by infill elements. The worst behaviour, in terms <strong>of</strong> maximum localductility demand, was shown by the Pilotis frame.Negro and Colombo (1997) carried out a numerical-experimentalcomparison with the results <strong>of</strong> the pseudo-dynamic tests on the four-storey <strong>RC</strong>buil<strong>di</strong>ng reported in (Negro and Verzeletti, 1996) (see Section 3.3). Authorshighlighted the detrimental effect <strong>of</strong> localization <strong>of</strong> ductility demand due to anirregular infill <strong>di</strong>stribution, as expected. However, authors pointed out that adetrimental effect on seismic behaviour may be expected also from a uniform


220 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infillsinfill <strong>di</strong>stribution since storey-level sidesway mechanisms take place after thefailure <strong>of</strong> the panels at that storey, thus lea<strong>di</strong>ng to a similar effect <strong>of</strong> localization<strong>of</strong> ductility demand. This effect may or may not be counterbalanced by thebeneficial effect due to the increase in stiffness, strength and energy <strong>di</strong>ssipationcapacity provided by infills.Fajfar and Drobnič (1998) also presented a comparison between nonlineardynamic analyses and the results from the same test (Negro and Verzeletti,1996), coming to similar conclusions. Moreover, authors carried out StaticPush-Over analyses on the numerical models <strong>of</strong> tested structures and executed aspectral assessment <strong>of</strong> the seismic demand by means <strong>of</strong> the N2 method. Anidealized bilinear force-<strong>di</strong>splacement relationship was used to represent thenumerical response also for the infilled structure, in spite <strong>of</strong> the degra<strong>di</strong>ngbehaviour due to the failure <strong>of</strong> infills (see Figure 4.2.1). To this aim, thestiffness <strong>of</strong> the idealized bilinear relationship was determined as the averagestiffness <strong>of</strong> bare frames and uniformly infilled frames, while the ultimatestrength approximately corresponded to the average strength <strong>of</strong> the uniformlyinfilled structure in the <strong>di</strong>splacement range <strong>of</strong> interest.Figure 4.2.1. Base shear-top <strong>di</strong>splacement relationships determined by pushover analyses (solidlines) and idealized bilinear relationships (dotted lines) used in the N2 method (Fajfar andDrobnič, 1998)


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 221Dolšek and Fajfar (2000, 2002) presented an investigation <strong>of</strong> modellingissues about the behaviour <strong>of</strong> infilled <strong>RC</strong> frames, confirming that a detrimentaleffect on seismic behaviour may be due not only to an irregular infill<strong>di</strong>stribution but also to a regular one. As a matter <strong>of</strong> fact, in the latter case,although reducing the <strong>di</strong>splacement demand in structural elements, presence <strong>of</strong>infills may lead to an undesirable storey mechanism, which may represent apotential danger in the case <strong>of</strong> long duration ground motion. Furthermore,authors pointed out that the major issues about the modelling <strong>of</strong> infilledstructures were the determination <strong>of</strong> the characteristics <strong>of</strong> the equivalent strutsrepresenting the infill, due to the high uncertainties involved in thisdetermination, and the characteristics <strong>of</strong> ground motion. Hence, the need for thedevelopment <strong>of</strong> simplified procedures provi<strong>di</strong>ng rough estimates <strong>of</strong> seismicresponse <strong>of</strong> infilled structures and allowing quick analysis <strong>of</strong> a number <strong>of</strong>variants was highlighted.In Dolšek and Fajfar (2001) – starting from the observation <strong>of</strong> damage toinfilled <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> after the 1999 Kocaeli earthquake – nonlinear dynamicanalyses were carried out on numerical models representing two <strong>di</strong>fferentstructures, one (“contemporary”) designed for a base shear coefficient equal to0.15 and complying with Capacity Design principles (e.g., weak beam/strongcolumn con<strong>di</strong>tion) and the other one (“<strong>existing</strong>”) designed for a base shearcoefficient equal to 0.08 and without applying Capacity Design principles.These models represented the test structures reported in (Negro and Verzeletti,1996) and (Pinto et al., 2002), respectively (see Section 3.3). Both structureswere uniformly infilled, considering two <strong>di</strong>fferent cases for infill mechanicalcharacteristics, namely “weak” and “strong” infills. Nonlinear dynamic analyseswere carried out with increasing ground motion intensity. Numerical resultshighlighted that uniformly <strong>di</strong>stributed infills led to a beneficial reduction in<strong>di</strong>splacement demand up to a certain intensity <strong>of</strong> ground motion, but if thisthreshold (that increased with the infill strength) was exceeded a s<strong>of</strong>t storeymechanism occurred at one <strong>of</strong> the bottom storeys, resulting in a sudden increase


222 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infillsin (localized) <strong>di</strong>splacement demand. In the contemporary <strong>RC</strong> frame theobserved <strong>di</strong>splacement demand was generally lower if compared with the<strong>existing</strong>, but a concentration <strong>of</strong> <strong>di</strong>splacement demand was anyhow observed atthe bottom <strong>of</strong> the structure when weak infills were considered. Hence, thecon<strong>di</strong>tions for a collapse due to the formation <strong>of</strong> such a collapse mechanism inuniformly infilled structure were (i) a high ground motion intensity, (ii) a lowglobal and local ductility <strong>of</strong> the bare frame and (iii) a low infill strength.A fundamental work for the assessment <strong>of</strong> seismic performance <strong>of</strong> infilled<strong>RC</strong> frames was presented by Dolšek and Fajfar (2004a). In this study, a R-µ-Trelationship for the evaluation <strong>of</strong> inelastic <strong>di</strong>splacement demand starting fromelastic demand spectra was presented, which was evaluated on SDOF systemscharacterized by the typical idealized force-<strong>di</strong>splacement envelope <strong>of</strong> an infilled<strong>RC</strong> frame, <strong>di</strong>fferent from the usual elasto-plastic system (see Figure 4.2.2).Figure 4.2.2. Force-<strong>di</strong>splacement envelope <strong>of</strong> the SDOF system (Dolšek and Fajfar, 2004a)The first, equivalent elastic part represented both the initial elasticbehaviour and the behaviour after cracking has occurred in both the frame andthe infills. The second part, correspon<strong>di</strong>ng to the horizontal branch, representedyiel<strong>di</strong>ng. The third part represented the strength degradation <strong>of</strong> the infills. Then,the horizontal branch represents the stage when infills are failed and only the<strong>RC</strong> frame resists the horizontal actions.


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 223A parametric study was carried out executing nonlinear dynamic analyseson the considered SDOF system with three sets <strong>of</strong> 7 accelerograms, varying<strong>di</strong>fferent parameters:- T/T C : ratio between the period <strong>of</strong> the SDOF system and the cornerperiod <strong>of</strong> the ground motion;- r u : ratio between the residual strength and the maximum strength(F 3 /F 1 , see Figure 4.2.2);- µ s : ductility at the beginning <strong>of</strong> the degradation (D 2 /D 1 );- µ u : ductility at the end <strong>of</strong> the degradation (D 3 /D 1 ).First two sets <strong>of</strong> accelerograms were used to evaluate the R-µ-Trelationship, the third one was used to validate the same relationship.Based on obtained results, an increase in ductility demand was observedwith r u decreasing. Moreover, it was observed that µ u had a negligible influenceon ductility demand. Hence, this parameter was not included in the proposedrelationship, which is shown in Figure 4.2.3.Based on the proposed R-µ-T relationship, seismic assessment <strong>of</strong> infilled<strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> can be included within the spectral framework <strong>of</strong> the N2 method,through Static Push-Over analyses.The applicability <strong>of</strong> such relationship was validated in a companion paper(Dolšek and Fajfar, 2005) through a comparison between a seismic assessmentcarried out by means <strong>of</strong> the N2 method, employing such relationship, and theresults obtained by Incremental Dynamic Analysis (IDA) on two uniformlyinfilled case study <strong>RC</strong> structures, one contemporary and one <strong>existing</strong> (see(Dolšek and Fajfar, 2001)). In this study, a methodology to evaluate theidealized multi-linear curve from the Push-Over curve for infilled <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>was also proposed.


224 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infillsFigure 4.2.3. Comparison between the R-µ-T relationship for an infilled <strong>RC</strong> frame proposed in(Dolšek and Fajfar, 2004a) and the R-µ-T relationship for an elasto-plastic system withoutstrength degradation (from (Dolšek and Fajfar, 2008a))It can also be observed that, from a qualitative standpoint, based on thisrelationship, the sudden increase in <strong>di</strong>splacement demand observed when as<strong>of</strong>t-storey occurs in uniformly infilled structures for a seismic demandexcee<strong>di</strong>ng a certain threshold (Dolšek and Fajfar, 2001) may be explained notonly by the localization <strong>of</strong> the <strong>di</strong>splacement demand, but also by the typicalbrittle behaviour shown by the structural response when this is controlled by theresponse <strong>of</strong> a storey where the infills fail; such a strength drop is representedthrough the parameter r u .The N2 method extended with the above illustrated relationship was appliedto the seismic assessment <strong>of</strong> infilled <strong>RC</strong> frames also in (Dolšek and Fajfar,2008a). In this work, a case study <strong>RC</strong> frame was considered, based on a tested


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 225structure (see (Pinto et al., 2002)), and was analyzed in <strong>di</strong>fferent configurations:Bare, Partially Infilled (infills with openings) and Fully Infilled. Based onnumerical results, authors pointed out again that infills may significantly reducedamage, but only up to a certain intensity <strong>of</strong> ground motion. Above thisthreshold level, a small increase in the ground motion intensity leads to a verysignificant drop <strong>of</strong> strength, due to the failure <strong>of</strong> infills, resulting in a severeincrease in <strong>di</strong>splacement demand.In the companion paper (Dolšek and Fajfar, 2008b) the seismic assessment<strong>of</strong> infilled <strong>RC</strong> frames is considered in a probabilistic framework, combining theSAC/FEMA method for a probability assessment in closed form (Cornell et al.,2002) with the N2 method. In the paper, the relationship between seismicdemand (represented by an Engineering Demand Parameter (EDP)) and seismicintensity (represented by an Intensity Measure (IM)) is not represented by IDAcurves but by IN2 curves, obtained applying the N2 method for increasinglevels <strong>of</strong> seismic intensity (Dolšek and Fajfar, 2004b). Hence, an evaluation <strong>of</strong>the influence <strong>of</strong> infills on seismic response could be made in terms <strong>of</strong> failureprobability, for <strong>di</strong>fferent Limit States. Based on obtained results, the beneficialinfluence <strong>of</strong> infills was even more evident than in the companion paper (Dolšekand Fajfar, 2008a). When evaluating failure probabilities, authors observed that,despite the higher inherent uncertainty in their capacity and response, regularinfilled frames were less sensitive to randomness and uncertainty. Nevertheless,authors highlighted that <strong>di</strong>fferent kind <strong>of</strong> failures, which were not considered inthe study (such as brittle failure mechanisms due to local interaction betweeninfills and structural elements), may change the results lea<strong>di</strong>ng to the illustratedconclusions.Another study assessing the seismic performance <strong>of</strong> <strong>RC</strong> frames with infillswas proposed by Dymiotis et al. (2001). In this paper, the seismic reliability <strong>of</strong>an infilled <strong>RC</strong> frame was evaluated focusing the attention on uncertainties inmaterial characteristics (both in reinforced concrete and in masonry infills) andon deformation capacity <strong>of</strong> <strong>RC</strong> members. The considered frame was designed


226 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infillsaccor<strong>di</strong>ng to Eurocode 8 (CEN, 1995), for the interme<strong>di</strong>ate ductility class and adesign PGA equal to 0.25g. <strong>Seismic</strong> performance was evaluated at two LimitStates (Serviceability (SLS) and Ultimate (ULS)). Vulnerability curves wereevaluated through nonlinear dynamic analyses carried out for <strong>di</strong>fferent levels <strong>of</strong>ground motion intensity. Two configurations were considered: Uniformlyinfilled and Pilotis frame. Results for Bare frame were available from aprevious study (Dymiotis et al., 1999). Authors observed that the Pilotis framewas more vulnerable than the Uniformly infilled frame, at both Limit States.Compared with the Bare frame, the Uniformly infilled frame was lessvulnerable at SLS but more vulnerable at ULS. The Pilotis frame resulted as themost vulnerable system at both SLS and ULS (see Figure 4.2.4).Figure 4.2.4. Comparison between <strong>vulnerability</strong> curves for Bare, Uniformly infilled and Pilotisframes for Serviceability and Ultimate Limit States (Dymiotis et al., 2001)<strong>Seismic</strong> performance <strong>of</strong> infilled <strong>RC</strong> frames were also stu<strong>di</strong>ed by Madan andHashmi (2008), considering seven and fourteen-storey infilled <strong>RC</strong> framessubjected to near-fault ground motions. Sattar and Liel (2010) evaluated


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 227<strong>vulnerability</strong> curves at collapse for a four- and a eight-storey old seismicdesigned <strong>RC</strong> frame, in Bare, Uniformly infilled and Pilotis configurations. IDAanalyses were performed; modelled uncertainty only consisted in record-torecord variability. For both four- and eight-storey frames, the Uniformly infilledconfiguration resulted as the most vulnerable, whereas the Bare frame resultedas the less vulnerable.In conclusion, based on the illustrated numerical stu<strong>di</strong>es, <strong>of</strong>ten supported byexperimental data or observed damage, the following general conclusions canbe drawn:- an irregular <strong>di</strong>stribution <strong>of</strong> infills (s<strong>of</strong>t-storey effect) results in a worseseismic performance through a detrimental localization <strong>of</strong> inelastic<strong>di</strong>splacement demand in the storey where infills are not present;- a regular <strong>di</strong>stribution <strong>of</strong> infills may lead to a beneficial reduction in<strong>di</strong>splacement demand compared with the bare structure, especially ifthe seismic demand intensity does not overcome a certain threshold(e.g., for Damage Limitation Limit State);- as the seismic demand intensity increases (e.g., for Collapse LimitState), a detrimental localization <strong>of</strong> inelastic <strong>di</strong>splacement demandtakes place also in the case <strong>of</strong> uniform infill <strong>di</strong>stribution since the<strong>di</strong>splacement demand tends to concentrate in one storey, thus resultingin a worse seismic performance compared with the bare structure;- previous considerations are strongly dependent (i) on the design <strong>of</strong> thebare structure, both in terms <strong>of</strong> strength (e.g., base shear coefficient)and application <strong>of</strong> Capacity Design principles such as weakbeam/strong column con<strong>di</strong>tion, and (ii) on the strength <strong>of</strong> infills.


228 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills4.3 SEISMIC CAPACITY ASSESSMENT OF A FOUR-STOREY GLDBUILDING WITH DIFFERENT INFILL CONFIGURATIONSIn this Section, the influence <strong>of</strong> infills on the seismic behaviour <strong>of</strong> <strong>existing</strong><strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> is evaluated on a case-study Gravity Load Designed buil<strong>di</strong>ng with<strong>di</strong>fferent infill configurations are considered (Bare, Uniformly infilled andPilotis). <strong>Seismic</strong> response is evaluated through Static Push-Over analyses.<strong>Seismic</strong> demand is assessed by means <strong>of</strong> the N2 method.In Section 4.3.1 the case study buil<strong>di</strong>ng is described, together with theadopted modelling and analysis method.The results <strong>of</strong> a sensitivity analysis evaluating the influence <strong>of</strong> mainmaterial and capacity parameters on the seismic response <strong>of</strong> the buil<strong>di</strong>ng arepresented in Section 4.3.2.A comparison between the seismic capacity <strong>of</strong> the buil<strong>di</strong>ng in <strong>di</strong>fferent infillconfigurations is shown in Section 4.3.3.In Section 4.3.4 a comparison between the seismic capacity assessmentbased on “exact” models and on correspon<strong>di</strong>ng Shear Type models is carriedout, in view <strong>of</strong> the simplified approach developed in next Chapter.4.3.1. Case study structure: numerical modelling and analysis methodologyThe case study structure is a Gravity Load Designed buil<strong>di</strong>ng, defined bymeans <strong>of</strong> a simulated design procedure accor<strong>di</strong>ng to code prescriptions anddesign practices in force in Italy between 1950s and 1970s (RDL 2229, 1939;Verderame et al., 2010a). The buil<strong>di</strong>ng is symmetric in plan, both inlongitu<strong>di</strong>nal (X) and in transversal (Y) <strong>di</strong>rection. It is a four-storey buil<strong>di</strong>ng,with five bays in longitu<strong>di</strong>nal <strong>di</strong>rection and three bays in transversal <strong>di</strong>rection.Interstorey height is equal to 3.0 m, bay length is equal to 4.5 m. The structuralconfiguration follows the parallel plane frames system: gravity loads from slabsare carried only by frames in longitu<strong>di</strong>nal <strong>di</strong>rection. Beams in transversal<strong>di</strong>rection are present only in the external frames. Slab way is always parallel tothe transversal <strong>di</strong>rection. Element <strong>di</strong>mensions are calculated accor<strong>di</strong>ng to the


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 229allowable stresses method; the design value for maximum concretecompressive stress is assumed equal to 5.0 and 7.5 MPa for axial load and axialload combined with ben<strong>di</strong>ng, respectively. Column <strong>di</strong>mensions are calculatedaccor<strong>di</strong>ng only to the axial load, beam <strong>di</strong>mensions and reinforcement aredetermined from ben<strong>di</strong>ng due to loads from slabs. Reinforcement in columnscorresponds to the minimum amount <strong>of</strong> 0.8% <strong>of</strong> the section area, as prescribedby code (RDL 2229, 1939). Reinforcing bars are smooth.Three hypotheses are made for the infill:- Case 1: infill panels are uniformly <strong>di</strong>stributed along the height(Uniformly infilled frame, see Figure 4.3.1.1).- Case 2: first storey is bare and upper storeys are infilled (Pilotis frame,see Figure 4.3.1.2).- Case 3: no infill panel is present (Bare frame, see Figure 4.3.1.3).Infills panels, if present, are uniformly <strong>di</strong>stributed in all the external frames<strong>of</strong> the buil<strong>di</strong>ng. Panel thickness is equal to 20cm. Presence <strong>of</strong> openings is nottaken into account.Figure 4.3.1.1. Uniformly infilled frame


230 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infillsFigure 4.3.1.2. Pilotis frameFigure 4.3.1.3. Bare frameNonlinear response <strong>of</strong> <strong>RC</strong> elements is modelled by means <strong>of</strong> a lumpedplasticity approach: beams and columns are represented by elastic elementswith rotational hinges at the ends. A three-linear envelope is used, characteristic


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 231points are cracking, yiel<strong>di</strong>ng and ultimate. Section moment and curvature atcracking and yiel<strong>di</strong>ng are calculated on a fiber section, for an axial load valuecorrespon<strong>di</strong>ng to gravity loads. The behaviour is assumed linear elastic up tocracking and perfectly-plastic after yiel<strong>di</strong>ng. Rotations at yiel<strong>di</strong>ng and ultimateare evaluated through the formulations given in (Far<strong>di</strong>s, 2007) (see Section2.2.1.1, Eq. 2.2.1.7). No reduction <strong>of</strong> ultimate rotation for the lack <strong>of</strong> seismicdetailing is applied, due to the presence <strong>of</strong> smooth reinforcement (see Section2.2.2).Infill panels are modelled by means <strong>of</strong> equivalent struts. The adopted modelfor the envelope curve <strong>of</strong> the force-<strong>di</strong>splacement relationship is the modelproposed by Panagiotakos and Far<strong>di</strong>s (see Section 3.2.4). The ratio betweenpost-capping degra<strong>di</strong>ng stiffness and elastic stiffness (parameter α) is assumedequal to 0.03. The ratio between residual strength and maximum strength(parameter β) is assumed equal to 0.01.Nonlinear Static Push-Over (SPO) analyses are performed on the case studybuil<strong>di</strong>ng both in X and Y <strong>di</strong>rection. The assumed lateral load pattern isproportional to the <strong>di</strong>splacement shape <strong>of</strong> the first mode. Lateral response isevaluated in terms <strong>of</strong> base shear-top <strong>di</strong>splacement relationship.Structural modelling, numerical analyses and post-processing <strong>of</strong> damagedata, inclu<strong>di</strong>ng the 3D graphic visualization <strong>of</strong> the deformed shape, areperformed through the “PBEE toolbox” s<strong>of</strong>tware (Dolšek, 2010), combiningMATLAB® with OpenSees (McKenna et al., 2004). The functions for infillelements were added by the author <strong>of</strong> this thesis during a cooperation stay at theInstitute <strong>of</strong> Structural Engineering, Earthquake Engineering and Construction(IKPIR) <strong>of</strong> the Faculty <strong>of</strong> Civil and Geodetic Engineering, at the University <strong>of</strong>Ljubljana.When the lateral response is characterized by a strength degradation due toinfill failure, a multi-linearization <strong>of</strong> the pushover curve is carried out byapplying the equal energy rule respectively between the initial point and themaximum resistance point, between the maximum resistance point and thepoint correspon<strong>di</strong>ng to the last infill failure, between the point correspon<strong>di</strong>ng to


232 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infillsthe last infill failure and the point correspon<strong>di</strong>ng to the first <strong>RC</strong> elementconventional collapse.When the lateral response is not characterized by a strength degradation(because infill elements are not present or not involved in the collapsemechanism) an elasto-plastic bi-linearization is carried out by applying theequal energy rule between the initial point and the maximum resistance point.Moreover, the procedure proposed in (Dolšek and Fajfar, 2005) to improvethe accuracy <strong>of</strong> the <strong>di</strong>splacement demand assessment in the case <strong>of</strong> low seismicdemand is applied, by approximating the first part <strong>of</strong> the pushover curve by abilinear curve rather than a linear one and applying specific R-µ-T relationshipsin this range <strong>of</strong> behaviour, as proposed by the authors.Two limit states are defined: Damage Limitation (DL), correspon<strong>di</strong>ng to the<strong>di</strong>splacement when the last infill reaches its maximum resistance thus startingto degrade (Dolšek and Fajfar, 2008a) or when the first yiel<strong>di</strong>ng in <strong>RC</strong> membersoccurs, and Near Collapse (NC), correspon<strong>di</strong>ng to the first conventionalcollapse in <strong>RC</strong> members.Then, the IN2 curves (Dolšek and Fajfar, 2004b) for the equivalent SDOFsystems are obtained by assuming as Intensity Measure both the elastic spectralacceleration at the period <strong>of</strong> the equivalent SDOF system (S ae (T eff )) and thePeak Ground Acceleration (PGA). Values <strong>of</strong> these seismic intensity parameterscorrespon<strong>di</strong>ng to characteristic values <strong>of</strong> <strong>di</strong>splacement (ductility) demand(inclu<strong>di</strong>ng the considered Limit States) are calculated, based on the R-µ-Trelationships given in (Dolšek and Fajfar, 2004a) or in (Fajfar, 1999) fordegra<strong>di</strong>ng or non-degra<strong>di</strong>ng response, respectively.Elastic spectra are the Uniform Hazard Newmark-Hall demand spectraadopted in Italian code (DM 14/1/2008) – provided in (INGV-DPC S1, 2007) –for a high seismic city in Southern Italy (Avellino, Lon.: 14.793 Lat.: 40.915).Soil type A (stiff soil) and 1 st topographic category are assumed (noamplification for stratigraphic or topographic effects).It is worth noting that a double iterative procedure is required to evaluateS ae (T eff ) and PGA from the characteristic parameters <strong>of</strong> equivalent SDOF


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 233system – namely the ductility at the point <strong>of</strong> interest (µ), the period (T eff ) andfor degra<strong>di</strong>ng systems also the ductility at the beginning <strong>of</strong> the degradation (µ s )and the ratio between the residual strength and the maximum strength (r u ) – forthe following reasons:- the spectral shape depends on some parameters, such as the cornerperiod (T C ) and the ratio between the spectral acceleration on theconstant branch and the PGA (F 0 ), which are not constant with theseismic intensity (i.e., with the return period), hence also the ratiobetween S ae (T eff ) and PGA changes with the seismic intensity;- some characteristic parameters <strong>of</strong> the elastic spectrum, such as T C , areinput parameters for the R-µ-T relationship, but also depends on theresults obtained from the R-µ-T relationship since they depends on theseismic intensity.Due to the fact that the ratio between S ae (T eff ) and PGA is not constant, theIN2 curves in terms <strong>of</strong> S ae (T eff ) or in terms <strong>of</strong> PGA may have <strong>di</strong>fferent shapes.Demand spectra are provided in (INGV-DPC S1, 2007) in terms <strong>of</strong>parameters PGA, F 0 and T C * (which is multiplied by another coefficientdepen<strong>di</strong>ng on stratigraphic characteristics, C C , to obtain T C ) for a range <strong>of</strong>return periods from 30 to 2475 years. For interme<strong>di</strong>ate values <strong>of</strong> seismicintensity, an interpolation procedure is proposed (DM 14/1/2008). Nevertheless,in this study there is the need to extend elastic demand spectra above and belowthe extreme values, as in (Crowley et al., 2009). To this aim, the formulationsproposed for the interpolation procedure are also used to extrapolate the abovementioned parameters out <strong>of</strong> the given range <strong>of</strong> values.In order to evaluate the influence <strong>of</strong> material characteristics and elementcapacity on the seismic response <strong>of</strong> the case study structure, the followingparameters are selected as Random Variables to carry out a sensitivity analysis(Section 4.3.2) and an based on the Response Surface Method (Section 4.3.2):- Concrete compressive strength f c ;


234 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills- Steel yield strength f y ;- Infill shear elastic modulus G w ;- Rotation at yiel<strong>di</strong>ng in <strong>RC</strong> members θ y ;- Rotation at ultimate in <strong>RC</strong> members θ u .A lognormal <strong>di</strong>stribution is assumed for all <strong>of</strong> the Random Variables. Each<strong>di</strong>stribution is defined through the central (me<strong>di</strong>an) value and the Coefficient <strong>of</strong>Variation (CoV).For the concrete compressive strength, reference values come from astatistical analysis on the mechanical properties <strong>of</strong> concrete employed in Italyduring 1960s (Verderame et al., 2001).For the steel yield strength, values are referred to Aq50 steel typology, themost widely spread in Italy during 1960s (Verderame et al., 2010b).The determination <strong>of</strong> infill material characteristics is affected by high<strong>di</strong>fficulties and uncertainties, and literature does not <strong>of</strong>fer an enough largeamount <strong>of</strong> experimental data. In this study, a me<strong>di</strong>an value <strong>of</strong> 1240 MPa for theshear elastic modulus G w is adopted, provided in (Far<strong>di</strong>s, 1997), based onwallette tests carried out at the University <strong>of</strong> Pavia on specimens made up <strong>of</strong>hollow clay bricks with a void ratio <strong>of</strong> 42%, selected as representative <strong>of</strong> typicallight non-structural masonry. Nevertheless, there are further infill mechanicalcharacteristics to be determined in order to define, accor<strong>di</strong>ng to the adoptedmodel, the load-<strong>di</strong>splacement relationship <strong>of</strong> the infill trusses, namely theelastic Young’s modulus E w and the shear cracking stress τ cr . A certain amount<strong>of</strong> correlation certainly exists between these parameters, although it is not easyat all to be determined. In this study, a fully correlation is assumed, based onthe proposal <strong>of</strong> the Italian code (Circolare 617, 2009) for the mechanicalcharacteristics <strong>of</strong> hollow clay brick panels. Hence, the ratio between E w and G wis assumed equal to 10/3, whereas τ cr is assumed as linearly dependent on G w ,assuming τ cr equal to 0.3 and 0.4 MPa for G w equal to 1080 and 1620 MPa,respectively. As far as the modelling <strong>of</strong> uncertainty in infill mechanicalcharacteristics is concerned, some in<strong>di</strong>cations can be drawn from literature: in(Dymiotis et al., 2001) the authors state that “the model uncertainty in


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 235pre<strong>di</strong>cting the masonry capacity may be accounted for effectively through theuse <strong>of</strong> two model uncertainty factors. These relate to the maximum shear stressand the area under the τ-γ envelope curve up to γ = 3γ max ”. In particular, theauthors refer to the envelope for infill response proposed in (Valiasis, 1989).Referring to these parameters the authors write that “the model uncertaintyvariables X m,τmax and X m,A , which are ratios <strong>of</strong> experimental to analyticalvalues, may be described by lognormal <strong>di</strong>stributions with mean values <strong>of</strong> 0.88and 0.95 and coefficients <strong>of</strong> variation (COV) <strong>of</strong> 26 and 19%, respectively”. In(Rossetto and Elnashai, 2005) the authors assume for the random variable“infill compressive strength” a lognormal <strong>di</strong>stribution with a CoV equal to 0.20.They write that “the probability <strong>di</strong>stribution functions assigned to eachmaterial property for the assessment <strong>of</strong> the example infilled frame population[…] were determined through consideration <strong>of</strong> numerous tests on Europeanconstruction materials dating from the assumed time <strong>of</strong> construction, (e.g. Pipaand Carvalho, Petersons, amongst others)”, but they do not specify clearlywhat was the reference used to establish the assumed value <strong>of</strong> CoV for the infillcompressive strength. In (Calvi et al., 2004) the authors describe theexperimental results from 20 experimental test on small size wallettes. Theywrite that “the low absolute values for compression and tensile strength and thevery large <strong>di</strong>spersion <strong>of</strong> the stiffness values […] are considered to berepresentative <strong>of</strong> infill panels commonly constructed in the Me<strong>di</strong>terraneanarea”. CoV values <strong>of</strong> 0.25 and 0.36 are provided for the tensile strength and forthe shear elastic modulus, respectively. Based on these in<strong>di</strong>cations, a CoV equalto 0.30 is assumed for G w .As far as deformations at yiel<strong>di</strong>ng and ultimate in <strong>RC</strong> members areconcerned, me<strong>di</strong>an and CoV values are evaluated starting from the valuescalculated through the formulations proposed in (Far<strong>di</strong>s, 2007) and usingme<strong>di</strong>an and CoV values <strong>of</strong> the experimental-to-pre<strong>di</strong>cted ratio, as illustrated bythe author.A summary <strong>of</strong> me<strong>di</strong>an and CoV values for the selected Random Variables isreported in Table 4.3.1.1.


236 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infillsR.V. Me<strong>di</strong>an Value Reference Distrib. CoV Referencef cf y25.0 MPa369.7 MPaVerderame et al.,2001Verderame et al.,2010bLognormal 0.31Lognormal 0.08Verderame et al.,2001Verderame et al.,2010bG w 1240 MPa Far<strong>di</strong>s, 1997 Lognormal 0.30 -θ yθ u1.015*calculatedFar<strong>di</strong>s, 2007Far<strong>di</strong>s, 2007Lognormal 0.331(Eq. 2.20a, Table 2.4)(Table 2.4)0.995*calculatedFar<strong>di</strong>s, 2007Far<strong>di</strong>s, 2007Lognormal 0.409(Eq. 3.27a, Table 3.2)(Table 3.2)Table 4.3.1.1. Summary <strong>of</strong> me<strong>di</strong>an and CoV values for the selected Random Variables4.3.2. Sensitivity analysisBased on the assumed Random Variables, a sensitivity analysis is carriedout to investigate the influence <strong>of</strong> each variable on the seismic capacity <strong>of</strong> thecase study structure. To this aim, two models are generated for each randomvariable assuming me<strong>di</strong>an-minus-1.7-standard-deviation and me<strong>di</strong>an-plus-1.7-standard-deviation values for the considered variable, and me<strong>di</strong>an values for theremaining variables. The choice <strong>of</strong> these values will be better explained in nextSection, when the Response Surface Method will be used for the generation <strong>of</strong><strong>vulnerability</strong> curves for the case study structure.In ad<strong>di</strong>tion to these analyses, another one is carried out assuming me<strong>di</strong>anvalues for all <strong>of</strong> the variables (Model #1).In the following, obtained results are presented and <strong>di</strong>scussed for Uniformlyinfilled, Pilotis and Bare frames, in both longitu<strong>di</strong>nal (X) and transversal (Y)<strong>di</strong>rections and at Damage Limitation and Near Collapse Limit States. The [top<strong>di</strong>splacement, S ae (T eff )] and [top <strong>di</strong>splacement, PGA] points on IN2 curvescorrespon<strong>di</strong>ng to DL and NC Limit State are reported as yellow and red circles,respectively.


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 237The results will be reported accor<strong>di</strong>ng to the following notation:VariableSymbolElastic period [sec]T elMDOF <strong>di</strong>splacement capacity at last infill maximum [m]∆ limMDOF <strong>di</strong>splacement capacity at first yiel<strong>di</strong>ng in <strong>RC</strong> members [m]∆ f<strong>RC</strong>yMDOF <strong>di</strong>splacement capacity at first <strong>RC</strong> element collapse [m]∆ collapseMaximum base shear [kN]V b,maxModal participation factorΓEffective mass [t] m*Period <strong>of</strong> the equivalent SDOF system [sec]T effDisplacement at yiel<strong>di</strong>ng <strong>of</strong> the equivalent SDOF system [m]S dyDuctility at the beginning <strong>of</strong> the degradationµ sDuctility at the end <strong>of</strong> the degradationµ uMaximum inelastic acceleration capacity (=S ay ) [g]C s,maxMinimum inelastic acceleration capacity [g]C s,minRatio between C s,min and C s,maxr uDuctility at last infill maximumµ limDuctility at first yiel<strong>di</strong>ng in <strong>RC</strong> membersµ f<strong>RC</strong>yDuctility at first <strong>RC</strong> element collapseµ collapseElastic spectral acceleration (at T eff ) lea<strong>di</strong>ng to ductility demand equal to µ s [g] S ae,sElastic spectral acceleration (at T eff ) lea<strong>di</strong>ng to last infill maximum [g]S ae,limElastic spectral acceleration (at T eff ) lea<strong>di</strong>ng to first yiel<strong>di</strong>ng in <strong>RC</strong> members [g] S ae,f<strong>RC</strong>yElastic spectral acceleration (at T eff ) lea<strong>di</strong>ng to collapse [g]S ae,collapseRatio between S ae,s and S ayR sRatio between S ae,lim and S ayR limRatio between S ae,f<strong>RC</strong>y and S ayR f<strong>RC</strong>yRatio between S ae,collapse and S ayR collapsePeak ground acceleration lea<strong>di</strong>ng to ductility demand equal to µ s [g]PGA sPeak ground acceleration lea<strong>di</strong>ng to last infill maximum [g]PGA limPeak ground acceleration lea<strong>di</strong>ng to first yiel<strong>di</strong>ng in <strong>RC</strong> members [g]PGA lf<strong>RC</strong>yPeak ground acceleration lea<strong>di</strong>ng to collapse [g]PGA collapseChange in PGA collapse compared with Model #1 [%]∆ PGA,NCChange in PGA lim compared with Model #1 [%]∆ PGA,limChange in PGA f<strong>RC</strong>y compared with Model #1 [%]∆ PGA,f<strong>RC</strong>yIt is to be noted that the influence <strong>of</strong> each single variable, which will beillustrated through the sensitivity analysis, not only depends on the influence <strong>of</strong>the variable on the seismic response, but also depends on the assumed


238 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills<strong>di</strong>spersion for that variable. As a matter <strong>of</strong> fact, the amount <strong>of</strong> <strong>di</strong>spersionconsidered for the variable (through the assigned Coefficient <strong>of</strong> Variation) leadsto consider – as Lower and Upper limits – values more or less <strong>di</strong>stant from thecentral (me<strong>di</strong>an) value. A variable characterized by a lower uncertainty (i.e., alower CoV) will have me<strong>di</strong>an-minus-1.7-standard-deviation and me<strong>di</strong>an-plus-1.7-standard-deviation values closer to the me<strong>di</strong>an value, and vice versa.Hence, the amount <strong>of</strong> the change in PGA capacity due to the change in eachvariable, compared with the model where me<strong>di</strong>an values are assigned to allvariables (Model #1), should be interpreted taking into account also the CoVvalue assigned to each variable.


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 2394.3.2.1 Uniformly Infilled frameX <strong>di</strong>rection2.52S ae(T eff) [g]1.510.500 0.02 0.04 0.06 0.08 0.1 0.12 0.14Top <strong>di</strong>splacement in X <strong>di</strong>rection [m]Figure 4.3.2.1. Pushover and IN2 curves for Model #1 (Uniformly Infilled frame – X <strong>di</strong>rection)Figure 4.3.2.2. Deformed shape and element damage for Model #1 at NC (Uniformly Infilledframe – X <strong>di</strong>rection)


240 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infillsSensitivity analysisthufcVariableGwfythyUpper valueLower value-60 -40 -20 0 20 40 60Change in PGA at collapse (%)Figure 4.3.2.3. Results <strong>of</strong> sensitivity analysis for NC LS (Uniformly Infilled frame – X<strong>di</strong>rection)Pushover and IN2 curves for Model #1 in X <strong>di</strong>rection are reported in Figure4.3.2.1. Results <strong>of</strong> sensitivity analysis for NC and DL Limit States are reporte<strong>di</strong>n Figures 4.3.2.3 and 4.3.2.8, respectively.The buil<strong>di</strong>ng collapses under a s<strong>of</strong>t-storey mechanism at the 1 st storey in allcases except when a lower value is assumed for infill mechanicalcharacteristics: in this case there is a s<strong>of</strong>t-storey mechanism at the 2 nd storey.The sensitivity analysis shows that θ u has the highest influence on the PGAat collapse. This is clearly due to the fact the <strong>di</strong>splacement capacity at collapseis <strong>di</strong>rectly given by the rotational capacity <strong>of</strong> columns, given the s<strong>of</strong>t-storeycollapse mechanism. Thus, an increase in θ u results in an increase in ∆ collapse ,that is, an increase in µ collapse , lea<strong>di</strong>ng to higher values <strong>of</strong> S ae,collapse (see Figure4.3.2.4) and, hence, <strong>of</strong> PGA collapse (see Figure 4.3.2.5). Vice versa if θ udecreases.f c influences the collapse capacity through the value <strong>of</strong> θ u : given equal theaxial load, as f c increases the axial load ratio decreases and the rotational


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 241capacity <strong>of</strong> the columns increases, thus lea<strong>di</strong>ng to a higher global ductility. Viceversa if f c decreases.When E w , G w and τ cr increase, several effects can be observed: the increasein stiffness and strength leads to a lower T eff and a higher C s,max ; C s,min does notchange significantly, hence a decrease in r u is observed. ∆ collapse does not changesignificantly, but the decrease in S dy leads to an increase in µ collapse .In R-µ-T relationships, as T eff decreases, given equal the ductility µ, Rdecreases too; as µ increases, given equal the period T eff , R increases. If theeffective stiffness <strong>of</strong> the equivalent system increases but the strength and the<strong>di</strong>splacement capacity do not change (i.e., only a decrease in S dy is observed),both these effects are observed (decrease in T eff and increase in µ) but the lattertends to prevail over the former, lea<strong>di</strong>ng to a higher R.Nevertheless, in our case the increase in µ collapse is only given by thedecrease in S dy , whereas the decrease in T eff is given not only by the lower S dybut also by the higher C s,max . Hence, the effect <strong>of</strong> the decrease in T eff prevailsover the increase in µ collapse , finally lea<strong>di</strong>ng to a lower value <strong>of</strong> R.Moreover, the detrimental effect <strong>of</strong> the decrease in r u also leads to a lowervalue <strong>of</strong> R. Hence, these effects globally lead to a much lower value <strong>of</strong> R collapse ;however, the higher base shear capacity C s,max leads to a value <strong>of</strong> S ae,collapse onlyslightly lower, compared with Model #1 (see Figure 4.3.2.6). Nevertheless, dueto the decrease in T eff , this lower value <strong>of</strong> S ae,collapse corresponds to a highervalue <strong>of</strong> PGA collapse (see Figure 4.3.2.7).When E w , G w and τ cr decrease, the buil<strong>di</strong>ng collapses under a s<strong>of</strong>t-storeymechanism at the 2 nd storey instead <strong>of</strong> the 1 st one. From a qualitativestandpoint, a higher infill strength leads to a more uniform <strong>di</strong>stribution <strong>of</strong>maximum interstorey shear strength along the height <strong>of</strong> the buil<strong>di</strong>ng: moreuniform is this <strong>di</strong>stribution, higher is the probability to have a s<strong>of</strong>t storeymechanism at the 1 st storey, where the shear demand is higher. For the samereasons, a lower infill strength may lead to the formation <strong>of</strong> a s<strong>of</strong>t-storeymechanism at the 2 nd storey instead <strong>of</strong> the 1 st one. At the 2 nd storey the strength<strong>of</strong> <strong>RC</strong> columns is lower, thus lea<strong>di</strong>ng to a lower value <strong>of</strong> the residual strength


242 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infillsC s,min , which is essentially due to the contribution <strong>of</strong> <strong>RC</strong> frame due to thefailure <strong>of</strong> infills.Opposite observations, compared with the previous case, can be made: thedecrease in stiffness and strength leads to a higher T eff and a lower C s,max ;hence, an increase in r u is observed. ∆ collapse does not change significantly, butthe increase in S dy leads to a decrease in µ collapse . These effects globally lead to amuch higher value <strong>of</strong> R collapse ; however, the lower base shear capacity C s,maxleads to a lower value <strong>of</strong> S ae,collapse compared with Model #1 (see Figure4.3.2.6), also resulting in a lower PGA collapse (see Figure 4.3.2.7).The only parameter significantly influenced by f y is the residual base shearC s,min . An increase in f y results in a higher C s,min , thus lea<strong>di</strong>ng to a higher r u .This beneficial effect results in a higher R collapse , lea<strong>di</strong>ng to higher values <strong>of</strong>S ae,collapse and PGA collapse . Vice versa if f y decreases.The rotation at yiel<strong>di</strong>ng θ y has no significant influence on PGA capacity atcollapse.


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 2433.532.5S ae(T eff) [g]21.510.500 0.05 0.1 0.15 0.2 0.25 0.3 0.35Top <strong>di</strong>splacement in X <strong>di</strong>rection [m]Figure 4.3.2.4. Pushover and IN2 curves in terms <strong>of</strong> S ae (T eff ) for Models #10, #1 and #11:Lower, Me<strong>di</strong>an and Upper values for θ u (Uniformly Infilled frame – X <strong>di</strong>rection)1.41.21PGA [g]0.80.60.40.200 0.05 0.1 0.15 0.2 0.25 0.3 0.35Top <strong>di</strong>splacement in X <strong>di</strong>rection [m]Figure 4.3.2.5. IN2 curves in terms <strong>of</strong> PGA for Models #10, #1 and #11: Lower, Me<strong>di</strong>an andUpper values for θ u (Uniformly Infilled frame – X <strong>di</strong>rection)


244 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills2.52S ae(T eff) [g]1.510.500 0.02 0.04 0.06 0.08 0.1 0.12 0.14 0.16Top <strong>di</strong>splacement in X <strong>di</strong>rection [m]Figure 4.3.2.6. Pushover and IN2 curves in terms <strong>of</strong> S ae (T eff ) for Models #6, #1 and #7: Lower,Me<strong>di</strong>an and Upper values for infill mechanical characteristics (Uniformly Infilled frame – X<strong>di</strong>rection)0.90.80.70.6PGA [g]0.50.40.30.20.100 0.02 0.04 0.06 0.08 0.1 0.12 0.14 0.16Top <strong>di</strong>splacement in X <strong>di</strong>rection [m]Figure 4.3.2.7. IN2 curves in terms <strong>of</strong> PGA for Models #6, #1 and #7: Lower, Me<strong>di</strong>an andUpper values for infill mechanical characteristics (Uniformly Infilled frame – X <strong>di</strong>rection)


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 245Sensitivity analysisGwfcVariablefythythuUpper valueLower value-60 -40 -20 0 20 40 60Change in PGA at last infill maximum (%)Figure 4.3.2.8. Results <strong>of</strong> sensitivity analysis for DL LS (Uniformly Infilled frame – X<strong>di</strong>rection)As far as PGA capacity at last infill maximum is concerned, from aqualitative standpoint, the same trend observed for PGA capacity at collapsewith the infill mechanical characteristics are observed. Hence, a beneficialeffect <strong>of</strong> an increase in stiffness and strength is observed.When f c increases, C s,max increases too, mainly due to the highercontribution <strong>of</strong> <strong>RC</strong> columns – due to their higher stiffness and strength – to themaximum base shear, which corresponds to the attainment <strong>of</strong> the maximumstrength in the infills in the storey involved in collapse and is attained for thesame <strong>di</strong>splacement. On the whole, the change in f c does not influencesignificantly R lim , but the increase in C s,max leads to higher values <strong>of</strong> S ae,lim andPGA lim . Vice versa if f c decreases.Remaining parameters do not have a significant influence on PGA lim .


246 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infillsY <strong>di</strong>rection21.81.61.4S ae(T eff) [g]1.210.80.60.40.200 0.02 0.04 0.06 0.08 0.1 0.12 0.14Top <strong>di</strong>splacement in Y <strong>di</strong>rection [m]Figure 4.3.2.9. Pushover and IN2 curves for Model #1 (Uniformly Infilled frame – Y <strong>di</strong>rection)Figure 4.3.2.10. Deformed shape and element damage for Model #1 at NC (Uniformly Infilledframe – Y <strong>di</strong>rection)


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 247Sensitivity analysisthufcVariableGwfythyUpper valueLower value-60 -40 -20 0 20 40 60Change in PGA at collapse (%)Figure 4.3.2.11. Results <strong>of</strong> sensitivity analysis for NC LS (Uniformly Infilled frame – Y<strong>di</strong>rection)Pushover and IN2 curves for Model #1 in Y <strong>di</strong>rection are reported in Figure4.3.2.9. Results <strong>of</strong> sensitivity analysis for NC and DL Limit States are reporte<strong>di</strong>n Figures 4.3.2.11 and 4.3.2.14, respectively.The buil<strong>di</strong>ng collapses under a s<strong>of</strong>t-storey mechanism at the 2 nd storey in allcases except when a lower value is assumed for f c and when an upper value isassumed for infill mechanical characteristics. In these cases, the storey involvedby the collapse mechanism is the 1 st one. As already highlighted, a lowerstiffness and/or strength <strong>of</strong> the <strong>RC</strong> structure and a higher strength <strong>of</strong> infills leadto a more uniform <strong>di</strong>stribution <strong>of</strong> maximum interstorey shear strength along theheight <strong>of</strong> the buil<strong>di</strong>ng: more uniform is this <strong>di</strong>stribution, higher is theprobability to have a s<strong>of</strong>t storey mechanism at the 1 st storey, where the sheardemand is higher. The attention has to be focused not only on the strength <strong>of</strong>the <strong>RC</strong> structure, but also on its stiffness. As a matter <strong>of</strong> fact, in infilled <strong>RC</strong>frames the s<strong>of</strong>t-storey collapse mechanism generally takes place at the storeywhere – under the given <strong>di</strong>stribution <strong>of</strong> lateral forces – the maximum ratiobetween the interstorey shear demand and the interstorey shear strength takes


248 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infillsplace. From a qualitative standpoint, the latter value is provided by the strengthcontribution <strong>of</strong> infills, correspon<strong>di</strong>ng to their maximum resistance and attainedfor rather low <strong>di</strong>splacement values, and by a contribution <strong>of</strong> <strong>RC</strong> columns,which at this stage <strong>of</strong> behaviour have not developed their entire strength yet.Hence, the latter contribution is significantly influenced by stiffness <strong>of</strong> <strong>RC</strong>elements, and not only by their strength.As already illustrated for the X <strong>di</strong>rection, when E w , G w and τ cr increase,several effects are observed, inclu<strong>di</strong>ng the decrease in r u , globally lea<strong>di</strong>ng to alower value <strong>of</strong> R collapse ; this effect may or may not be counterbalanced by thehigher C s,max . Opposite to X <strong>di</strong>rection, in the case <strong>of</strong> Y <strong>di</strong>rection the effect <strong>of</strong>decrease in R collapse prevails over the increase in C s,max , lea<strong>di</strong>ng to a lowerS ae,collapse (see Figure 4.3.2.12) and also to a lower PGA collapse (see Figure4.3.2.13). Vice versa when lower values <strong>of</strong> infill mechanical characteristics areconsidered.The influence <strong>of</strong> remaining parameter is quite similar to X <strong>di</strong>rection.


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 2492.52S ae(T eff) [g]1.510.500 0.02 0.04 0.06 0.08 0.1 0.12 0.14 0.16Top <strong>di</strong>splacement in Y <strong>di</strong>rection [m]Figure 4.3.2.12. Pushover and IN2 curves in terms <strong>of</strong> S ae (T eff ) for Models #6, #1 and #7: Lower,Me<strong>di</strong>an and Upper values for infill mechanical characteristics (Uniformly Infilled frame – Y<strong>di</strong>rection)0.80.70.60.5PGA [g]0.40.30.20.100 0.02 0.04 0.06 0.08 0.1 0.12 0.14 0.16Top <strong>di</strong>splacement in Y <strong>di</strong>rection [m]Figure 4.3.2.13. IN2 curves in terms <strong>of</strong> PGA for Models #6, #1 and #7: Lower, Me<strong>di</strong>an andUpper values for infill mechanical characteristics (Uniformly Infilled frame – Y <strong>di</strong>rection)


250 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infillsSensitivity analysisGwfcVariablethyfythuUpper valueLower value-60 -40 -20 0 20 40 60Change in PGA at last infill maximum (%)Figure 4.3.2.14. Results <strong>of</strong> sensitivity analysis for DL LS (Uniformly Infilled frame – Y<strong>di</strong>rection)As far as PGA capacity at last infill maximum is concerned, opposite toPGA capacity at collapse, a beneficial effect <strong>of</strong> the increase in E w , G w and τ cr isobserved; as a matter <strong>of</strong> fact, see Figure 4.3.2.12, the beneficial effect <strong>of</strong> ahigher strength (higher value <strong>of</strong> C s,max ) on the capacity – in terms <strong>of</strong> S ae (T eff ) –is more important when the ductility capacity is in a lower range <strong>of</strong> values (e.g.,DL limit state). If the ductility capacity is, on average, higher (e.g., NC limitstate), the detrimental effect <strong>of</strong> a more brittle behaviour (lower value <strong>of</strong> r u ) onthe correspon<strong>di</strong>ng capacity – expressed as S ae (T eff ) – tends to prevail. This tren<strong>di</strong>s reflected by the decrease in the slope <strong>of</strong> IN2 curves when the infillmechanical characteristics assume upper values.Based on these observations, when E w , G w and τ cr decrease a lower PGAcapacity at last infill maximum is expected. Nevertheless, due to the fullcorrelation assumed between the infill mechanical characteristics, in theadopted model a lower strength and a lower secant-to-maximum stiffness areobserved at the same time, resulting in a higher <strong>di</strong>splacement capacity at thisLimit State. This effect partially counterbalances the detrimental effect <strong>of</strong> lower


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 251initial stiffness and strength, lea<strong>di</strong>ng to a only slightly lower PGA capacity atlast infill maximum.Remaining parameters do not have a significant influence on the PGAcapacity at last infill maximum.Comparison between X and Y <strong>di</strong>rectionsIf a comparison is carried out between the seismic capacity in X and Y<strong>di</strong>rections for Model #1 (see Figures 4.3.2.15 and 4.3.2.16) it is observed howthe <strong>di</strong>splacement capacity does not change significantly and the beneficial effect<strong>of</strong> a higher strength, both maximum (C s,max ) and residual (C s,min ), leads tohigher PGA capacities in X <strong>di</strong>rection, both at collapse and last infill maximum.The higher strength in X <strong>di</strong>rection compared with Y <strong>di</strong>rection is due (i) to thelarger amount <strong>of</strong> infill panels in X <strong>di</strong>rection and (ii) to the orientation <strong>of</strong> columnelements, which, following the parallel plane frame configuration, provide ahigher strength in X <strong>di</strong>rection.2.52S ae(T eff) [g]1.510.500 0.02 0.04 0.06 0.08 0.1 0.12 0.14Top <strong>di</strong>splacement [m]Figure 4.3.2.15. Pushover and IN2 curves in terms <strong>of</strong> S ae (T eff ) for Model #1 in X and Y<strong>di</strong>rections (Uniformly Infilled frame)


252 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills0.90.80.70.6PGA [g]0.50.40.30.20.100 0.02 0.04 0.06 0.08 0.1 0.12 0.14Top <strong>di</strong>splacement [m]Figure 4.3.2.16. IN2 curves in terms <strong>of</strong> PGA for Model #1 in X and Y <strong>di</strong>rections (UniformlyInfilled frame)


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 253ModelNo.Mo<strong>di</strong>fiedVariableStoreyValue T el ∆ lim ∆ coll T eff µ s C s,max C s,min r u µ lim µ coll R lim R coll S ae,lim S ae,coll PGA lim PGA coll involved incollapse∆ PGA,NC ∆ PGA,lim1 - - 0.13 0.01 0.14 0.16 3.04 0.73 0.29 0.39 2.21 23.26 1.33 2.97 0.97 2.17 0.38 0.80 1 - -2 f cµ-1.7σ 0.13 0.01 0.11 0.16 2.89 0.70 0.26 0.37 2.23 18.74 1.34 2.62 0.94 1.84 0.37 0.69 1 -14.4 -2.53 " µ+1.7σ 0.13 0.01 0.17 0.16 2.94 0.76 0.30 0.40 2.15 27.21 1.31 3.19 0.99 2.42 0.39 0.90 1 12.3 2.54 f yµ-1.7σ 0.13 0.01 0.14 0.16 3.00 0.73 0.27 0.37 2.21 23.29 1.33 2.88 0.97 2.10 0.38 0.78 1 -3.1 0.25 " µ+1.7σ 0.13 0.01 0.14 0.16 3.04 0.73 0.30 0.41 2.20 23.28 1.33 3.08 0.97 2.24 0.38 0.83 1 3.4 -0.26 G wµ-1.7σ 0.16 0.02 0.16 0.20 3.44 0.57 0.23 0.41 2.41 20.95 1.50 3.74 0.85 2.13 0.34 0.79 2 -2.2 -10.87 " µ+1.7σ 0.10 0.01 0.14 0.13 2.57 1.00 0.29 0.29 2.21 25.46 1.25 2.01 1.26 2.02 0.52 0.85 1 6.0 35.78 θ yµ-1.7σ 0.13 0.01 0.14 0.16 3.05 0.73 0.29 0.39 2.20 23.19 1.33 2.97 0.97 2.17 0.38 0.80 1 0.0 0.19 " µ+1.7σ 0.13 0.01 0.14 0.16 3.02 0.73 0.29 0.39 2.21 23.38 1.33 2.98 0.97 2.17 0.38 0.80 1 0.1 -0.210 θ uµ-1.7σ 0.13 0.01 0.07 0.16 3.04 0.73 0.29 0.39 2.21 12.21 1.33 2.25 0.97 1.64 0.38 0.62 1 -23.0 0.011 " µ+1.7σ 0.13 0.01 0.27 0.16 3.04 0.73 0.29 0.39 2.21 44.82 1.33 4.17 0.97 3.04 0.38 1.15 1 42.6 0.0Table 4.3.2.1. Results <strong>of</strong> pushover and IN2 analyses on the Uniformly Infilled frame in X <strong>di</strong>rectionModelNo.Mo<strong>di</strong>fiedVariableStoreyValue T el ∆ lim ∆ coll T eff µ s C s,max C s,min r u µ lim µ coll R lim R coll S ae,lim S ae,coll PGA lim PGA coll involved incollapse∆ PGA,NC ∆ PGA,lim1 - - 0.17 0.02 0.15 0.22 2.81 0.44 0.20 0.45 2.20 22.29 1.48 4.39 0.65 1.94 0.27 0.72 2 - -2 f cµ-1.7σ 0.18 0.01 0.11 0.22 2.94 0.43 0.21 0.48 2.23 16.81 1.49 3.87 0.64 1.65 0.26 0.62 1 -13.4 -2.33 " µ+1.7σ 0.17 0.02 0.18 0.22 3.04 0.45 0.21 0.46 3.04 26.71 1.77 4.95 0.79 2.22 0.32 0.82 2 13.2 19.84 f yµ-1.7σ 0.17 0.02 0.15 0.22 2.86 0.44 0.19 0.42 2.19 22.26 1.48 4.25 0.65 1.88 0.27 0.70 2 -2.8 0.05 " µ+1.7σ 0.17 0.02 0.15 0.22 2.80 0.44 0.21 0.48 2.21 22.44 1.48 4.57 0.65 2.01 0.27 0.75 2 3.4 0.06 G wµ-1.7σ 0.22 0.02 0.16 0.27 3.63 0.33 0.20 0.59 2.86 21.08 1.91 6.31 0.63 2.08 0.26 0.77 2 6.8 -3.17 " µ+1.7σ 0.14 0.01 0.14 0.18 2.56 0.61 0.22 0.37 2.15 22.93 1.35 3.09 0.82 1.88 0.33 0.70 1 -2.8 23.68 θ yµ-1.7σ 0.17 0.02 0.15 0.22 2.83 0.44 0.20 0.45 2.26 22.33 1.50 4.40 0.66 1.94 0.27 0.72 2 0.2 1.49 " µ+1.7σ 0.17 0.02 0.15 0.22 2.80 0.44 0.20 0.45 2.20 22.30 1.48 4.40 0.65 1.94 0.27 0.72 2 -0.1 0.010 θ uµ-1.7σ 0.17 0.02 0.08 0.22 2.81 0.44 0.20 0.44 2.20 12.05 1.48 3.09 0.65 1.36 0.27 0.52 2 -27.5 0.011 " µ+1.7σ 0.17 0.02 0.29 0.22 2.81 0.44 0.20 0.45 2.20 42.27 1.48 6.59 0.65 2.90 0.27 1.04 2 44.9 0.0Table 4.3.2.2. Results <strong>of</strong> pushover and IN2 analyses on the Uniformly Infilled frame in Y <strong>di</strong>rection


254 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills4.3.2.2 Pilotis frameX <strong>di</strong>rection2.52S ae(T eff) [g]1.510.500 0.02 0.04 0.06 0.08 0.1 0.12 0.14 0.16 0.18Top <strong>di</strong>splacement in X <strong>di</strong>rection [m]Figure 4.3.2.17. Pushover and IN2 curves for Model #1 (Pilotis frame – X <strong>di</strong>rection)Figure 4.3.2.18. Deformed shape and element damage for Model #1 at NC (Pilotis frame – X<strong>di</strong>rection)


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 255Sensitivity analysisthufcVariableGwfythyUpper valueLower value-60 -40 -20 0 20 40 60Change in PGA at collapse (%)Figure 4.3.2.19. Results <strong>of</strong> sensitivity analysis for NC LS (Pilotis frame – X <strong>di</strong>rection)Pushover and IN2 curves for Model #1 in X <strong>di</strong>rection are reported in Figure4.3.2.17. Results <strong>of</strong> sensitivity analysis for NC and DL Limit States are reporte<strong>di</strong>n Figures 4.3.2.19 and 4.3.2.22, respectively.The buil<strong>di</strong>ng collapses under a s<strong>of</strong>t-storey mechanism at the 1 st storey,where infills are not present, in all cases.Similar to previous cases, the sensitivity analysis shows that θ u has thehighest influence on the PGA at collapse through ∆ collapse , that is, throughµ collapse , <strong>di</strong>rectly influencing S ae,collapse (see Figure 4.3.2.20) and, hence,PGA collapse (see Figure 4.3.2.21).f c also influences the collapse capacity through the value <strong>of</strong> θ u , as alreadyillustrated.The beneficial effect <strong>of</strong> the increase in E w , G w and τ cr is due to fact that inhis case the <strong>di</strong>stribution <strong>of</strong> lateral forces is closer to a uniform <strong>di</strong>stribution (thisis reflected by the decrease in the modal participation factor Γ), lea<strong>di</strong>ng to ahigher initial stiffness <strong>of</strong> the pushover curve, resulting in lower values <strong>of</strong> T effand S dy , whereas the <strong>di</strong>splacement capacity ∆ collapse does not change


256 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infillssignificantly and, hence, µ collapse increases. Given practically equal the strengthC s,max , in R-µ-T relationships, as already illustrated, the latter (beneficial) effectprevails over the former (detrimental) effect lea<strong>di</strong>ng to higher values <strong>of</strong>S ae,collapse and PGA collapse .An increase in f y leads to a higher C s,max , but also to higher values <strong>of</strong> S dy andT eff . Given practically equal the <strong>di</strong>splacement capacity ∆ collapse , µ collapse decreasesand this effect prevails over the beneficial increase in C s,max , lea<strong>di</strong>ng to lowervalues <strong>of</strong> S ae,collapse and PGA collapse . Vice versa if f y decreases.The rotation at yiel<strong>di</strong>ng θ y has no significant influence on PGA capacity atcollapse.


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 25743.53S ae(T eff) [g]2.521.510.500 0.05 0.1 0.15 0.2 0.25 0.3 0.35Top <strong>di</strong>splacement in X <strong>di</strong>rection [m]Figure 4.3.2.20. Pushover and IN2 curves in terms <strong>of</strong> S ae (T eff ) for Models #10, #1 and #11:Lower, Me<strong>di</strong>an and Upper values for θ u (Pilotis frame – X <strong>di</strong>rection)1.41.21PGA [g]0.80.60.40.200 0.05 0.1 0.15 0.2 0.25 0.3 0.35Top <strong>di</strong>splacement in X <strong>di</strong>rection [m]Figure 4.3.2.21. IN2 curves in terms <strong>of</strong> PGA for Models #10, #1 and #11: Lower, Me<strong>di</strong>an andUpper values for θ u (Pilotis frame – X <strong>di</strong>rection)


258 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infillsSensitivity analysisfcfyVariableGwthythuUpper valueLower value-60 -40 -20 0 20 40 60Change in PGA at first <strong>RC</strong> yiel<strong>di</strong>ng (%)Figure 4.3.2.22. Results <strong>of</strong> sensitivity analysis for DL LS (Pilotis frame – X <strong>di</strong>rection)When f c decreases, both S dy and ∆ f<strong>RC</strong>y increase, but the former effectprevails on the latter, lea<strong>di</strong>ng to a lower value <strong>of</strong> µ f<strong>RC</strong>y and, hence, <strong>of</strong> R f<strong>RC</strong>y .Moreover, the detrimental effect <strong>of</strong> a decrease in f c on S ae,f<strong>RC</strong>y is also given bythe decrease in C s,max . Vice versa when f c increases.Opposite to the case <strong>of</strong> f c , when f y decreases both S dy and ∆ f<strong>RC</strong>y decrease, butthe former effect prevails on the latter, lea<strong>di</strong>ng to a higher value <strong>of</strong> µ f<strong>RC</strong>y and,hence, <strong>of</strong> R f<strong>RC</strong>y . Nevertheless, the detrimental effect <strong>of</strong> the decrease in C s,maxprevails. Vice versa when f y increases.Contrary to expectations, an increase in θ y does not have a great beneficialinfluence on S ae,f<strong>RC</strong>y and, hence, on PGA f<strong>RC</strong>y . This is due to the fact that whenθ y increases, the <strong>di</strong>splacement capacity ∆ f<strong>RC</strong>y increases, but S dy increases too,lea<strong>di</strong>ng to a not much <strong>di</strong>fferent value <strong>of</strong> µ f<strong>RC</strong>y and, hence, <strong>of</strong> R f<strong>RC</strong>y .An increase in E w , G w and τ cr , as already illustrated, leads to a higher initialstiffness <strong>of</strong> the pushover curve, resulting in lower values <strong>of</strong> S dy but also <strong>of</strong>∆ f<strong>RC</strong>y . These two effects counterbalance each other, globally lea<strong>di</strong>ng to nosignificant change in µ f<strong>RC</strong>y and, hence, in R f<strong>RC</strong>y . When E w , G w and τ cr decrease,


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 259both S dy and ∆ f<strong>RC</strong>y increase, but the former effect prevails on the latter, lea<strong>di</strong>ngto a lower value <strong>of</strong> µ f<strong>RC</strong>y and, hence, <strong>of</strong> R f<strong>RC</strong>y .Y <strong>di</strong>rection1.41.21S ae(T eff) [g]0.80.60.40.200 0.02 0.04 0.06 0.08 0.1 0.12 0.14 0.16Top <strong>di</strong>splacement in Y <strong>di</strong>rection [m]Figure 4.3.2.23. Pushover and IN2 curves for Model #1 (Pilotis frame – Y <strong>di</strong>rection)Figure 4.3.2.24. Deformed shape and element damage for Model #1 at NC (Pilotis frame – Y<strong>di</strong>rection)


260 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infillsSensitivity analysisthufcVariablefyGwthyUpper valueLower value-60 -40 -20 0 20 40 60Change in PGA at collapse (%)Figure 4.3.2.25. Results <strong>of</strong> sensitivity analysis for NC LS (Pilotis frame – Y <strong>di</strong>rection)Pushover and IN2 curves for Model #1 in Y <strong>di</strong>rection are reported in Figure4.3.2.23. Results <strong>of</strong> sensitivity analysis for NC and DL Limit States are reporte<strong>di</strong>n Figures 4.3.2.25 and 4.3.2.26, respectively.Also in this <strong>di</strong>rection, the buil<strong>di</strong>ng always collapses under a s<strong>of</strong>t-storeymechanism at the 1 st storey, where infills are not present.The same considerations made for X <strong>di</strong>rection can be reported for allparameters, except infill mechanical characteristics since in this <strong>di</strong>rection theirinfluence – which was already not particularly significant in X <strong>di</strong>rection – isabsolutely negligible, due to the lower number <strong>of</strong> infill panels in Y <strong>di</strong>rection.


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 261Sensitivity analysisfyfcVariablethyGwthuUpper valueLower value-60 -40 -20 0 20 40 60Change in PGA at first <strong>RC</strong> yiel<strong>di</strong>ng (%)Figure 4.3.2.26. Results <strong>of</strong> sensitivity analysis for DL LS (Pilotis frame – Y <strong>di</strong>rection)From a qualitative standpoint, analyzed parameters influence the PGAcapacity at first <strong>RC</strong> yiel<strong>di</strong>ng by the same way in Y <strong>di</strong>rection, compared with X<strong>di</strong>rection. Again, the only exception is for infill mechanical characteristics,whose influence on the seismic behaviour in Y <strong>di</strong>rection is absolutelynegligible.


262 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infillsComparison between X and Y <strong>di</strong>rectionsIf a comparison is carried out between the seismic capacity in X and Y<strong>di</strong>rections for Model #1 (see Figures 4.3.2.27 and 4.3.2.28) it is observed howthe <strong>di</strong>splacement capacity at collapse does not change significantly and thebeneficial effect <strong>of</strong> the higher strength in X <strong>di</strong>rection compared with Y<strong>di</strong>rection, due to the orientation <strong>of</strong> column elements – which, following theparallel plane frame configuration, provide a higher strength in X <strong>di</strong>rection –leads to a higher S ae,collapse and also to a higher PGA collapse in X <strong>di</strong>rection. The<strong>di</strong>fference between the values <strong>of</strong> S ae,collapse in X and Y <strong>di</strong>rections is higher thanthe <strong>di</strong>fference between the values <strong>of</strong> PGA collapse , due to the <strong>di</strong>fference in T effbetween the two <strong>di</strong>rections.As far as first <strong>RC</strong> yiel<strong>di</strong>ng is concerned, column orientation leads to a lower<strong>di</strong>splacement capacity in X <strong>di</strong>rection compared with Y <strong>di</strong>rection; nevertheless,beneficial effect <strong>of</strong> the higher strength in X <strong>di</strong>rection leads to a higher seismiccapacity in terms <strong>of</strong> S ae also at this Limit State. Again, due to the <strong>di</strong>fference inT eff between the two <strong>di</strong>rections, the <strong>di</strong>fference between the values <strong>of</strong> S ae,f<strong>RC</strong>y inX and Y <strong>di</strong>rections is higher than the <strong>di</strong>fference between the values <strong>of</strong> PGA f<strong>RC</strong>y .2.52S ae(T eff) [g]1.510.500 0.02 0.04 0.06 0.08 0.1 0.12 0.14 0.16 0.18Top <strong>di</strong>splacement [m]Figure 4.3.2.27. Pushover and IN2 curves in terms <strong>of</strong> S ae (T eff ) for Model #1 in X and Y<strong>di</strong>rections (Pilotis frame)


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 2630.90.80.70.6PGA [g]0.50.40.30.20.100 0.02 0.04 0.06 0.08 0.1 0.12 0.14 0.16 0.18Top <strong>di</strong>splacement [m]Figure 4.3.2.28. IN2 curves in terms <strong>of</strong> PGA for Model #1 in X and Y <strong>di</strong>rections (Pilotis frame)


264 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infillsModelNo.Mo<strong>di</strong>fiedVariableStoreyValue T el ∆ f<strong>RC</strong>y ∆ coll T eff C s,max µ f<strong>RC</strong>y µ coll R f<strong>RC</strong>y R coll S ae,f<strong>RC</strong>y S ae,coll PGA f<strong>RC</strong>y PGA coll involved incollapse∆ PGA,NC ∆ PGA,f<strong>RC</strong>y1 - - 0.39 0.02 0.14 0.49 0.24 1.12 9.15 1.12 9.11 0.27 2.22 0.16 0.82 1 - -2 f c µ-1.7σ 0.46 0.02 0.11 0.57 0.22 1.01 5.83 1.01 5.83 0.22 1.30 0.15 0.61 1 -25.7 -4.33 " µ+1.7σ 0.35 0.02 0.17 0.43 0.26 1.33 13.92 1.33 11.52 0.34 2.96 0.17 1.06 1 30.0 7.04 f yµ-1.7σ 0.38 0.02 0.14 0.48 0.23 1.15 10.14 1.15 9.83 0.27 2.28 0.15 0.84 1 2.1 -4.55 " µ+1.7σ 0.40 0.02 0.14 0.52 0.26 1.05 7.89 1.05 7.89 0.27 2.04 0.16 0.79 1 -3.4 3.26 G wµ-1.7σ 0.39 0.02 0.14 0.52 0.24 1.02 8.18 1.02 8.18 0.25 2.00 0.15 0.78 1 -4.6 -3.97 " µ+1.7σ 0.38 0.02 0.14 0.48 0.24 1.16 9.58 1.16 9.35 0.28 2.28 0.16 0.84 1 2.3 1.48 θ y µ-1.7σ 0.38 0.02 0.14 0.50 0.24 1.06 8.86 1.06 8.86 0.26 2.16 0.15 0.81 1 -1.3 -3.49 " µ+1.7σ 0.39 0.02 0.14 0.50 0.24 1.12 8.79 1.12 8.79 0.27 2.15 0.16 0.81 1 -1.5 1.410 θ uµ-1.7σ 0.39 0.02 0.07 0.49 0.24 1.12 4.71 1.12 4.71 0.27 1.15 0.16 0.49 1 -39.6 0.011 " µ+1.7σ 0.39 0.02 0.27 0.49 0.24 1.12 17.80 1.12 15.92 0.27 3.88 0.16 1.36 1 66.6 0.0Table 4.3.2.3. Results <strong>of</strong> pushover and IN2 analyses on the Pilotis frame in X <strong>di</strong>rectionModelNo.Mo<strong>di</strong>fiedVariableStoreyValue T el ∆ f<strong>RC</strong>y ∆ coll T eff C s,max µ f<strong>RC</strong>y µ coll R f<strong>RC</strong>y R coll S ae,f<strong>RC</strong>y S ae,coll PGA f<strong>RC</strong>y PGA coll involved incollapse∆ PGA,NC ∆ PGA,f<strong>RC</strong>y1 - - 0.54 0.02 0.14 0.68 0.19 0.98 6.18 0.99 6.18 0.18 1.15 0.15 0.63 1 - -2 f c µ-1.7σ 0.61 0.02 0.11 0.77 0.17 0.89 3.94 0.91 3.94 0.16 0.68 0.15 0.47 1 -25.8 -2.33 " µ+1.7σ 0.49 0.02 0.17 0.61 0.20 1.10 8.90 1.10 8.90 0.21 1.74 0.16 0.80 1 26.1 4.44 f yµ-1.7σ 0.53 0.02 0.14 0.65 0.18 1.04 7.17 1.04 7.17 0.18 1.26 0.14 0.66 1 3.5 -4.35 " µ+1.7σ 0.55 0.02 0.14 0.71 0.20 0.94 5.38 0.95 5.38 0.19 1.07 0.16 0.62 1 -2.8 5.96 G wµ-1.7σ 0.55 0.02 0.14 0.69 0.19 0.96 6.03 0.97 6.03 0.18 1.13 0.15 0.63 1 -0.6 -0.37 " µ+1.7σ 0.54 0.02 0.14 0.69 0.19 0.95 6.05 0.96 6.05 0.18 1.13 0.15 0.63 1 -0.4 -1.18 θ y µ-1.7σ 0.54 0.02 0.14 0.68 0.19 0.97 6.24 0.98 6.24 0.18 1.16 0.15 0.64 1 0.4 -1.39 " µ+1.7σ 0.55 0.02 0.14 0.68 0.19 1.01 6.14 1.01 6.14 0.19 1.15 0.15 0.63 1 -0.2 2.410 θ uµ-1.7σ 0.54 0.02 0.07 0.68 0.19 0.98 3.19 0.99 3.19 0.18 0.60 0.15 0.38 1 -39.4 0.011 " µ+1.7σ 0.54 0.02 0.27 0.68 0.19 0.98 11.99 0.99 11.99 0.18 2.24 0.15 1.05 1 65.5 0.0Table 4.3.2.4. Results <strong>of</strong> pushover and IN2 analyses on the Pilotis frame in Y <strong>di</strong>rection


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 2654.3.2.3 Bare frameX <strong>di</strong>rection0.70.60.5S ae(T eff) [g]0.40.30.20.100 0.05 0.1 0.15 0.2 0.25Top <strong>di</strong>splacement in X <strong>di</strong>rection [m]Figure 4.3.2.29. Pushover and IN2 curves for Model #1 (Bare frame – X <strong>di</strong>rection)Figure 4.3.2.30. Deformed shape and element damage for Model #1 at NC (Bare frame – X<strong>di</strong>rection)


266 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infillsSensitivity analysisthuVariablefcfythyUpper valueLower value-60 -40 -20 0 20 40 60Change in PGA at collapse (%)Figure 4.3.2.31. Results <strong>of</strong> sensitivity analysis for NC LS (Bare frame – X <strong>di</strong>rection)Pushover and IN2 curves for Model #1 in X <strong>di</strong>rection are reported in Figure4.3.2.29. Results <strong>of</strong> sensitivity analysis for NC and DL Limit States are reporte<strong>di</strong>n Figures 4.3.2.31 and 4.3.2.32, respectively.The buil<strong>di</strong>ng collapses under a s<strong>of</strong>t-storey mechanism at the 3 rd storey in allcases. The formation <strong>of</strong> a s<strong>of</strong>t-storey mechanism also without the presence <strong>of</strong>infill panels is likely to occur in such a buil<strong>di</strong>ng, which has not been designedfor seismic loads and, obviously, does not comply with Capacity Designprinciples such as weak beam/strong column con<strong>di</strong>tion. In the Uniformlyinfilled frame the s<strong>of</strong>t-storey mechanism occurs at one storey at the bottom (1 stor 2 nd storey), thus confirming the well-known phenomenon <strong>of</strong> concentration <strong>of</strong><strong>di</strong>splacement demand in bottom storeys in this kind <strong>of</strong> structures, due to themore uniform <strong>di</strong>stribution <strong>of</strong> strength along the height, whereas in the Bareframe this mechanism occurs at the 3 rd storey, where a decrease in column<strong>di</strong>mension (and strength) is observed, due to the Gravity Load Designprocedure.


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 267Again, the sensitivity analysis shows that θ u has the highest influence on thePGA at collapse through ∆ collapse , that is, through µ collapse , <strong>di</strong>rectly influencingS ae,collapse and, hence, PGA collapse .Similarly, f c also influences the collapse capacity through the value <strong>of</strong> θ u , asalready illustrated.When f y increases, the <strong>di</strong>splacement capacity ∆ collapse does not changesignificantly, but S dy increases, thus lea<strong>di</strong>ng to a reduction in µ collapse .Nevertheless, this effect is counterbalanced by the increase in C s,max , resultingin no significant change in S ae,collapse and PGA collapse . Vice versa if f y decreases.The rotation at yiel<strong>di</strong>ng θ y has no significant influence on PGA capacity atcollapse.Sensitivity analysisfyVariablefcthythuUpper valueLower value-60 -40 -20 0 20 40 60Change in PGA at first <strong>RC</strong> yiel<strong>di</strong>ng (%)Figure 4.3.2.32. Results <strong>of</strong> sensitivity analysis for DL LS (Bare frame – X <strong>di</strong>rection)When f y decreases both S dy and ∆ f<strong>RC</strong>y decrease, but (contrary to the Pilotisframe) the latter effect prevails on the former, lea<strong>di</strong>ng to a lower value <strong>of</strong> µ f<strong>RC</strong>yand, hence, <strong>of</strong> R f<strong>RC</strong>y . Moreover, the decrease in C s,max leads to a further decreasein S ae,f<strong>RC</strong>y and PGA f<strong>RC</strong>y . Vice versa when f y increases.


268 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infillsFor the same reasons illustrated for the Pilotis frame, when f c decreases alower value <strong>of</strong> S ae,f<strong>RC</strong>y is observed. Nevertheless, the increase in T effcounterbalances this effect, lea<strong>di</strong>ng to a slightly higher capacity in terms <strong>of</strong>PGA. Vice versa when f c increases.Again, an increase in θ y does not have a great beneficial influence on S ae,f<strong>RC</strong>yand, hence, on PGA f<strong>RC</strong>y , for the same reasons above illustrated for the Pilotisframe: when θ y increases, the <strong>di</strong>splacement capacity ∆ f<strong>RC</strong>y increases, but S dyincreases too, lea<strong>di</strong>ng to a not much <strong>di</strong>fferent value <strong>of</strong> µ f<strong>RC</strong>y and, hence, <strong>of</strong>R f<strong>RC</strong>y .As expected, θ u has no significant influence on PGA capacity at this LimitState.Y <strong>di</strong>rection0.40.350.3S ae(T eff) [g]0.250.20.150.10.0500 0.1 0.2 0.3 0.4 0.5 0.6 0.7Top <strong>di</strong>splacement in Y <strong>di</strong>rection [m]Figure 4.3.2.33. Pushover and IN2 curves for Model #1 (Bare frame – Y <strong>di</strong>rection)


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 269Figure 4.3.2.34. Deformed shape and element damage for Model #1 at NC (Bare frame – Y<strong>di</strong>rection)Sensitivity analysisthuVariablefcfythyUpper valueLower value-60 -40 -20 0 20 40 60Change in PGA at collapse (%)Figure 4.3.2.35. Results <strong>of</strong> sensitivity analysis for NC LS (Bare frame – Y <strong>di</strong>rection)Pushover and IN2 curves for Model #1 in Y <strong>di</strong>rection are reported in Figure4.3.2.33. Results <strong>of</strong> sensitivity analysis for NC and DL Limit States are reported


270 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infillsin Figures 4.3.2.35 and 4.3.2.36, respectively.In this <strong>di</strong>rection, the buil<strong>di</strong>ng always collapses under a global mechanism atinvolving all the four storeys. This collapse mechanism is certainly stronglyinfluenced by the structural configuration, where beams in transversal <strong>di</strong>rectionare present only in external frames. A strong <strong>di</strong>fference with the Uniformlyinfilled and the Pilotis frame, where the presence <strong>of</strong> infill panels forces thecollapse mechanism to develop only in one storey (at the bottom), is noted.As far as the influence <strong>of</strong> single variables is concerned, the main influence<strong>of</strong> <strong>di</strong>splacement capacity through θ u and, in<strong>di</strong>rectly, through f c is observedagain.The decrease in f y leads to a lower value <strong>of</strong> S dy , whereas the <strong>di</strong>splacementcapacity ∆ collapse does not change significantly, thus lea<strong>di</strong>ng to a higher µ collapseand, hence, to a higher R collapse . However, this effect is counterbalanced by alower C s,max , thus lea<strong>di</strong>ng to a only slightly higher PGA collapse .Sensitivity analysisfyVariablefcthythuUpper valueLower value-60 -40 -20 0 20 40 60Change in PGA at first <strong>RC</strong> yiel<strong>di</strong>ng (%)Figure 4.3.2.36. Results <strong>of</strong> sensitivity analysis for DL LS (Bare frame – Y <strong>di</strong>rection)Similar to PGA capacity at collapse, it is observed that the decrease in f yleads to a lower value <strong>of</strong> S dy , whereas the <strong>di</strong>splacement capacity ∆ f<strong>RC</strong>y also


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 271decreases but in a lower measure, thus lea<strong>di</strong>ng to a higher µ f<strong>RC</strong>y and, hence, to ahigher R f<strong>RC</strong>y . However, this effect is counterbalanced by a lower C s,max , thuslea<strong>di</strong>ng to a only slightly higher PGA f<strong>RC</strong>y .As far as θ y is concerned, it is observed again that when θ y increases, the<strong>di</strong>splacement capacity ∆ f<strong>RC</strong>y increases, but S dy increases too, thuscounterbalancing the former effect. Vice versa when θ y decreases.For the same reasons, also f c has a negligible influence on PGA capacity atfirst <strong>RC</strong> yiel<strong>di</strong>ng.Comparison between X and Y <strong>di</strong>rectionsIf a comparison is carried out between the seismic capacity in X and Y<strong>di</strong>rections for Model #1 (see Figures 4.3.2.37 and 4.3.2.38) a clear <strong>di</strong>fference isobserved in the lateral response <strong>of</strong> the buil<strong>di</strong>ng: the column-sway storeymechanism in X <strong>di</strong>rection leads to a higher strength but also to a lowerductility, whereas the opposite happens in Y <strong>di</strong>rection, where a globalmechanism occurs. Globally, S ae,collapse in Y <strong>di</strong>rection is lower than in X<strong>di</strong>rection, since – due to the higher deformability (higher value <strong>of</strong> S dy ) – in Y<strong>di</strong>rection the ductility capacity µ collapse is not as higher (compared with the X<strong>di</strong>rection) as the <strong>di</strong>splacement capacity ∆ collapse . Hence, the lower strength is noteffectively counterbalanced by the higher ductility capacity.Nevertheless, due to the <strong>di</strong>fference in T eff between the two <strong>di</strong>rections, interms <strong>of</strong> PGA a higher capacity is observed in Y <strong>di</strong>rection.As far as first <strong>RC</strong> yiel<strong>di</strong>ng is concerned, a similar <strong>di</strong>splacement capacity isobserved, but the higher value <strong>of</strong> S dy and, above all, the lower strength, lead to alower S ae,f<strong>RC</strong>y in Y <strong>di</strong>rection. Due to the <strong>di</strong>fference in T eff , this <strong>di</strong>fferencedecreases in terms <strong>of</strong> PGA, but, however, a higher PGA f<strong>RC</strong>y is observed in X<strong>di</strong>rection.


272 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills0.70.60.5S ae(T eff) [g]0.40.30.20.100 0.1 0.2 0.3 0.4 0.5 0.6 0.7Top <strong>di</strong>splacement [m]Figure 4.3.2.37. Pushover and IN2 curves in terms <strong>of</strong> S ae (T eff ) for Model #1 in X and Y<strong>di</strong>rections (Bare frame)0.70.60.5PGA [g]0.40.30.20.100 0.1 0.2 0.3 0.4 0.5 0.6 0.7Top <strong>di</strong>splacement [m]Figure 4.3.2.38. IN2 curves in terms <strong>of</strong> PGA for Model #1 in X and Y <strong>di</strong>rections (Bare frame)


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 273ModelNo.Mo<strong>di</strong>fiedVariableStoreyValue T el ∆ f<strong>RC</strong>y ∆ coll T eff C s,max µ f<strong>RC</strong>y µ coll R f<strong>RC</strong>y R coll S ae,f<strong>RC</strong>y S ae,coll PGA f<strong>RC</strong>y PGA coll involved incollapse∆ PGA,NC ∆ PGA,f<strong>RC</strong>y1 - - 0.76 0.06 0.22 1.01 0.20 0.95 3.33 0.95 3.33 0.19 0.68 0.22 0.57 3 - -2 f c µ-1.7σ 0.99 0.08 0.20 1.18 0.19 0.89 2.38 0.90 2.38 0.17 0.46 0.23 0.48 3 -16.3 3.63 " µ+1.7σ 0.67 0.05 0.24 0.85 0.21 1.03 4.80 1.03 4.80 0.22 1.02 0.21 0.68 3 19.8 -4.14 f yµ-1.7σ 0.74 0.05 0.22 1.00 0.19 0.81 3.54 0.82 3.54 0.16 0.68 0.18 0.57 3 -0.4 -16.55 " µ+1.7σ 0.78 0.08 0.22 1.04 0.22 1.04 3.00 1.04 3.00 0.23 0.65 0.25 0.57 3 -0.8 16.16 θ y µ-1.7σ 0.75 0.06 0.22 1.00 0.20 0.94 3.37 0.95 3.37 0.19 0.69 0.22 0.57 3 0.2 -1.57 " µ+1.7σ 0.77 0.07 0.22 1.02 0.20 0.95 3.24 0.96 3.24 0.20 0.66 0.22 0.57 3 -0.6 1.88 θ uµ-1.7σ 0.76 0.06 0.15 1.01 0.20 0.95 2.22 0.95 2.22 0.19 0.45 0.22 0.42 3 -26.5 0.09 " µ+1.7σ 0.76 0.06 0.36 1.01 0.20 0.95 5.50 0.95 5.50 0.19 1.12 0.22 0.84 3 46.3 0.0Table 4.3.2.5. Results <strong>of</strong> pushover and IN2 analyses on the Bare frame in X <strong>di</strong>rectionModelNo.Mo<strong>di</strong>fiedVariableStoreyValue T el ∆ f<strong>RC</strong>y ∆ coll T eff C s,max µ f<strong>RC</strong>y µ coll R f<strong>RC</strong>y R coll S ae,f<strong>RC</strong>y S ae,coll PGA f<strong>RC</strong>y PGA coll involved incollapse∆ PGA,NC ∆ PGA,f<strong>RC</strong>y1 - - 1.35 0.08 0.56 2.10 0.09 0.61 4.34 0.71 4.34 0.06 0.40 0.16 0.66 1+2+3+4 - -2 f c µ-1.7σ 1.57 0.09 0.45 2.36 0.09 0.57 2.84 0.64 2.84 0.06 0.25 0.16 0.51 1+2+3+4 -23.3 2.53 " µ+1.7σ 1.19 0.07 0.67 1.85 0.09 0.70 6.45 0.79 6.45 0.07 0.60 0.16 0.83 1+2+3+4 25.5 1.54 f yµ-1.7σ 1.32 0.07 0.57 2.02 0.08 0.64 5.13 0.74 5.13 0.06 0.43 0.15 0.69 1+2+3+4 3.9 -6.55 " µ+1.7σ 1.38 0.09 0.55 2.14 0.10 0.61 3.75 0.69 3.75 0.07 0.37 0.17 0.64 1+2+3+4 -3.0 7.46 θ y µ-1.7σ 1.34 0.08 0.56 2.07 0.09 0.62 4.44 0.71 4.44 0.06 0.40 0.16 0.67 1+2+3+4 0.9 -0.87 " µ+1.7σ 1.36 0.08 0.56 2.12 0.09 0.62 4.22 0.71 4.22 0.06 0.38 0.16 0.65 1+2+3+4 -1.2 1.58 θ uµ-1.7σ 1.35 0.08 0.26 2.10 0.09 0.61 2.01 0.71 2.01 0.06 0.18 0.16 0.37 1+2+3+4 -44.3 0.09 " µ+1.7σ 1.35 0.08 1.14 2.10 0.09 0.61 8.80 0.71 8.80 0.06 0.80 0.16 1.13 1+2+3+4 71.1 0.0Table 4.3.2.6. Results <strong>of</strong> pushover and IN2 analyses on the Bare frame in Y <strong>di</strong>rection


274 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills4.3.3. Comparison between <strong>di</strong>fferent infill configurationsIn this Section, the influence <strong>of</strong> <strong>di</strong>fferent infill configurations on the seismiccapacity <strong>of</strong> the case study buil<strong>di</strong>ng is evaluated. To this aim, the IN2 curves arecompared (always referring to Model #1, where a me<strong>di</strong>an value is consideredfor all the variables). The comparison is carried out in both <strong>di</strong>rections. Hence,<strong>vulnerability</strong> curves are evaluated, through the application <strong>of</strong> a ResponseSurface Method.4.3.3.1 Comparison between <strong>di</strong>fferent infill configurations: IN2 curvesX <strong>di</strong>rectionA first comparison can be carried out between the IN2 curves in terms <strong>of</strong>S ae (T eff ) for Uniformly infilled, Pilotis and Bare frame.Actually, the MDOF <strong>di</strong>splacement capacity at Collapse is almost coincidentbetween the Uniformly infilled and the Pilotis frame since the collapsemechanism involve in both cases <strong>RC</strong> columns at the 1 st storey; nevertheless, alower <strong>di</strong>splacement capacity <strong>of</strong> the equivalent SDOF is observed in Figure4.3.3.1, due to the lower modal participation factor Γ for the Pilotis frame. The<strong>di</strong>splacement capacity <strong>of</strong> the Bare frame is the highest one since in this framethe collapse mechanism involves the columns at the 3 rd storey, which arecharacterized by a lower axial load and, hence, by a higher ductility. The highbase shear capacity <strong>of</strong> the Uniformly infilled frame leads to much higher values<strong>of</strong> S ae for relatively low <strong>di</strong>splacement values (e.g., DL Limit State). As theductility increases, the detrimental effect given by the increase in the slope <strong>of</strong>the IN2 curve, due to the drop <strong>of</strong> strength represented through the parameter r u ,prevails over the higher base shear and, at NC Limit State, the S ae capacity <strong>of</strong>the Uniformly infilled frame is lower compared with the correspon<strong>di</strong>ng capacity<strong>of</strong> the Pilotis frame. The higher <strong>di</strong>splacement capacity <strong>of</strong> the Bare frame iscounterbalanced by its lower strength but, above all, by the lower stiffness <strong>of</strong>the pushover curve, resulting in lower S ae capacity at both Limit States,compared with other frames.


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 2752.52S ae (T eff ) [g]1.510.500 0.05 0.1 0.15 0.2 0.25Top <strong>di</strong>splacement in X <strong>di</strong>rection [m]Figure 4.3.3.1. Pushover and IN2 curves in terms <strong>of</strong> S ae (T eff ) for Model #1 in X <strong>di</strong>rection(Uniformly infilled, Pilotis and Bare frame)Nevertheless, in order to compare the seismic capacity <strong>of</strong> <strong>di</strong>fferent frames, itis more correct to plot the IN2 curves in terms <strong>of</strong> PGA since this can beconsidered as a common measure <strong>of</strong> seismic intensity, whereas it is notappropriate to compare the seismic capacity in terms <strong>of</strong> spectral acceleration ifthe periods <strong>of</strong> the various frames are significantly <strong>di</strong>fferent.It can be observed that the relative ratios between the seismic capacities <strong>of</strong>the Uniformly infilled and the Pilotis frame do not change significantly if PGAis considered instead <strong>of</strong> S ae (T eff ) (see Figure 4.3.3.2), because in both cases theperiod T eff is lower than T C , hence the spectral acceleration is on the constantbranch <strong>of</strong> the spectrum. Therefore, when PGA is considered instead <strong>of</strong> S ae (T eff ),the only (slight) change in the relative ratios between the seismic capacities <strong>of</strong>the frames is due to the little change in F 0 with the <strong>di</strong>fferent PGA. A severechange, instead, is observed if the seismic capacity <strong>of</strong> the Bare frame isconsidered in terms <strong>of</strong> PGA. In this case, due to the relatively high period T eff ,the evaluation <strong>of</strong> the seismic capacity significantly changes: the PGA capacityat NC Limit States remains the lowest, compared with Uniformly infilled and


276 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infillsBare frames, but anyhow the relative <strong>di</strong>stance between the seismic capacity <strong>of</strong>the Bare frame and <strong>of</strong> remaining frames significantly decreases. Moreover, atDL Limit State the PGA capacity <strong>of</strong> the Bare frame is higher, compared withthe capacity <strong>of</strong> the Pilotis frame.0.90.80.70.6PGA [g]0.50.40.30.20.100 0.05 0.1 0.15 0.2 0.25Top <strong>di</strong>splacement in X <strong>di</strong>rection [m]Figure 4.3.3.2. IN2 curves in terms <strong>of</strong> PGA for Model #1 in X <strong>di</strong>rection (Uniformly infilled,Pilotis and Bare frame)In conclusion, the better seismic performance at DL Limit State is shown bythe Uniformly infilled frame, due to the high contribution <strong>of</strong> infill elements interms <strong>of</strong> stiffness and strength, whereas at NC Limit State the betterperformance is shown by the Pilotis frame since for higher values <strong>of</strong> ductilitythe detrimental effect due to the brittle behaviour <strong>of</strong> infills counterbalancestheir strength contribution. At NC Limit State the Bare frame shows the worstbehaviour. Nevertheless, it is to be noted that in this frame the collapsemechanism, even without infills, is an unfavourable s<strong>of</strong>t-storey mechanism, asmay happen in <strong>existing</strong> <strong>buil<strong>di</strong>ngs</strong> not designed accor<strong>di</strong>ng to modern principlessuch as weak beam/strong column con<strong>di</strong>tion.


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 277Y <strong>di</strong>rectionIn Y <strong>di</strong>rection, <strong>di</strong>fferent considerations can be made if the seismic capacity<strong>of</strong> Uniformly infilled and Pilotis frames are compared, see Figure 4.3.3.3. In theformer case, the s<strong>of</strong>t-storey collapse mechanism takes place at the 2 nd storey,where <strong>RC</strong> columns are characterized by a slightly higher deformation capacitycompared with the 1 st storey, where the s<strong>of</strong>t-storey collapse mechanism takesplace in the Pilotis frame. Hence, the detrimental effect (in terms <strong>of</strong> SDOF<strong>di</strong>splacement capacity) <strong>of</strong> higher modal participation factor for the Uniformlyinfilled frame is partially counterbalanced. Moreover, in this <strong>di</strong>rection thehigher strength provided by the Uniformly infilled frame counterbalances thedetrimental effect given by the increase in the slope <strong>of</strong> the IN2 curve, due to thedrop <strong>of</strong> strength, thus lea<strong>di</strong>ng to a higher capacity, in terms <strong>of</strong> S ae (T eff ), at bothLimit States. If the Bare frame is considered, it is noted how the global collapsemechanism provides a significantly higher ductility, compared with otherframes, but also a significantly lower strength, globally resulting in a lowercapacity, in terms <strong>of</strong> S ae (T eff ), at both Limit States.21.81.61.4S ae (T eff ) [g]1.210.80.60.40.200 0.05 0.1 0.15 0.2 0.25 0.3 0.35 0.4 0.45 0.5Top <strong>di</strong>splacement in Y <strong>di</strong>rection [m]Figure 4.3.3.3. Pushover and IN2 curves in terms <strong>of</strong> S ae (T eff ) for Model #1 in Y <strong>di</strong>rection(Uniformly infilled, Pilotis and Bare frame)


278 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infillsIf the seismic capacity is assessed in terms <strong>of</strong> PGA, see Figure 4.3.3.4,<strong>di</strong>fferent effects are observed: first, the relative <strong>di</strong>stance between seismiccapacity <strong>of</strong> Uniformly infilled and Pilotis frames decreases, especially at NCLimit State, mainly because in this case T eff is lower than T C for the Uniformlyinfilled frame and higher than T C for the Pilotis. Therefore, when PGA isconsidered instead <strong>of</strong> S ae , seismic capacities <strong>of</strong> these frames become muchcloser to each other.For the same reason, the assessment <strong>of</strong> the seismic capacities <strong>of</strong> the Bareframe, which is characterized by a much higher value <strong>of</strong> T eff , significantlychanges if PGA is considered instead <strong>of</strong> S ae (T eff ), showing a seismic capacityhigher than the Pilotis frame at both Limit States.0.80.70.60.5PGA [g]0.40.30.20.100 0.05 0.1 0.15 0.2 0.25 0.3 0.35 0.4 0.45 0.5Top <strong>di</strong>splacement in Y <strong>di</strong>rection [m]Figure 4.3.3.4. IN2 curves in terms <strong>of</strong> PGA for Model #1 in Y <strong>di</strong>rection (Uniformly infilled,Pilotis and Bare frame)It is observed how, in Y <strong>di</strong>rection, opposite to X <strong>di</strong>rection, the seismicperformance <strong>of</strong> the Bare frame at NC Limit State is better compared with thePilotis frame and very closer to the Uniformly infilled frame. This is abeneficial consequence <strong>of</strong> the higher ductility provided by the global collapsemechanism observed in the Bare frame in this <strong>di</strong>rection. At DL Limit State, the


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 279beneficial influence <strong>of</strong> the higher stiffness and strength provided by infills leadsto a higher PGA for this kind <strong>of</strong> frame.Summary <strong>of</strong> remarksNumerical results confirm how the presence <strong>of</strong> infills provides a beneficialincrease in stiffness and strength which may or may not be counterbalanced bythe detrimental effect due to the sudden loss <strong>of</strong> strength, which leads to anincrease in <strong>di</strong>splacement demand when a certain threshold <strong>of</strong> seismic intensityis exceeded. The latter effect is expressed in the adopted R-µ-T relationships(Dolšek and Fajfar, 2004a) by the coefficient r u , and is reflected in thedecreasing slope <strong>of</strong> IN2 curves with r u decreasing.Compared with the Bare frame, in the Uniformly infilled frame thebeneficial influence <strong>of</strong> the increase in stiffness and strength prevails over thedetrimental influence <strong>of</strong> the brittle behaviour, both in X and Y <strong>di</strong>rection.The detrimental effect <strong>of</strong> an irregular <strong>di</strong>stribution <strong>of</strong> infills – lea<strong>di</strong>ng, asexpected, to a localization <strong>of</strong> inelastic <strong>di</strong>splacement demand at the bottom barestorey – is evident in Y <strong>di</strong>rection, where the <strong>di</strong>splacement capacity <strong>of</strong> the Bareframe is significantly higher, due to the formation <strong>of</strong> a favourable globalcollapse mechanism. On the contrary, in X <strong>di</strong>rection, where the formation <strong>of</strong> anunfavourable column-sway storey mechanism is observed also in the Bareframe, the detrimental effect <strong>of</strong> an irregular <strong>di</strong>stribution <strong>of</strong> infills is notobserved. These observations confirm how the evaluation <strong>of</strong> the infill influenceon seismic behaviour cannot be independent <strong>of</strong> the evaluation <strong>of</strong> the seismicbehaviour shown by the bare structure.4.3.3.2 Comparison between <strong>di</strong>fferent infill configurations: fragility curvesEvaluation <strong>of</strong> fragility curves: methodologyIn this paragraph, the methodology used for the evaluation <strong>of</strong> fragilitycurves for the case study structure is illustrated.A fragility curve represents a relationship between a seismic intensity


280 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infillsparameter and the correspon<strong>di</strong>ng probability <strong>of</strong> exceedance <strong>of</strong> a given damagethreshold (typically represented by a <strong>di</strong>splacement capacity).The PGA capacity – for a certain Limit State – is defined as the PGAcorrespon<strong>di</strong>ng to the demand spectrum under which the <strong>di</strong>splacement deman<strong>di</strong>s equal to the <strong>di</strong>splacement capacity for that Limit State. PGA capacity for acertain Limit State is represented by the or<strong>di</strong>nate <strong>of</strong> the IN2 curve (expressed interms <strong>of</strong> PGA) correspon<strong>di</strong>ng to the <strong>di</strong>splacement capacity <strong>of</strong> the equivalentSDOF system at that Limit State. Hence, if the seismic intensity is given by aPGA higher than the PGA capacity, the threshold <strong>di</strong>splacement capacity for thatLimit State is exceeded, and vice versa.If PGA capacity is “observed” in a population <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong>, accor<strong>di</strong>ng to afrequentistic approach the cumulative frequency <strong>di</strong>stribution <strong>of</strong> theseobservations provides the fragility curve (based on PGA seismic intensitymeasure) for that population <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong> and for that Limit State, based on thedefinitions themselves <strong>of</strong> fragility curve and PGA capacity.Given a defined buil<strong>di</strong>ng, some variables – which are input parameters forthe determination <strong>of</strong> the PGA capacity – can be defined as Random Variables,in order to investigate the influence <strong>of</strong> the uncertainty in the determination <strong>of</strong>such Variables on the seismic capacity <strong>of</strong> the structure. Hence, ProbabilityDensity Functions describing the expected values and the correspon<strong>di</strong>ngvariability for each one <strong>of</strong> these Variables can be defined. Accor<strong>di</strong>ng to asimulation technique, for instance, a number <strong>of</strong> samplings for these Variablescan be carried out. In this way, a population <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong> is generated, each onecorrespon<strong>di</strong>ng to a <strong>di</strong>fferent set <strong>of</strong> values <strong>of</strong> the defined Random Variables. IfPGA capacity, at a given Limit State, is calculated for all the generated<strong>buil<strong>di</strong>ngs</strong>, the cumulative frequency <strong>di</strong>stribution <strong>of</strong> the obtained values providesthe fragility curve for the buil<strong>di</strong>ng at that Limit State.In this study, the Monte Carlo simulation technique is used, and sampling <strong>of</strong>Random Variables is executed through the Latin Hypercube Sampling (LHS)technique. However, it would be too computationally deman<strong>di</strong>ng to carry out aSPO analysis (for calculating the PGA capacity) for each sample <strong>of</strong> the chosen


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 281Random Variables. Hence, a Response Surface Method (RSM) is applied (Pintoet al., 2004), briefly described in the following.In RSM, a scalar output variable y is assumed as depen<strong>di</strong>ng on k inputvariables x i . The relationship between the output variable and the inputvariables can be set in the form <strong>of</strong> a polynomial function <strong>of</strong> second order:k k k∑ ∑∑ (4.3.3.1)y = β + β x + β x x + ε0 i i ij i ji= 1 i= 1 j≥iwhere x i are the k input variables, β 0 , β i and β ij are the coefficients to bedetermined and ε is the error term. Hence, the mean model correspon<strong>di</strong>ng toEq. (4.3.3.1) isk k k k21 k= β0+ βi i+ βii i+ βij i ji= 1 i= 1 i= 1 j≥i( )∑ ∑ ∑∑ (4.3.3.2)y x ,..., x x x x xIf k input variables x i are considered, β coefficients are in the number <strong>of</strong>p = 1+ 2k + k( k − 1 ) / 2 .In order to estimate the β coefficients, some experiments have to be carried out.An experiment is defined as an observation (or measurement) <strong>of</strong> the outputvariable as response to some values <strong>of</strong> the assumed input variables x i . Theresults <strong>of</strong> n experiments can be written as⎡β0⎤⎢...⎥⎢ ⎥2⎢i( 1 ... xi... xi... xix j...β ⎥⎡ y)1 ⎤⎡⎤1 ⎡ε1⎤⎢ ......⎥⎢ ⎥ ⎢... ⎢⎥⎥ ⎢...⎥⎢ ⎥= ⎢⎥ + =⎢β⎥ ⎢ ⎥2ii⎢⎢⎥⎣y ⎥n ⎦ ⎢( 1 ... xi... xi... xix j...)⎢ ⎥ ⎢ε⎥n⎣ n⎥⎦ ⎣ ⎦ ⎢ ... ⎥⎢β⎥ij⎢ ⎥⎢⎣... ⎥⎦= Zβ + ε(4.3.3.3)where Z is the n × p design matrix, collecting the n row vectors correspon<strong>di</strong>ng


282 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infillsto the n experiments, and β is the p× 1 column vector collecting the βcoefficients to be determined. In each <strong>of</strong> the n row vectors <strong>of</strong> Z (one for eachexperiment) the so-called explanatory functions are collected. The explanatoryfunctions are the functions <strong>of</strong> the x i variables shown in Eq. (4.3.3.2).After carrying out n experiments, an estimate <strong>of</strong> β coefficients, representedby the p× 1 column vector b, can be obtained through the Or<strong>di</strong>nary LeastSquares method as1−1Tb = Z Z Z⎢...T( )⎡ y ⎤⎥⎢ ⎥⎢⎣y ⎥n ⎦(4.3.3.4)Now the Response Surface is defined, and m estimates <strong>of</strong> y can be obtainedthrough the RSM, as a function <strong>of</strong> m row vectors containing the explanatoryfunctions correspon<strong>di</strong>ng to the m chosen sets <strong>of</strong> values for the input variablesx i :2( 1 ... xi... xi... xix j...)⎡ y1⎤⎡⎤1⎢...⎥⎢⎥⎢ ⎥ = ⎢ ... ⎥ b⎢⎢y2⎥⎣ ⎥m ⎦ ⎢( 1 ... xi... xi... xix j...⎣) ⎥m ⎦(4.3.3.5)Hence, in order to estimate the second-order polynomial relationshipsbetween y and the input variables, n experiments have to be designed. To thisaim, the Central Composite Design (CCD) (Pinto et al., 2004) is used. Thismethod is interme<strong>di</strong>ate between the two-level and the three-level factorialdesigns. Considering that two levels (low and high) are chosen for each <strong>of</strong> the kinput variables x i , symmetrically located above and below an interme<strong>di</strong>atevalue, in a two-level factorial design experiments are performed for all the 2 kpossible combinations <strong>of</strong> low and high values. In a three-level factorial design,aimed at the determination <strong>of</strong> a full quadratic form, experiments are performedfor all the 3 k possible combinations that also include the interme<strong>di</strong>ate value foreach variable. CCD consists <strong>of</strong> ad<strong>di</strong>ng to a two-level factorial design furtherpoints, located at the centre and at two other points along each <strong>of</strong> the variables


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 283axes (Star points), see Figure 4.3.3.5.Figure 4.3.3.5. Component portions <strong>of</strong> Central Composite Design <strong>of</strong> experiments for 3 variables(Pinto et al., 2004)Once thekn = 1+ 2k + 2 CCD-based experiments have been carried out, theb vector – inclu<strong>di</strong>ng p = 1+ 2k + k( k − 1 ) / 2 parameters – can be estimated.Moreover, the scatter between the observed values <strong>of</strong> y from the nexperiments and the correspon<strong>di</strong>ng values that would be estimated on theResponse Surface can be calculated, representing the residual r u . Hence, thevariance <strong>of</strong> the error termthe fit, can be estimated assn2 2ε= ⋅ run p u=12σε, provi<strong>di</strong>ng an in<strong>di</strong>cation about the reliability <strong>of</strong>1∑ (4.3.3.6)−In our case, RSM is applied considering the PGA capacity as scalar outputvariable (y) and assuming as input variables <strong>di</strong>fferent material characteristicsand capacity parameters influencing the seismic capacity. Hence, in order toevaluate fragility curves, the Monte Carlo simulation technique is applied. Tothis aim, m sets <strong>of</strong> samplings <strong>of</strong> the considered input variables are carried out,accor<strong>di</strong>ng to the Probability Density Functions respectively assumed. Samplingis executed accor<strong>di</strong>ng to the LHS technique (McKay et al., 1979), assuming a


284 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills“me<strong>di</strong>an” sampling scheme (Vorechovsky and Novak, 2009). For each <strong>of</strong> the msets <strong>of</strong> sampled values, the correspon<strong>di</strong>ng value <strong>of</strong> the output variable (PGAcapacity) is estimated through RSM (see Eq. 4.3.3.5). Hence, fragility curvesare obtained as cumulative frequency <strong>di</strong>stributions <strong>of</strong> the PGA capacity.Evaluation <strong>of</strong> fragility curves: analysis <strong>of</strong> resultsThe above illustrated methodology for the evaluation <strong>of</strong> fragility curves isapplied to the case study buil<strong>di</strong>ng. In our case, the scalar output variable y is thePGA capacity for the Limit State <strong>of</strong> interest and the input variables are theRandom Variables selected in Section 4.3.1 (see Table 4.3.1.1), alreadyconsidered for the sensitivity analysis. In particular, in order to apply the aboveillustrated procedure, the considered input variables are represented by theRandom Variables normalized to their me<strong>di</strong>an values:Variable Me<strong>di</strong>an Value Distribution CoVf̂ c1 Lognormal 0.31f̂ y1 Lognormal 0.08G w1 Lognormal 0.30θ ̂ y1.015 Lognormal 0.331θ ̂ u0.995 Lognormal 0.409Table 4.3.3.1. Random Variables assumed to evaluate fragility curvesWhen designing the experiments to be carried out, CCD is applied asshown. In our case, the interme<strong>di</strong>ate values are represented by the me<strong>di</strong>anvalues. The Cube points are at a <strong>di</strong>stance <strong>of</strong> 1 time the standard deviation fromthe me<strong>di</strong>an values, whereas the position <strong>of</strong> the Star points is assumed at a<strong>di</strong>stance <strong>of</strong> 1.7 times the standard deviation from the centre <strong>of</strong> design (Liel etal., 2009). Each experiment is represented by a SPO analysis.Hence, the Center point corresponds to Model #1, as defined in Section4.3.1. These results, together with the results <strong>of</strong> the SPO analyses carried out


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 285with the sets <strong>of</strong> values correspon<strong>di</strong>ng to Star points (Models #2 to #11 – in thenumber <strong>of</strong> 2× 5 – for <strong>buil<strong>di</strong>ngs</strong> with infills, i.e. Uniformly infilled and Pilotisframes, and Models #2 to #9 – in the number <strong>of</strong> 2× 4 – for <strong>buil<strong>di</strong>ngs</strong> withoutinfills, i.e. Bare frame), have been illustrated in the sensitivity analysis.Therefore, SPO analyses with the sets <strong>of</strong> values correspon<strong>di</strong>ng to Cubepoints, in the number <strong>of</strong> 2 5 or 2 4 , are carried out now. Results are not reportedherein in detail for the sake <strong>of</strong> brevity.Hence, the number <strong>of</strong> experiments adds to5n = 1+ 2⋅ 5 + 2 = 43 or4n = 1+ 2⋅ 4 + 2 = 25 analyses for each buil<strong>di</strong>ng, in each <strong>di</strong>rection. These dataallow to estimate, accor<strong>di</strong>ng to Eq. 4.3.3.4, the 3× 2× 2 = 12 b vectors for PGAcapacity in Uniformly infilled, Pilotis and Bare frames, in X and Y <strong>di</strong>rectionsand at DL and NC Limit States, respectively. Each b vector includes theestimates <strong>of</strong> p = 1+ 2⋅ 5+ 5⋅( 5− 1 ) / 2 = 21 or ( )p = 1+ 2⋅ 4 + 4⋅ 4 − 1 / 2 = 15 βcoefficients.Variance <strong>of</strong> the error term (Eq. 4.3.3.6) is checked for all the 12 obtainedResponse Surfaces; maximum value is 2.9⋅ 10 −4 for Pilotis frame in X <strong>di</strong>rectionat NC Limit State, thus highlighting an acceptable scatter between the values <strong>of</strong>PGA capacity obtained from the n experiments and the correspon<strong>di</strong>ng values onResponse Surfaces.Subsequently, a LHS <strong>of</strong> the k=5 considered Random Variables is carriedout, thus obtaining m sets <strong>of</strong> values <strong>of</strong> these variables. In particular, m=1000samplings are executed. The m× k obtained sampling matrix is used to estimate– through RSM – the correspon<strong>di</strong>ng m values <strong>of</strong> PGA capacity, by applying Eq.4.3.3.5. This procedure is carried out 12 times, each time with a <strong>di</strong>fferent bvector (note that the same sampling matrix is always used; obviously in Bareframe only 4 <strong>of</strong> the 5 columns <strong>of</strong> the matrix are used). The correspon<strong>di</strong>ngcumulative frequency <strong>di</strong>stributions <strong>of</strong> the obtained PGA capacity valuesrepresent the 12 fragility curves for Uniformly infilled, Pilotis and Bare frames,in X and Y <strong>di</strong>rections and at DL and NC Limit States. Results are illustrated inthe following.


286 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infillsThe comparison between the me<strong>di</strong>an values <strong>of</strong> the fragility curves reportedherein has been actually already carried out through the previously reportedobservations, when comparing the seismic capacities <strong>of</strong> Uniformly infilled,Pilotis and Bare frame referring to Model #1. From a qualitative standpoint, theslope <strong>of</strong> the fragility curves – representing the variability associated with theseismic capacity – depends on the amount <strong>of</strong> variation in PGA capacity with thevariation in each Random Variable, shown in the sensitivity analysis. Lowerthis amount, lower the change in PGA capacity with the change in RandomVariables, less sensitive the PGA capacity to the modelled uncertainties, steeperthe fragility curve (as typically happens, for instance, at DL Limit State).1NC Limit State - X <strong>di</strong>rectionP f0.90.80.70.60.50.40.30.2Uniformly infilled0.1PilotisBare00 0.5 1 1.5 2 2.5PGA [g]Figure 4.3.3.6. Fragility curves at Near Collapse Limit State in X <strong>di</strong>rection


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 2871DL Limit State - X <strong>di</strong>rectionP f0.90.80.70.60.50.40.30.2Uniformly infilled0.1PilotisBare00 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1PGA [g]Figure 4.3.3.7. Fragility curves at Damage Limitation Limit State in X <strong>di</strong>rectionIf fragility curves at NC Limit State in X <strong>di</strong>rection are observed (see Figure4.3.3.6), a quite close me<strong>di</strong>an seismic capacity is noted between Uniformlyinfilled and Pilotis frame, whereas the Bare frame results as the morevulnerable. Nevertheless, the relatively low slope <strong>of</strong> the fragility curve for thePilotis frame reflects the particularly high influence <strong>of</strong> the uncertainty in θ u onthe seismic capacity <strong>of</strong> this frame (compare Figure 4.3.2.3 with Figures 4.3.2.19and 4.3.2.31).Fragility curves at DL Limit State in X <strong>di</strong>rection (see Figure 4.3.3.7)highlight the beneficial effect <strong>of</strong> uniformly <strong>di</strong>stributed infills on the seismiccapacity at this Limit State, that is, for relatively low seismic demand.Moreover, it is observed how in this case the detrimental effect <strong>of</strong> localizationin <strong>di</strong>splacement demand leads to a lower capacity <strong>of</strong> the Pilotis frame,compared with the remaining ones.


288 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills1NC Limit State - Y <strong>di</strong>rectionP f0.90.80.70.60.50.40.30.2Uniformly infilled0.1PilotisBare00 0.5 1 1.5 2 2.5PGA [g]Figure 4.3.3.8. Fragility curves at Near Collapse Limit State in Y <strong>di</strong>rectionIn Y <strong>di</strong>rection the fragility curves at NC Limit State (see Figure 4.3.3.8)highlight that the best seismic performance is provided by the Uniformlyinfilled frame, whereas the worst one is provided by the Pilotis frame.Moreover, it is noted how the seismic capacity <strong>of</strong> the Uniformly infilled frameis also less affected by <strong>di</strong>spersion compared with other frames.


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 2891DL Limit State - Y <strong>di</strong>rectionP f0.90.80.70.60.50.40.30.2Uniformly infilled0.1PilotisBare00 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1PGA [g]Figure 4.3.3.9. Fragility curves at Damage Limitation Limit State in Y <strong>di</strong>rectionFinally, also in Y <strong>di</strong>rection the beneficial effect <strong>of</strong> the increase in stiffnessand strength provided by uniformly <strong>di</strong>stributed infills on the seismic capacity atDL Limit State is clearly shown (see Figure 4.3.3.9).4.3.4. Comparison with simplified models based on Shear Type assumptionThe observation <strong>of</strong> failure modes carried out in Section 4.3.2 hashighlighted the importance <strong>of</strong> storey collapse mechanisms when evaluating theseismic capacity <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>. In particular, frames with infills arelikely to collapse under such a kind <strong>of</strong> mechanism, as already pointed out inliterature (see Section 4.2).In this Section, in view <strong>of</strong> the proposal <strong>of</strong> a simplified method for theassessment <strong>of</strong> seismic capacity <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> (see Chapter V), theidentical set <strong>of</strong> analyses previously illustrated is carried out on structuralmodels where the top and the bottom ends <strong>of</strong> each column have been restrainedagainst rotation (Shear Type models). Obviously, the only possible collapsemechanism in these models is a column-sway storey mechanism.


290 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infillsThe approximation <strong>of</strong> a seismic capacity assessment based on thisassumption is investigated through the comparison with the results evaluated on“exact” models and already illustrated in Section 4.3.2.4.3.4.1 Uniformly infilled frameX <strong>di</strong>rection1Uniformly infilled frame - X <strong>di</strong>rectionP f0.90.80.70.60.50.40.30.2DL - "exact"DL - Shear Type0.1NC - "exact"NC - Shear Type00 0.5 1 1.5 2 2.5PGA [g]Figure 4.3.4.1. Comparison between the fragility curves evaluated on “exact” and Shear Typemodels (Uniformly infilled frame – X <strong>di</strong>rection)It is to be noted that if “exact” models are considered, the Uniformly infilledframe in X <strong>di</strong>rection collapses under a s<strong>of</strong>t-storey mechanism at the 1 st storey inall cases except when a lower value is assumed for infill mechanicalcharacteristics; in this case there is a s<strong>of</strong>t-storey mechanism at the 2 nd storey.On the contrary, if Shear Type models are considered the frame alwayscollapses under a s<strong>of</strong>t-storey mechanism at the 1 st storey.The reasons for this <strong>di</strong>fference can be understood looking at the evolution <strong>of</strong>the damage in the frame that collapses under a s<strong>of</strong>t-storey mechanism at the 2 nd


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 291storey, <strong>di</strong>fferent from others (“exact” model, lower value <strong>of</strong> infill mechanicalcharacteristics). In uniformly infilled <strong>RC</strong> frames the s<strong>of</strong>t-storey collapsemechanism generally takes place at the storey the maximum strength in infillsis attained first. Nevertheless, in some cases the evolution <strong>of</strong> damage is<strong>di</strong>fferent. For instance, in the considered case, as the top <strong>di</strong>splacementincreases:1. the <strong>di</strong>splacement correspon<strong>di</strong>ng to maximum infill strength is overcomein all infill elements at 1 st storey;2. the <strong>di</strong>splacement correspon<strong>di</strong>ng to maximum infill strength is overcomein all infill elements at 2 nd storey;3. first <strong>RC</strong> column yields at 2 nd storey;4. s<strong>of</strong>t-storey collapse mechanism activates at 2 nd storey.This kind <strong>of</strong> “re<strong>di</strong>stribution“ <strong>of</strong> <strong>di</strong>splacement demand from the 1 st to the 2 ndstorey can take place if rotation at the ends <strong>of</strong> the columns is not retained, henceshear force contribution <strong>of</strong> these elements, step by step, is not <strong>di</strong>rectly andexclusively related to the interstorey <strong>di</strong>splacement, as happens in the ShearType model.However, more importantly, given equal the input material and capacitycharacteristics, a slight overestimation <strong>of</strong> the seismic capacity is noted whenShear Type models are used. As a matter <strong>of</strong> fact, if two correspon<strong>di</strong>ng modelsare considered, one “exact” and one Shear Type, in the Shear Type model the<strong>di</strong>splacement capacity does not change significantly, but the base shear capacityis slightly higher (due to the higher contribution <strong>of</strong> <strong>RC</strong> columns to themaximum base shear C s,max , due to their higher stiffness since rotation isretained at both ends). Moreover, the increase in stiffness also leads to abeneficial slight decrease in S dy , given practically equal the <strong>di</strong>splacementcapacity ∆ collapse . Hence, a slightly higher seismic capacity is obtained.Nevertheless, on the whole a very good agreement is observed between thetwo models, at both Limit States.


292 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infillsY <strong>di</strong>rection1Uniformly infilled frame - Y <strong>di</strong>rectionP f0.90.80.70.60.50.40.30.2DL - "exact"DL - Shear Type0.1NC - "exact"NC - Shear Type00 0.5 1 1.5 2 2.5PGA [g]Figure 4.3.4.2. Comparison between the fragility curves evaluated on “exact” and Shear Typemodels (Uniformly infilled frame – Y <strong>di</strong>rection)In Y <strong>di</strong>rection a very good agreement is observed, too. In the “exact” model,the buil<strong>di</strong>ng collapses under a s<strong>of</strong>t-storey mechanism at the 2 nd storey in allcases except when a lower value is assumed for f c and when an upper value isassumed for infill mechanical characteristics (in these cases the storey involvedby the collapse mechanism is the 1 st one) whereas in the Shear Type model thebuil<strong>di</strong>ng always collapses under a s<strong>of</strong>t-storey mechanism at the 1 st storey. Thereasons for this <strong>di</strong>fference have been previously described.As above illustrated, at NC Limit State in Shear Type models a slightoverestimation <strong>of</strong> the seismic capacity is observed, even if the collapsemechanism takes place at the same storey compared with the “exact” model. Inthis case, the fact that the collapse mechanism activate at the 1 st storey instead<strong>of</strong> the 2 nd one exalts this effect <strong>of</strong> decrease in <strong>di</strong>splacement capacity butincrease in base shear capacity, thus lea<strong>di</strong>ng to a slightly higher overestimation<strong>of</strong> seismic capacity, compared with the X <strong>di</strong>rection.


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 293ModelNo.Mo<strong>di</strong>fiedVariableStoreyValue T el ∆ lim ∆ coll T eff µ s C s,max C s,min r u µ lim µ coll R lim R coll S ae,lim S ae,coll PGA lim PGA coll involved incollapse∆ PGA,NC ∆ PGA,lim1 - - 0.12 0.01 0.14 0.15 3.13 0.75 0.28 0.38 2.29 26.36 1.33 2.88 0.99 2.16 0.39 0.84 1 - -2 f cµ-1.7σ 0.12 0.01 0.11 0.15 3.06 0.72 0.26 0.36 2.32 21.20 1.34 2.56 0.97 1.85 0.38 0.71 1 -15.1 -2.53 " µ+1.7σ 0.12 0.01 0.17 0.15 3.05 0.78 0.30 0.38 2.25 31.34 1.31 3.11 1.02 2.41 0.40 0.95 1 12.8 2.24 f yµ-1.7σ 0.12 0.01 0.14 0.15 3.06 0.75 0.27 0.36 2.30 26.50 1.33 2.78 1.00 2.09 0.39 0.81 1 -3.3 0.35 " µ+1.7σ 0.12 0.01 0.14 0.15 3.20 0.75 0.30 0.40 2.28 26.23 1.32 2.99 0.99 2.24 0.39 0.87 1 3.6 -0.36 G wµ-1.7σ 0.15 0.02 0.14 0.19 3.49 0.60 0.28 0.47 2.23 21.13 1.41 3.77 0.84 2.25 0.34 0.83 1 -1.7 -14.57 " µ+1.7σ 0.10 0.01 0.14 0.12 2.78 1.02 0.29 0.28 2.31 29.89 1.25 1.98 1.27 2.02 0.55 0.90 1 6.6 40.98 θ yµ-1.7σ 0.12 0.01 0.14 0.15 3.15 0.75 0.28 0.38 2.29 26.37 1.33 2.88 1.00 2.16 0.39 0.84 1 0.1 0.19 " µ+1.7σ 0.12 0.01 0.14 0.15 3.10 0.75 0.28 0.38 2.28 26.35 1.32 2.88 0.99 2.16 0.39 0.84 1 -0.2 -0.210 θ uµ-1.7σ 0.12 0.01 0.07 0.15 3.13 0.75 0.28 0.38 2.29 13.75 1.33 2.21 0.99 1.65 0.39 0.64 1 -24.4 0.011 " µ+1.7σ 0.12 0.01 0.27 0.15 3.13 0.75 0.28 0.38 2.29 50.98 1.33 4.01 0.99 3.01 0.39 1.19 1 41.4 0.0Table 4.3.4.1. Results <strong>of</strong> pushover and IN2 analyses on the Uniformly infilled frame (Shear Type model) in X <strong>di</strong>rectionModelNo.Mo<strong>di</strong>fiedVariableStoreyValue T el ∆ lim ∆ coll T eff µ s C s,max C s,min r u µ lim µ coll R lim R coll S ae,lim S ae,coll PGA lim PGA coll involved incollapse∆ PGA,NC ∆ PGA,lim1 - - 0.16 0.01 0.14 0.20 3.21 0.48 0.24 0.50 2.05 23.01 1.38 4.43 0.66 2.11 0.27 0.78 1 - -2 f cµ-1.7σ 0.17 0.01 0.11 0.20 3.15 0.45 0.22 0.49 2.12 18.35 1.41 3.86 0.64 1.75 0.26 0.66 1 -15.5 -2.33 " µ+1.7σ 0.16 0.01 0.17 0.20 3.06 0.50 0.25 0.50 1.99 27.42 1.36 4.85 0.67 2.40 0.27 0.88 1 12.9 2.24 f yµ-1.7σ 0.16 0.01 0.14 0.20 3.17 0.48 0.22 0.47 2.06 23.16 1.39 4.27 0.66 2.04 0.27 0.75 1 -3.1 0.45 " µ+1.7σ 0.16 0.01 0.14 0.20 3.23 0.47 0.25 0.53 2.04 22.83 1.38 4.60 0.66 2.18 0.27 0.80 1 3.2 -0.36 G wµ-1.7σ 0.20 0.01 0.14 0.25 4.08 0.38 0.23 0.61 1.99 18.88 1.46 5.56 0.56 2.12 0.23 0.78 1 0.7 -14.17 " µ+1.7σ 0.13 0.01 0.14 0.16 2.69 0.64 0.24 0.38 2.12 25.93 1.31 3.10 0.84 1.98 0.34 0.74 1 -5.5 25.18 θ yµ-1.7σ 0.16 0.01 0.14 0.20 3.24 0.48 0.24 0.50 2.05 22.97 1.38 4.42 0.66 2.11 0.27 0.78 1 0.0 0.29 " µ+1.7σ 0.16 0.01 0.14 0.20 3.16 0.47 0.24 0.50 2.05 23.06 1.39 4.44 0.66 2.11 0.27 0.78 1 -0.1 -0.210 θ uµ-1.7σ 0.16 0.01 0.07 0.20 3.21 0.48 0.24 0.50 2.05 12.07 1.38 3.08 0.66 1.46 0.27 0.56 1 -28.3 0.011 " µ+1.7σ 0.16 0.01 0.27 0.20 3.21 0.48 0.24 0.50 2.05 44.36 1.38 6.72 0.66 3.20 0.27 1.14 1 46.5 0.0Table 4.3.4.2. Results <strong>of</strong> pushover and IN2 analyses on the Uniformly infilled frame (Shear Type model) in Y <strong>di</strong>rection


294 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills4.3.4.2 Pilotis frameX <strong>di</strong>rection1Pilotis frame - X <strong>di</strong>rectionP f0.90.80.70.60.50.40.30.2DL - "exact"DL - Shear Type0.1NC - "exact"NC - Shear Type00 0.5 1 1.5 2 2.5PGA [g]Figure 4.3.4.3. Comparison between the fragility curves evaluated on “exact” and Shear Typemodels (Pilotis frame – X <strong>di</strong>rection)In Pilotis frame, as expected, the collapse mechanism takes place at thebottom bare storey in all cases, both for the “exact” and Shear Type models.Moreover, practically no <strong>di</strong>fference is observed in <strong>di</strong>splacement and base shearcapacity between these models. The only <strong>di</strong>fference is in the initial stiffness,consisting in a decrease in S dy for Shear Type models. This decrease isbeneficial at NC Limit State, lea<strong>di</strong>ng to an overestimation <strong>of</strong> seismic capacity.Nevertheless, at DL Limit State, which in this case is defined as the firstyiel<strong>di</strong>ng in <strong>RC</strong> elements, the higher stiffness leads to a decrease in the<strong>di</strong>splacement capacity ∆ f<strong>RC</strong>y , too, thus counterbalancing the decrease in S dy andfinally lea<strong>di</strong>ng to no appreciable <strong>di</strong>fference in seismic capacity.


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 295Y <strong>di</strong>rection1Pilotis frame - Y <strong>di</strong>rectionP f0.90.80.70.60.50.40.30.2DL - "exact"DL - Shear Type0.1NC - "exact"NC - Shear Type00 0.5 1 1.5 2 2.5PGA [g]Figure 4.3.4.4. Comparison between the fragility curves evaluated on “exact” and Shear Typemodels (Pilotis frame – Y <strong>di</strong>rection)In Y <strong>di</strong>rection, very similar considerations can be made. Also in this case, asexpected, the frame always collapses under a s<strong>of</strong>t-storey mechanism at thebottom bare storey, and an overestimation <strong>of</strong> seismic capacity is noted at NCLimit State when using Shear Type models, due to the beneficial influence <strong>of</strong>the higher initial stiffness.Also in this <strong>di</strong>rection, at DL Limit State, the decrease in the <strong>di</strong>splacementcapacity ∆ f<strong>RC</strong>y tends to counterbalance the decrease in S dy , thus lea<strong>di</strong>ng to a verysimilar seismic capacity.


296 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infillsModelNo.Mo<strong>di</strong>fiedVariableStoreyValue T el ∆ f<strong>RC</strong>y ∆ coll T eff C s,max µ f<strong>RC</strong>y µ coll R f<strong>RC</strong>y R coll S ae,f<strong>RC</strong>y S ae,coll PGA f<strong>RC</strong>y PGA coll involved incollapse∆ PGA,NC ∆ PGA,f<strong>RC</strong>y1 - - 0.35 0.02 0.14 0.46 0.24 1.22 10.37 1.22 9.65 0.30 2.35 0.16 0.86 1 - -2 f cµ-1.7σ 0.39 0.02 0.11 0.51 0.22 1.20 7.27 1.20 7.27 0.27 1.62 0.16 0.66 1 -23.5 -0.13 " µ+1.7σ 0.31 0.02 0.17 0.39 0.26 1.54 16.69 1.54 12.45 0.40 3.21 0.18 1.14 1 32.6 10.54 f yµ-1.7σ 0.34 0.02 0.14 0.44 0.23 1.28 11.80 1.28 10.52 0.30 2.43 0.16 0.89 1 3.1 -3.35 " µ+1.7σ 0.35 0.02 0.14 0.46 0.26 1.28 10.00 1.28 9.21 0.33 2.38 0.17 0.87 1 0.9 8.66 G wµ-1.7σ 0.35 0.02 0.14 0.44 0.24 1.34 11.22 1.34 9.93 0.33 2.43 0.17 0.89 1 2.9 4.57 " µ+1.7σ 0.34 0.02 0.14 0.46 0.24 1.25 10.75 1.25 9.85 0.31 2.40 0.16 0.88 1 1.8 1.48 θ yµ-1.7σ 0.34 0.02 0.14 0.44 0.24 1.32 11.51 1.32 10.11 0.32 2.47 0.17 0.90 1 4.4 2.79 " µ+1.7σ 0.35 0.02 0.14 0.46 0.24 1.25 10.22 1.25 9.58 0.30 2.34 0.17 0.86 1 -0.6 2.910 θ uµ-1.7σ 0.35 0.02 0.07 0.46 0.24 1.22 5.33 1.22 5.33 0.30 1.30 0.16 0.52 1 -40.0 0.011 " µ+1.7σ 0.35 0.02 0.27 0.46 0.24 1.22 20.21 1.22 16.81 0.30 4.10 0.16 1.43 1 66.1 0.0Table 4.3.4.3. Results <strong>of</strong> pushover and IN2 analyses on the Pilotis frame (Shear Type model) in X <strong>di</strong>rectionModelNo.Mo<strong>di</strong>fiedVariableStoreyValue T el ∆ f<strong>RC</strong>y ∆ coll T eff C s,max µ f<strong>RC</strong>y µ coll R f<strong>RC</strong>y R coll S ae,f<strong>RC</strong>y S ae,coll PGA f<strong>RC</strong>y PGA coll involved incollapse∆ PGA,NC ∆ PGA,f<strong>RC</strong>y1 - - 0.45 0.02 0.14 0.56 0.20 1.31 8.38 1.31 8.38 0.27 1.71 0.17 0.74 1 - -2 f cµ-1.7σ 0.50 0.02 0.11 0.65 0.19 1.11 5.01 1.11 5.01 0.21 0.95 0.16 0.53 1 -27.6 -6.83 " µ+1.7σ 0.41 0.02 0.17 0.51 0.21 1.42 11.65 1.42 11.65 0.30 2.49 0.18 0.91 1 24.4 3.34 f yµ-1.7σ 0.44 0.02 0.14 0.53 0.19 1.38 9.66 1.38 9.66 0.27 1.87 0.17 0.76 1 3.2 -4.35 " µ+1.7σ 0.46 0.02 0.14 0.59 0.22 1.21 7.00 1.21 7.00 0.26 1.52 0.18 0.70 1 -4.4 3.46 G wµ-1.7σ 0.45 0.02 0.14 0.58 0.20 1.23 7.69 1.23 7.69 0.25 1.58 0.17 0.71 1 -3.6 -2.57 " µ+1.7σ 0.44 0.02 0.14 0.58 0.20 1.21 7.80 1.21 7.80 0.25 1.59 0.17 0.72 1 -2.4 -3.78 θ yµ-1.7σ 0.44 0.02 0.14 0.57 0.20 1.24 8.08 1.24 8.08 0.25 1.65 0.17 0.72 1 -1.4 -3.39 " µ+1.7σ 0.45 0.02 0.14 0.56 0.20 1.32 8.16 1.32 8.16 0.27 1.67 0.18 0.73 1 -1.0 1.910 θ uµ-1.7σ 0.45 0.02 0.07 0.56 0.20 1.31 4.32 1.31 4.32 0.27 0.88 0.17 0.44 1 -39.5 0.011 " µ+1.7σ 0.45 0.02 0.27 0.56 0.20 1.31 16.30 1.31 16.30 0.27 3.33 0.17 1.22 1 65.6 0.0Table 4.3.4.4. Results <strong>of</strong> pushover and IN2 analyses on the Pilotis frame (Shear Type model) in Y <strong>di</strong>rection


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 2974.3.4.3 Bare frameX <strong>di</strong>rection1Bare frame - X <strong>di</strong>rectionP f0.90.80.70.60.50.40.30.2DL - "exact"DL - Shear Type0.1NC - "exact"NC - Shear Type00 0.5 1 1.5 2 2.5PGA [g]Figure 4.3.4.5. Comparison between the fragility curves evaluated on “exact” and Shear Typemodels (Bare frame – X <strong>di</strong>rection)The Bare frame in X <strong>di</strong>rection always collapses under a column-sway storeymechanism at the 3 rd storey, both in “exact” and in Shear Type models. Hence,the only reason for the slight shift in PGA capacity at NC Limit State (whenShear Type models are used instead <strong>of</strong> “exact” ones) is the beneficial thedecrease in S dy again observed. Moreover, it is observed how the fragility curveevaluated on “exact” models is steeper. The reason for this slight <strong>di</strong>fference canbe understood looking at the <strong>di</strong>fferent influence <strong>of</strong> the change in randomvariables observed in the two kind <strong>of</strong> models (see Figure 4.3.4.6): PGAcapacity at NC in Shear Type models is slightly more sensitive to the variation<strong>of</strong> θ u and f c (which are the only parameters characterized by a significantinfluence) compared with the “exact” models. Hence, a higher variability inPGA capacity at NC in Shear Type models is expected, reflected by the


298 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills<strong>di</strong>fferent slope <strong>of</strong> the fragility curve. At DL Limit State, instead, no appreciable<strong>di</strong>fference is observed.Sensitivity analysisSensitivity analysisthuthuVariablefcfyVariablefcfythyUpper valueLower value-60 -40 -20 0 20 40 60Change in PGA at collapse (%)thyUpper valueLower value-60 -40 -20 0 20 40 60Change in PGA at collapse (%)(a)(b)Figure 4.3.4.6. Comparison between the influence <strong>of</strong> random variables on the PGA capacity atNC LS in “exact” (a) and Shear Type (b) models (Bare frame – X <strong>di</strong>rection)Y <strong>di</strong>rection1Bare frame - Y <strong>di</strong>rectionP f0.90.80.70.60.50.40.30.2DL - "exact"DL - Shear Type0.1NC - "exact"NC - Shear Type00 0.5 1 1.5 2 2.5PGA [g]Figure 4.3.4.7. Comparison between the fragility curves evaluated on “exact” and Shear Typemodels (Bare frame – Y <strong>di</strong>rection)


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 299The most significant <strong>di</strong>fferences between the results obtained from “exact”and Shear Type models are observed for the Bare frame in Y <strong>di</strong>rection.These <strong>di</strong>fferences are essentially due to the complete change in collapsemechanism: in “exact” models the frame collapses under a global mechanisminvolving all the four storeys; a reason for the formation <strong>of</strong> such a mechanismcan be certainly found in the absence <strong>of</strong> beams in internal frames along this<strong>di</strong>rection. On the contrary, in Shear Type models only column-sway storeymechanism can take place. In particular, the collapsed storey is the 2 nd one in allcases except when a lower value <strong>of</strong> f c is considered; in this case, the collapsemechanism involves the 3 rd storey. This <strong>di</strong>fference leads a much lower ductility,obviously, but also to a much higher base shear capacity in the Shear Typemodel. If IN2 in terms <strong>of</strong> S ae (T eff ) curves are compared (see Figure 4.3.4.8), asignificant overestimation <strong>of</strong> the seismic capacity in the Shear Type model,compared with the “exact” model, is observed. Nevertheless, the correct way tocompare seismic capacities is in terms <strong>of</strong> PGA (see Figure 4.3.4.9), and in thiscase the relative ratio between the seismic capacities significantly changes, dueto the high <strong>di</strong>fference in T eff , thus highlighting that in Shear Type models thedetrimental effect <strong>of</strong> ductility decrease prevails, lea<strong>di</strong>ng to an underestimation<strong>of</strong> the actual seismic capacity at NC Limit State.Moreover, it is observed how the fragility curve evaluated on Shear Typemodels is steeper. Again, the reason for this <strong>di</strong>fference can be understoodlooking at the <strong>di</strong>fferent influence <strong>of</strong> the change in random variables on the PGAcapacity (see Figure 4.3.4.10): PGA capacity at NC in Shear Type models isless sensitive to the variation <strong>of</strong> f c and, above all, <strong>of</strong> θ u , thus lea<strong>di</strong>ng to a higherslope <strong>of</strong> the fragility curve.At DL Limit State, instead, the increase in stiffness and strength observed inthe Shear Type model prevails, lea<strong>di</strong>ng to an overestimation <strong>of</strong> seismiccapacity.


300 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills0.90.80.70.6S ae (T eff ) [g]0.50.40.30.20.100 0.05 0.1 0.15 0.2 0.25 0.3 0.35 0.4 0.45 0.5Top <strong>di</strong>splacement in Y <strong>di</strong>rection [m]Figure 4.3.4.8. Pushover and IN2 curves in terms <strong>of</strong> S ae (T eff ) for Model #1 in “exact” and ShearType models (Bare frame – Y <strong>di</strong>rection)0.70.60.5PGA [g]0.40.30.20.100 0.05 0.1 0.15 0.2 0.25 0.3 0.35 0.4 0.45 0.5Top <strong>di</strong>splacement in Y <strong>di</strong>rection [m]Figure 4.3.4.9. IN2 curves in terms <strong>of</strong> PGA for Model #1 in “exact” and Shear Type models(Bare frame – Y <strong>di</strong>rection)


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 301Sensitivity analysisSensitivity analysisthuthuVariablefcfyVariablefcfythyUpper valueLower value-60 -40 -20 0 20 40 60Change in PGA at collapse (%)thyUpper valueLower value-60 -40 -20 0 20 40 60Change in PGA at collapse (%)(a)(b)Figure 4.3.4.10. Comparison between the influence <strong>of</strong> random variables on the PGA capacity atNC LS in “exact” (a) and Shear Type (b) models (Bare frame – Y <strong>di</strong>rection)


302 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infillsModelNo.Mo<strong>di</strong>fiedVariableStoreyValue T el ∆ f<strong>RC</strong>y ∆ coll T eff C s,max µ f<strong>RC</strong>y µ coll R f<strong>RC</strong>y R coll S ae,f<strong>RC</strong>y S ae,coll PGA f<strong>RC</strong>y PGA coll involved incollapse∆ PGA,NC ∆ PGA,f<strong>RC</strong>y1 - - 0.59 0.05 0.19 0.75 0.20 1.39 5.02 1.39 5.02 0.28 1.02 0.23 0.62 3 - -2 f cµ-1.7σ 0.67 0.06 0.16 0.86 0.19 1.26 3.58 1.26 3.58 0.24 0.69 0.23 0.51 3 -18.0 -1.73 " µ+1.7σ 0.53 0.04 0.21 0.63 0.21 1.64 7.67 1.64 7.67 0.35 1.62 0.24 0.77 3 24.0 1.74 f y µ-1.7σ 0.58 0.05 0.18 0.71 0.19 1.49 5.86 1.49 5.86 0.29 1.13 0.22 0.64 3 3.0 -4.25 " µ+1.7σ 0.61 0.06 0.19 0.77 0.22 1.38 4.53 1.38 4.53 0.30 0.98 0.25 0.62 3 -0.7 7.16 θ yµ-1.7σ 0.59 0.05 0.19 0.74 0.20 1.41 5.14 1.41 5.14 0.29 1.05 0.23 0.63 3 0.8 -0.57 " µ+1.7σ 0.60 0.05 0.19 0.76 0.20 1.39 4.89 1.39 4.89 0.28 1.00 0.24 0.62 3 -0.7 1.58 θ u µ-1.7σ 0.59 0.05 0.11 0.75 0.20 1.39 3.03 1.39 3.03 0.28 0.62 0.23 0.43 3 -31.8 0.09 " µ+1.7σ 0.59 0.05 0.33 0.75 0.20 1.39 8.89 1.39 8.89 0.28 1.81 0.23 0.96 3 54.4 0.0Table 4.3.4.5. Results <strong>of</strong> pushover and IN2 analyses on the Bare frame (Shear Type model) in X <strong>di</strong>rectionModelNo.Mo<strong>di</strong>fiedVariableStoreyValue T el ∆ f<strong>RC</strong>y ∆ coll T eff C s,max µ f<strong>RC</strong>y µ coll R f<strong>RC</strong>y R coll S ae,f<strong>RC</strong>y S ae,coll PGA f<strong>RC</strong>y PGA coll involved incollapse∆ PGA,NC ∆ PGA,f<strong>RC</strong>y1 - - 0.67 0.07 0.20 0.88 0.21 1.31 3.80 1.31 3.80 0.28 0.81 0.26 0.59 2 - -2 f cµ-1.7σ 0.76 0.07 0.17 1.01 0.20 1.14 2.69 1.14 2.69 0.23 0.53 0.25 0.48 2 -18.9 -4.93 " µ+1.7σ 0.60 0.06 0.22 0.77 0.22 1.50 5.39 1.50 5.39 0.33 1.18 0.27 0.71 3 21.3 3.34 f y µ-1.7σ 0.65 0.06 0.19 0.86 0.20 1.32 4.13 1.32 4.13 0.26 0.83 0.25 0.59 2 -0.1 -5.75 " µ+1.7σ 0.69 0.08 0.20 0.91 0.23 1.27 3.43 1.27 3.43 0.29 0.77 0.28 0.58 2 -0.5 5.46 θ yµ-1.7σ 0.66 0.07 0.20 0.87 0.21 1.29 3.81 1.29 3.81 0.27 0.81 0.26 0.59 2 -0.2 -1.37 " µ+1.7σ 0.68 0.07 0.20 0.89 0.21 1.31 3.72 1.31 3.72 0.28 0.79 0.27 0.58 2 -0.4 1.68 θ u µ-1.7σ 0.67 0.07 0.13 0.88 0.21 1.31 2.45 1.31 2.45 0.28 0.52 0.26 0.42 2 -28.4 0.09 " µ+1.7σ 0.67 0.07 0.33 0.88 0.21 1.31 6.45 1.31 6.45 0.28 1.37 0.26 0.88 2 49.3 0.0Table 4.3.4.6. Results <strong>of</strong> pushover and IN2 analyses on the Bare frame (Shear Type model) in Y <strong>di</strong>rection


Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infills 3034.3.4.4 Summary <strong>of</strong> remarksAs far as frames with infills are concerned (both Uniformly infilled andPilotis frame), a capacity assessment carried out with Shear Type models yieldsresults very close to the results obtained by means <strong>of</strong> “exact” models, except fora slight overestimation <strong>of</strong> seismic capacity due to the influence <strong>of</strong> the stiffnessincrease, whereas <strong>di</strong>splacement and strength capacities are actually very closebetween the two types <strong>of</strong> models. The effectiveness <strong>of</strong> the Shear Typeapproximation (that only allows column-sway storey mechanisms) certainlyderives from the fact that also in “exact” models a column-sway storeymechanism always occurs.Results from the Bare frame highlight the possible limits <strong>of</strong> the Shear Typeapproximation. In longitu<strong>di</strong>nal <strong>di</strong>rection, where a column-sway storeymechanisms occurs also in the “exact” model (due to the absence <strong>of</strong> weakbeam/strong column con<strong>di</strong>tion), the comparison <strong>of</strong> results obtained accor<strong>di</strong>ng tothe two models points out a still acceptable agreement. In longitu<strong>di</strong>nal<strong>di</strong>rection, where a global mechanism actually occurs in the “exact” model, theShear Type approximation yields less good results, as expected, at bothconsidered Limit States.Further research is needed in order to investigate the influence <strong>of</strong> otherparameter such as, for instance, the type <strong>of</strong> design or the number <strong>of</strong> storeys.However, especially for infilled <strong>buil<strong>di</strong>ngs</strong>, the illustrated approach based onShear Type assumption may fit the needs <strong>of</strong> a seismic <strong>vulnerability</strong> assessmentat large scale, which certainly requires the adoption <strong>of</strong> simplifiedmethodologies characterized by a low computational demand (see Section5.2.4) and based on poor knowledge data (see Sections 5.2.1 and 5.2.2), thusrepresenting a good compromise between acceptable approximation andeffectiveness in assessing the seismic capacity.


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308 Chapter IV – Numerical investigation <strong>of</strong> seismic capacity <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> with infillsand 10 th Cana<strong>di</strong>an Conference on Earthquake Engineering, Toronto,Canada, July 25-29.− Valiasis T.N., 1989. Experimental investigation <strong>of</strong> the behavior <strong>of</strong> <strong>RC</strong>frames infilled with masonry panels and subjected to cyclic horizontalload - Analytical modeling <strong>of</strong> the masonry panel. PhD thesis, AristotleUniversity <strong>of</strong> Thessaloniki, Greece. (in Greek)− Verderame G.M., Polese M, Mariniello C., Manfre<strong>di</strong> G., 2010a. Asimulated design procedure for the assessment <strong>of</strong> seismic capacity <strong>of</strong><strong>existing</strong> reinforced concrete <strong>buil<strong>di</strong>ngs</strong>. Advances in EngineeringS<strong>of</strong>tware, 41(2), 323-335.− Verderame G.M., Manfre<strong>di</strong> G., Frunzio G., 2001. Le proprietàmeccaniche dei calcestruzzi impiegati nelle strutture in cemento armatorealizzate negli anni ’60. Atti del X congresso nazionale ANIDIS‘‘L’ingegneria Sismica in Italia”, Potenza-Matera, Italy, September 9-13.(in Italian)− Verderame G.M., Ricci P., Manfre<strong>di</strong> G., 2010b. Statistical analysis <strong>of</strong>mechanical characteristics <strong>of</strong> reinforcing bars in Italy between 1950 and1980, ACI Structural Journal. (in preparation)− Vorechovsky M., Novak D., 2009. Correlation control in small-sampleMonte Carlo type simulations I: A simulated annealing approach.Probabilistic Engineering Mechanics, 24(3), 452-462.


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 309the case study <strong>of</strong> AvellinoChapter VSimplified approach to the seismic <strong>vulnerability</strong>assessment <strong>of</strong> <strong>existing</strong> reinforced concrete<strong>buil<strong>di</strong>ngs</strong>: the case study <strong>of</strong> Avellino5.1 INTRODUCTIONSimplified methodologies for seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong>tocks are <strong>of</strong> fundamental importance for the development <strong>of</strong> earthquake lossmodels. These models are needed to support the decision process in <strong>di</strong>sasterprevention and emergency management, as far as seismic risk is concerned (seeChapter I). In this Chapter, a simplified method is presented for reinforcedconcrete <strong>buil<strong>di</strong>ngs</strong>, employing a simulated design procedure to evaluate thebuil<strong>di</strong>ng structural characteristics based on few data such as number <strong>of</strong> storeys,global <strong>di</strong>mensions and type <strong>of</strong> design, and on the assumption <strong>of</strong> a Shear Typebehaviour to evaluate in closed form the non-linear static response. Theapproximation in the evaluation <strong>of</strong> seismic capacity due to a Shear Typeassumption has been illustrated in Section 4.3.4. Hence, the assessment <strong>of</strong> theseismic capacity is evaluated within the framework <strong>of</strong> the N2 method, lea<strong>di</strong>ngto the construction <strong>of</strong> fragility curves and, finally, to the evaluation <strong>of</strong> thefailure probability in given time windows and for given Limit States.The steps <strong>of</strong> the simplified procedure are described in detail in Section 5.2,


310 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> Avellinotogether with an example application.In Section 5.3, results from the field survey carried out on buil<strong>di</strong>ng stock <strong>of</strong>the Avellino city (southern Italy) within the SIMURAI project (2010) will bedescribed first, from the preparation <strong>of</strong> the survey form to the analysis <strong>of</strong>collected data. Then, the previously illustrated simplified approach to theseismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> will be applied to such data,and obtained results will be illustrated.5.2 A SIMPLIFIED PROCEDURE FOR THE ASSESSMENT OFSEISMIC VULNERABILITY OF <strong>RC</strong> BUILDINGIn this Section, the step <strong>of</strong> the previously summarized procedure areillustrated in detail. The procedure described herein has been implemented inPOST (PushOver on Shear Type models), a s<strong>of</strong>tware based on MATLAB®code, inclu<strong>di</strong>ng a graphical interface. Some screenshots from this s<strong>of</strong>tware willbe reported in next Sections.5.2.1. Definition <strong>of</strong> input dataThe first step <strong>of</strong> the procedure consists <strong>of</strong> the definition <strong>of</strong> input data. Thesedata include:- global geometrical parameters;- <strong>di</strong>stribution <strong>of</strong> infill panels;- type <strong>of</strong> design and values <strong>of</strong> allowable stresses to be employed in thesimulated design procedure;- material characteristics;- data for the definition <strong>of</strong> seismic hazard.Considered <strong>buil<strong>di</strong>ngs</strong> are rectangular in plan. Hence, the parameters neededto completely define the global buil<strong>di</strong>ng geometry include: number <strong>of</strong> storeys,plan <strong>di</strong>mensions in longitu<strong>di</strong>nal (X) and transversal (Y) <strong>di</strong>rections, number <strong>of</strong>bays in X and Y, height <strong>of</strong> the bottom storey, height <strong>of</strong> upper storeys. Hence, a


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 311the case study <strong>of</strong> Avellinopossible irregularity in interstorey height (<strong>of</strong>ten due to architectonic orfunctional reasons) is considered.The presence <strong>of</strong> infill panels can be defined accor<strong>di</strong>ng to three <strong>di</strong>fferentoptions: (i) Uniformly infilled buil<strong>di</strong>ng, (ii) Pilotis buil<strong>di</strong>ng or (iii) Barebuil<strong>di</strong>ng. The opening percentage can also be defined, both in bottom infillpanels (case i) and in upper infill panels (cases i and ii). If present, infill panelsare regularly <strong>di</strong>stributed in plan in all the external frames in X and Y <strong>di</strong>rections.The design can be defined as “gravitational” or “seismic”. If the design isseismic, the base shear coefficient prescribed by code (to be employed in thesimulated design procedure) is needed as input. Values <strong>of</strong> allowable stress forconcrete and steel are also defined. The details <strong>of</strong> the simulated designprocedure will be illustrated in Section 5.2.2.Material characteristics are defined, namely the concrete compressivestrength, the steel yield strength and the infill characteristics (if infill panels arepresent). The latter include the thickness <strong>of</strong> infill panels, the infill mechanicalcharacteristics (shear cracking strength, shear elastic modulus and Young’selastic modulus) and parameters α and β, respectively representing the ratiobetween post-capping degra<strong>di</strong>ng stiffness and elastic stiffness and the ratiobetween residual strength and maximum strength. Hence, the envelope <strong>of</strong> thelateral force <strong>di</strong>splacement relationship <strong>of</strong> infill panels can be completelydefined, accor<strong>di</strong>ng to the adopted model (see Section 5.2.3). Values <strong>of</strong> infillmechanical characteristics from the Italian code (Circolare 617, 2009) areproposed as default values for <strong>di</strong>fferent infill typologies.Finally, the data for the definition <strong>of</strong> seismic hazard are defined. Theprobabilistic seismic hazard assessment carried out for Italy (INGV-DPC S1,2007) is adopted. Hence, the location <strong>of</strong> the buil<strong>di</strong>ng is needed, defined by itsLongitude and Latitude. Stratigraphic (A to E) and topographic (T1 to T4)con<strong>di</strong>tions are defined, accor<strong>di</strong>ng to the Italian code (DM 14/1/2008).Moreover, V N , C U and P VR are defined (representing the nominal life, theimportance coefficient (provi<strong>di</strong>ng the reference period V R as V N·C U ) and theprobability <strong>of</strong> exceedance in the reference period, respectively) to obtain the


312 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> Avellinoelastic spectrum used for a single assessment <strong>of</strong> seismic demand (see Section5.2.5).Figure 5.2.1.1. Definition <strong>of</strong> input data in POST s<strong>of</strong>tware5.2.2. Simulated design procedureThe simulated design procedure adopted herein (Verderame et al., 2010a) isbased on the compliance with past code prescriptions and design practices forItalian <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>. Hence, the allowable stresses method is followed.First, design loads are defined. As far as gravity loads are concerned, deadloads are evaluated from a load analysis, whereas live loads are evaluated frompast code prescriptions for or<strong>di</strong>nary structures (e.g., 2 kN/m 2 ). Lateral loads(evaluated if the selected type <strong>of</strong> design is “seismic”) are calculated based onthe assigned base shear coefficient (ratio between the design base shear and theweight <strong>of</strong> the structure). Typical values for this coefficient were, for instance,0.07 or 0.10, accor<strong>di</strong>ng to the category <strong>of</strong> the seismic zone (e.g., see Section2.5).Then, element <strong>di</strong>mensions are evaluated. To this aim, accor<strong>di</strong>ng to pastdesign practices, column area is determined as the ratio between the axial load


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 313the case study <strong>of</strong> Avellino(evaluated referring to the area <strong>of</strong> influence <strong>of</strong> each column) and the allowablestress <strong>of</strong> concrete. In seismic design, the latter was typically multiplied by acoefficient γ lower than 1, roughly accounting for combined axial load andben<strong>di</strong>ng action acting on the column due to lateral loads (Pecce et al., 2004).Hence, γ was typically assumed equal to 1 in gravity load design. Coefficient γis given as an input for the simulated design procedure. The column section isthen determined from the calculated area, starting from a width equal to 30 cmand considering a maximum height <strong>of</strong> 70 cm. If the calculated area is higherthan ( 30× 70)cm 2 , column width is increased from 30 to 35 cm, and so on. Anupper approximation <strong>of</strong> 5 cm is considered for the determination <strong>of</strong> sectionheight. The beam width is given equal to 30 cm and the correspon<strong>di</strong>ng height iscalculated based on the maximum ben<strong>di</strong>ng moment acting on the beam forgravity loads from slabs; this moment is calculated with a formulationaccounting in a simplified way for the element constraint scheme. Finally,column <strong>di</strong>mensions are checked to avoid cross-section variation higher than 10cm between two adjacent storeys.Once column and beam <strong>di</strong>mensions have been calculated, reinforcement incolumns is designed. Beam reinforcement is not designed since in the assumedShear Type model the behaviour <strong>of</strong> beam elements has not to be modelled (seeSection 5.2.3).As far as gravitational design is concerned, the design <strong>of</strong> columnreinforcement is based on the minimum amount <strong>of</strong> longitu<strong>di</strong>nal reinforcementgeometric ratio prescribed by code (e.g., 0.8% <strong>of</strong> the minimum concrete areaaccor<strong>di</strong>ng to RDL 2229 (1939), or 0.6% accor<strong>di</strong>ng to DM 3/3/1975)). Once theminimum area <strong>of</strong> reinforcement has been determined, a set <strong>of</strong> possible values <strong>of</strong>bar <strong>di</strong>ameter is considered and the combination <strong>of</strong> (even) number and <strong>di</strong>ameter<strong>of</strong> bars provi<strong>di</strong>ng the best upper approximation is chosen. Hence, bars are<strong>di</strong>stributed along the periphery <strong>of</strong> the section as uniformly as possible.In seismic design, storey shear forces are evaluated from lateral forces,which are calculated as a fraction <strong>of</strong> the weight <strong>of</strong> the structure, based on theassigned base shear coefficient. Hence, the <strong>di</strong>stribution <strong>of</strong> the storey shear


314 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> Avellinoamong the columns <strong>of</strong> the storey is based on the ratio <strong>of</strong> inertia <strong>of</strong> the singlecolumn versus the sum <strong>of</strong> inertia <strong>of</strong> all the columns at the considered storey(Shear Type element model). The ben<strong>di</strong>ng moment acting at the ends <strong>of</strong> eachcolumn is obtained multiplying the correspon<strong>di</strong>ng shear force by half <strong>of</strong> thecolumn height, accor<strong>di</strong>ng to the assumed Shear Type model; the axial load iscalculated from gravity loads, given by the sum <strong>of</strong> gravity loads and <strong>of</strong> afraction <strong>of</strong> live loads (30%), always based on the area <strong>of</strong> influence <strong>of</strong> thecolumn. Then, based on the assigned values <strong>of</strong> allowable stress for steel andconcrete, the reinforcement area is designed to provide a flexural strength(accor<strong>di</strong>ng to the allowable stresses method) not lower than the ben<strong>di</strong>ngmoment from design. Again, the combination <strong>of</strong> number and <strong>di</strong>ameter <strong>of</strong> barsprovi<strong>di</strong>ng the best upper approximation is chosen, provided at least two barsper layer. The described procedure is carried out in both <strong>di</strong>rections. Hence, thetotal amount <strong>of</strong> longitu<strong>di</strong>nal reinforcement is compared with the minimumamount prescribed by the considered code; the maximum between these valuesis assumed.Transverse reinforcement in columns is designed too. In gravitationaldesign, a minimum amount <strong>of</strong> transverse reinforcement is provided, based oncode prescriptions. For instance, accor<strong>di</strong>ng to (RDL 2229/1939) stirrup spacingin columns had to be determined as the minimum value between (i) half <strong>of</strong> theminimum section <strong>di</strong>mension and (ii) ten times the <strong>di</strong>ameter <strong>of</strong> longitu<strong>di</strong>nalreinforcement, whereas accor<strong>di</strong>ng to (DM 40/1975) it was determined as theminimum value between (i) 25 cm and (ii) fifteen times the minimum <strong>di</strong>ameter<strong>of</strong> longitu<strong>di</strong>nal reinforcement. In seismic design, transverse reinforcement isdesigned to resist the shear force due to lateral forces, calculated as previouslyillustrated. It is to be noted that in several old technical codes a so-called“threshold-based” design method for transverse reinforcement was proposed(see Section 2.3): a value <strong>of</strong> allowable tangential stress was assumed (e.g., τ c0 )and, if the design stress <strong>di</strong>d not exceed this value, only a minimum amount <strong>of</strong>transverse reinforcement was prescribed. Hence, in the simulated designprocedure τ c0 is evaluated, depen<strong>di</strong>ng on the allowable concrete stress, and is


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 315the case study <strong>of</strong> Avellinocompared with the shear stress demand τ. Then, ifevaluated assA ⋅σ ⋅0.9dτ > τc0, the stirrup spacing issw s,adm= (5.2.2.1)Vwhere A sw is the unit transverse reinforcement area, σ s,adm is the allowable steelstress, d is the column effective depth and V is the shear force. Stirrup <strong>di</strong>ameteris given as an input.5.2.3. Characterization <strong>of</strong> nonlinear responseBased on the assumed Shear Type model, the lateral response <strong>of</strong> thestructure under a given <strong>di</strong>stribution <strong>of</strong> lateral forces can be completelydetermined based on the interstorey shear-<strong>di</strong>splacement relationships at eachstorey. Hence, the nonlinear response <strong>of</strong> column and infill elements has to bedetermined.The nonlinear behaviour <strong>of</strong> each column element is characterized as aT( ∆ ) relationship evaluated from the correspon<strong>di</strong>ng ( )consistent with the Shear Type assumption (see Figure 5.2.3.1).M θ relationship,TM∆hθL V =h/2MTMoment<strong>di</strong>stributionFigure 5.2.3.1. Shear type assumptionThe moment-rotation envelope M( θ ) is calculated assuming a shear span


316 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> Avellinoequal to half <strong>of</strong> the column height (L V = h/2). A tri-linear envelope for M( θ ) isassumed, with three characteristic points: cracking, yiel<strong>di</strong>ng and ultimatecon<strong>di</strong>tion. Behaviour is linear elastic up to cracking and perfectly-plastic afteryiel<strong>di</strong>ng.Moment and rotation at cracking are evaluated as:Mcr⎛ N ⎞ B⋅H= ⎜ − fct+ ⎟⋅⎝ B⋅H ⎠ 62(5.2.3.1)M hEI 6crθcr= ⋅ (5.2.3.2)where f ct is the concrete strength in tension, N is the axial load acting on thecolumn, B and H are width and height <strong>of</strong> the column section (in the considered<strong>di</strong>rection), EI is the gross flexural inertia <strong>of</strong> the section and h is the columnheight.Moment (M y ) and section curvature at yiel<strong>di</strong>ng are calculated in closed formby means <strong>of</strong> the first principles-based simplified formulations proposed in(Far<strong>di</strong>s, 2007 – Section 2.2.1.3, Eqs. 2.12 to 2.18). Hence, rotations at yiel<strong>di</strong>ng(θ y ) and ultimate (θ u ) are evaluated through Eqs. 2.20a and 3.27a, respectively,from the same study. The type <strong>of</strong> reinforcement is given as input, too; if smoothbars are present, no reduction for the lack <strong>of</strong> seismic detailing is applied, seeSection 2.2.2.The relationship between the <strong>di</strong>splacement ∆ and the shear T for eachcolumn is evaluated from the relationship between the rotation θ and themoment M, based on the following relationship:( )M θ ⋅2T( ∆ ) = T( θ⋅ h)= (5.2.3.3)hShear strength is also calculated for each column, accor<strong>di</strong>ng to the modelproposed by (Biskinis et al., 2004), also adopted in EC8-part 3 (CEN, 2005)(see Section 2.3). In this model, a degradation <strong>of</strong> the shear strength with the


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 317the case study <strong>of</strong> Avellinoductility demand is modelled. In particular, a coefficientrepresenting the plastic part <strong>of</strong> ductility demand.The initial shear strengthcalculated, the latter attained forplµ∆is adopted,VR,maxand the residual shear strength VR,minareµ = 5 , that is, for ∆ = ( 1+ 5) ⋅ ∆y. Hence, it ispl∆possible to determine if column behaviour is controlled by flexure, by shearflexureinteraction or by shear (see Section 2.3). In second and third cases, a<strong>di</strong>splacement is determined on the T − ∆ envelope (post- or pre-yiel<strong>di</strong>ng,respectively) correspon<strong>di</strong>ng to shear failure, thus representing a furthercharacteristic envelope point.Lateral force-<strong>di</strong>splacement relationships for infill panels are evaluated fromthe model proposed by Panagiotakos and Far<strong>di</strong>s (see Section 3.2.4), based onpreviously defined data (panel thickness, infill mechanical characteristics andmodel parameters α and β) and evaluating clear <strong>di</strong>mensions <strong>of</strong> the panelconsidering section <strong>di</strong>mensions <strong>of</strong> surroun<strong>di</strong>ng beams and columns. Theinfluence <strong>of</strong> openings is taken into account through a coefficient linearlydependent on the opening ratio A openings /A panel , based on the experimentalresults reported in (Kakaletsis and Karayannis, 2009):⎛ Aλopenings= max 0;1−1.8⋅⎜⎝ Aopeningspanel⎞⎟⎠(5.2.3.4)Hence, envelope forces in the load-<strong>di</strong>splacement relationship <strong>of</strong> the panel aremultiplied by λ openings .At each storey, the relationship between the interstorey <strong>di</strong>splacement andthe correspon<strong>di</strong>ng interstorey shear is evaluated considering all the <strong>RC</strong> columnsand the infill elements (if present) acting in parallel. To this aim, <strong>di</strong>splacementvalues correspon<strong>di</strong>ng to characteristic points <strong>of</strong> lateral force-<strong>di</strong>splacementenvelopes <strong>of</strong> <strong>RC</strong> columns and infill elements are sorted in a vector; then, foreach <strong>of</strong> these <strong>di</strong>splacement values the correspon<strong>di</strong>ng shear forces provided byeach element are evaluated and summed. In this way, a multi-linear storey


318 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> Avellinoshear-<strong>di</strong>splacement relationship is obtained.The illustrated procedure is carried out in both buil<strong>di</strong>ng <strong>di</strong>rections.5.2.4. Calculation <strong>of</strong> pushover curveOnce the interstorey shear-<strong>di</strong>splacement relationship at each storey has beendefined, the base shear-top <strong>di</strong>splacement relationship representing the lateralresponse <strong>of</strong> the Shear Type buil<strong>di</strong>ng model – under a given <strong>di</strong>stribution <strong>of</strong>lateral forces – can be evaluated through a closed-form procedure.First, the fundamental period <strong>of</strong> vibration and the correspon<strong>di</strong>ng lateral<strong>di</strong>splacement shape are evaluated by means <strong>of</strong> an eigenvalue analysis. To thisaim, mass and stiffness matrices <strong>of</strong> the Shear Type model are easilyconstructed; elastic stiffness at each storey is calculated as the ratio betweenforce and <strong>di</strong>splacement values correspon<strong>di</strong>ng to the first point <strong>of</strong> the multilinearenvelope representing the interstorey shear-<strong>di</strong>splacement relationship.Hence, a linear, uniform or 1 st mode lateral <strong>di</strong>splacement shape is chosenand the correspon<strong>di</strong>ng lateral load shape is determined.Once the shape <strong>of</strong> the applied <strong>di</strong>stribution <strong>of</strong> lateral forces is given, theshape <strong>of</strong> the correspon<strong>di</strong>ng <strong>di</strong>stribution <strong>of</strong> interstorey shear demand can bedetermined, too. A normalized <strong>di</strong>stribution <strong>of</strong> interstorey shear demand isassumed and the ratios between such demand forces and the correspon<strong>di</strong>nginterstorey shear strengths (i.e., maximum force values <strong>of</strong> the interstorey shear<strong>di</strong>splacementrelationships) are calculated. Hence, the storey characterized bythe maximum value <strong>of</strong> this ratio will be the first (and only) to reach itsmaximum resistance (with increasing lateral <strong>di</strong>splacement). Hence, if infillelements are present at that storey, lea<strong>di</strong>ng to a degra<strong>di</strong>ng post-peak behaviour<strong>of</strong> the interstorey shear-<strong>di</strong>splacement relationship, that storey will also be thefirst (and only) to start to degrade, thus controlling the s<strong>of</strong>tening behaviour <strong>of</strong>the structural response. Moreover, the peak <strong>of</strong> resistance <strong>of</strong> the pushover curvecan be calculated from the interstorey shear resistance <strong>of</strong> the same storey, basedon the constant ratio between the interstorey shear at that storey and the baseshear. As a matter <strong>of</strong> fact, due to the constant shape <strong>of</strong> the lateral force


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 319the case study <strong>of</strong> Avellino<strong>di</strong>stribution, such a ratio can be calculated at each storey and remains constantat each step <strong>of</strong> the pushover curve.Therefore, the pushover curve can be evaluated by means <strong>of</strong> a forcecontrolledprocedure up to the peak, and by means <strong>of</strong> a <strong>di</strong>splacement-controlledprocedure after the peak. In the latter phase, the evaluation <strong>of</strong> the response isbased on the interstorey shear-<strong>di</strong>splacement relationship <strong>of</strong> the storey where thecollapse mechanism has taken place. At each step, the top <strong>di</strong>splacement iscalculated as the sum <strong>of</strong> the interstorey <strong>di</strong>splacement at each storey, evaluatedas a function <strong>of</strong> the correspon<strong>di</strong>ng interstorey shear demand, whereas the baseshear is given by the sum <strong>of</strong> lateral applied forces. If the storey where thecollapse mechanism takes place is characterized by a s<strong>of</strong>tening post-peakbehaviour, during the post-peak phase in the remaining N-1 storeys (where N isthe number <strong>of</strong> storeys) the interstorey shear will decrease starting from a prepeakpoint <strong>of</strong> the interstorey shear-<strong>di</strong>splacement relationship; hence, thecorrespon<strong>di</strong>ng <strong>di</strong>splacement will decrease, too, following an unloa<strong>di</strong>ng branch.An unloa<strong>di</strong>ng stiffness equal to the elastic stiffness is assumed. Figure 5.2.4.1reports a schematic representation <strong>of</strong> the described procedure.Following this procedure, the pushover curve can be completely determine<strong>di</strong>n both <strong>di</strong>rections.


320 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> AvellinoPushovercurveLateral force<strong>di</strong>stribution∆ topDeformedshapeInterstorey shear<strong>di</strong>stributionInterstoreyshear-<strong>di</strong>splacementrelationshipsV base∆ topV base∆ topV base∆ topV base∆ topV base∆ topV baseFigure 5.2.4.1. Schematic representation <strong>of</strong> pushover analysis procedure on Shear Type models


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 321the case study <strong>of</strong> Avellino5.2.5. <strong>Seismic</strong> assessmentOnce the pushover curve has been determined, a multi- or bi-linearization iscarried out, accor<strong>di</strong>ng to the same procedure illustrated in Section 4.3.1.Figure 5.2.5.1. <strong>Seismic</strong> safety assessment in POST s<strong>of</strong>twareHence, characteristic parameters <strong>of</strong> the equivalent SDOF system aredetermined. The <strong>di</strong>splacement capacity is evaluated for <strong>di</strong>fferent Limit States:Damage Limitation, Severe Damage and Near Collapse. Damage Limitation isdefined as correspon<strong>di</strong>ng to the <strong>di</strong>splacement when the last infill starts todegrade or when yiel<strong>di</strong>ng occurs in the first <strong>RC</strong> column, whereas SevereDamage and Near Collapse respectively correspond to the <strong>di</strong>splacements when0.75×θuandθuoccur in the first <strong>RC</strong> column. Then, based on assigned data(namely site coor<strong>di</strong>nates, soil con<strong>di</strong>tions, reference period and probability <strong>of</strong>exceedance <strong>of</strong> the seismic demand) the elastic demand spectrum is evaluated.Hence, N2 method is applied and the inelastic <strong>di</strong>splacement demand under thisspectrum is calculated through <strong>di</strong>fferent R-µ-T relationships, accor<strong>di</strong>ng to thedegra<strong>di</strong>ng or non-degra<strong>di</strong>ng behaviour <strong>of</strong> the equivalent SDOF system (seeSection 4.3.1). In this way, a seismic safety assessment can be carried out by


322 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> Avellinocalculating the <strong>di</strong>splacement Demand/Capacity ratio for each Limit State.5.2.6. Evaluation <strong>of</strong> fragility curvesThe methodology for the evaluation <strong>of</strong> fragility curves from values <strong>of</strong> PGAcapacity “observed” in a population <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong> has been described in Section4.3.3.2. Nevertheless, in Section 4.3.3.2 a Response Surface Method (RSM) hasbeen applied since it would have been too computationally deman<strong>di</strong>ng to carryout a SPO analysis for each set <strong>of</strong> the sampled Random Variables. On thecontrary, in the described s<strong>of</strong>tware the evaluation <strong>of</strong> a pushover curve(inclu<strong>di</strong>ng the simulated design procedure and the characterization <strong>of</strong> nonlinearresponse) starting from the input data requires a reasonable time (typicallybetween 0.5 and 1.0 seconds on a “standard” Personal Computer). Hence, PGAcapacity (at the three considered Limit States) is explicitly calculated for eachbuil<strong>di</strong>ng <strong>of</strong> the generated population, without using any RSM.This procedure is applied in the described s<strong>of</strong>tware assuming as RandomVariables the same Variables described in Section 4.3.3.1. Moreover, theinelastic <strong>di</strong>splacement demand evaluated from R-µ-T relationships is assumedas Random Variable, too. The estimate <strong>of</strong> the uncertainty in the evaluation <strong>of</strong>the inelastic <strong>di</strong>splacement demand (in a spectral assessment method) derivesfrom the record-to-record variability observed in the results <strong>of</strong> the nonlineardynamic analyses carried out on SDOF systems (with several records) to obtainsuch R-µ-T relationships. Hence, when the inelastic <strong>di</strong>splacement demand istreated as a Random Variable, the value <strong>of</strong> inelastic <strong>di</strong>splacement demandcalculated by means <strong>of</strong> the given R-µ-T relationship is assumed as me<strong>di</strong>anvalue, and the correspon<strong>di</strong>ng variability has to be modelled; in this procedure, aCoefficient <strong>of</strong> Variation (CoV) equal to 0.70 is assumed (Dolšek and Fajfar,2004 – Sections 5 and 9).It is to be noted that in Section 4.3 the uncertainty in inelastic <strong>di</strong>splacementdemand associated with the employed R-µ-T relationships has not beenincluded among considered Random Variables. As a matter <strong>of</strong> fact, thisuncertainty does influence the assessment <strong>of</strong> seismic capacity (mo<strong>di</strong>fying the


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 323the case study <strong>of</strong> Avellinoslope <strong>of</strong> fragility curves) but there was no need to consider this uncertaintywhen carrying out a relative comparison (rather than a proper estimate)between the seismic capacities obtained through <strong>di</strong>fferent models (in particularbetween “exact” and Shear Type models). As a matter <strong>of</strong> fact, this uncertaintywould have affected in the same way the assessment <strong>of</strong> seismic capacity in the<strong>di</strong>fferent considered models, thus not influencing the relative comparisonbetween them. If two mechanical models <strong>of</strong> the same buil<strong>di</strong>ng provide the samecapacity curve then the results provided by a seismic assessments carried outaccor<strong>di</strong>ng to these two models would be equal to each other, the uncertainty ininelastic <strong>di</strong>splacement demand considered or not.It is worth noting that, actually, further parameters may be also consideredas Random Variables, such as the input data for the simulated design procedure,global <strong>di</strong>mensions or buil<strong>di</strong>ng mass. Nevertheless, in the illustrated procedureuncertainty is considered also in seismic assessment, whereas a deterministicknowledge <strong>of</strong> the structural model (i.e., element <strong>di</strong>mensions, reinforcement,etc.) is postulated (Rossetto and Elnashai, 2005; Polese et al., 2008; Verderameet al., 2010a).Once the Random Variables have been defined, their sampling is carried outaccor<strong>di</strong>ng to the Latin Hypercube Sampling (LHS) technique (McKay et al.,1979), adopting the “me<strong>di</strong>an”, “random” or “mean” sampling scheme(Vorechovsky and Novak, 2009). Hence, the number <strong>of</strong> samplings and thesampling scheme have to be defined in this phase.Subsequently, PGA capacity at the three defined Limit States is evaluatedfor each one <strong>of</strong> the generated <strong>buil<strong>di</strong>ngs</strong>. To this aim, the same procedureillustrated in Section 4.3.1 is applied. First, the “ductility capacity” on theequivalent SDOF system is evaluated, correspon<strong>di</strong>ng to the <strong>di</strong>splacement forwhich that Limit State is exceeded. Hence, the R-µ-T relationship is “backapplied”,calculating the R value correspon<strong>di</strong>ng to the determined ductilitycapacity, the period <strong>of</strong> the equivalent SDOF system T already evaluated. Then,the elastic spectral acceleration is obtained as the product between R and theacceleration capacity (C s,max ) <strong>of</strong> the equivalent SDOF system. Given the elastic


324 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> Avellinospectral acceleration at a certain period, the correspon<strong>di</strong>ng PGA is univocallydetermined, based on the demand spectra defined in (INGV-DPC S1, 2007)(also extrapolating seismic intensity parameters out <strong>of</strong> the given range, ifnecessary). As already highlighted in Section 4.3.1, a double iterative procedureis required to evaluate the PGA capacity since (i) the spectral shape changeswith the seismic intensity and (ii) some parameters are input parameters for theR-µ-T relationship but also depends on the results obtained from thisrelationship. In this procedure, assigned stratigraphic and topographiccon<strong>di</strong>tions are considered; hence, the obtained value <strong>of</strong> PGA capacity alreadyaccounts for these con<strong>di</strong>tions. In other words, capacity is expressed in terms <strong>of</strong>PGA on horizontal stiff soil.Once this procedure has been carried out for all the generated <strong>buil<strong>di</strong>ngs</strong>, thefragility curve is obtained as cumulative frequency <strong>di</strong>stribution <strong>of</strong> the PGAcapacity, for the three considered Limit States and in both <strong>di</strong>rections.Figure 5.2.6.1. Evaluation <strong>of</strong> fragility curves in POST s<strong>of</strong>tware


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 325the case study <strong>of</strong> Avellino5.2.7. Calculation <strong>of</strong> failure probabilityThe failure probability (P f ) <strong>of</strong> a structural system characterized by aresistance R under a seismic load S can be evaluated as+∞P = ∫ f S F S dS(5.2.7.1)( ) ( )f S R0where f ( )SS is the Probability Density Function (PDF) <strong>of</strong> the seismic intensityparameter and F ( )RS is the probability that the resistance R is lower than alevel S <strong>of</strong> seismic intensity. Hence, F ( )RS is represented by a fragility curve(see Section 4.3.3.2), whereas the PDF <strong>of</strong> the seismic intensity S – in a giventime window – is obtained from seismic hazard stu<strong>di</strong>es.In particular, based on the seismic hazard data provided in (INGV-DPC S1,2007) for the Italian territory, if the coor<strong>di</strong>nates <strong>of</strong> the site <strong>of</strong> interest are given,PGA values correspon<strong>di</strong>ng to <strong>di</strong>fferent return periods (T R ) can be determined.Hence, given a PGA value, the correspon<strong>di</strong>ng T R (PGA) can be calculated.Finally, given a time window (V R ), the excee<strong>di</strong>ng probability <strong>of</strong> the same PGAis given by the Poisson process:VR( )P PGA 1 e −VRTR( PGA)= − (5.2.7.2)In the procedure described herein, PGA is assumed as seismic intensityparameter S, F ( )RS is represented by the calculated fragility curves (assuminga linear interpolation between subsequent values <strong>of</strong> PGA) and f ( )represented by PV R( PGA ) .SS isHence, the failure probability Pfis calculated through Eq. 5.2.7.1, by means<strong>of</strong> a numerical integration based on Simpson quadrature.Pfis calculated (for the assigned time window V R ) for the three consideredLimit States and in both <strong>di</strong>rections.


326 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> Avellino5.2.8 Example applicationsIn this Section, the procedure described in detail in Section 5.2 is applied to<strong>di</strong>fferent case study buil<strong>di</strong>ng, varying main parameters such as the number <strong>of</strong>storeys, the surface area, the infill configuration and the age <strong>of</strong> construction, thelatter through material characteristics and type <strong>of</strong> design (gravitational orseismic). Hence, seismic safety assessment for a given seismic intensity andevaluation <strong>of</strong> fragility curves is carried out.First, seismic capacities <strong>of</strong> an Uniformly infilled frame are evaluatedconsidering <strong>di</strong>fferent numbers <strong>of</strong> storeys (3, 5 and 7) and two <strong>di</strong>fferentsimulated design procedures: for gravity loads only and for gravity and seismicloads. In the latter case, a base shear coefficient (i.e., ratio between design baseshear and buil<strong>di</strong>ng weight) equal to 0.10 is assumed. The buil<strong>di</strong>ng has five baysin longitu<strong>di</strong>nal <strong>di</strong>rection and three bays in transversal <strong>di</strong>rection. Interstoreyheight is equal to 3.0 m (at all storeys, inclu<strong>di</strong>ng the first one) and bay length isequal to 4.5 m.Infill panels are assumed to be 20 cm thick, with the followingcharacteristics: shear elastic modulus equal to 1240 MPa, Young’s elasticmodulus equal to (10/3×1240) MPa and shear cracking stress equal to 0.33MPa (see Section 4.3.1). Parameters α and β (see Section 5.2.1) are given equalto 0.03 and 0.01, respectively.A concrete compressive strength f c =25 MPa is assumed (Verderame et al.,2001). In simulated design procedure, the cubic compressive strength for theconcrete is assumed equal to 25 MPa, thus lea<strong>di</strong>ng (RDL 2229/1939, DM3/3/1975) to an allowable concrete compressive stress equal to 6.0 and 8.5 MPafor axial load and axial load combined with ben<strong>di</strong>ng, respectively. In order todetermine column <strong>di</strong>mensions, the allowable stress <strong>of</strong> concrete for axial load ismultiplied by a coefficient equal to 0.7 in seismic design, whereas it is notreduced in gravity load design.The reinforcement is assumed as smooth; hence, no reduction for the lack <strong>of</strong>seismic detailing is applied, see Section 2.2.2. Steel yield strength f y is assumedequal to 369.7 MPa and to 426.9 MPa for the gravity load designed and the


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 327the case study <strong>of</strong> Avellinoseismic load designed buil<strong>di</strong>ng, representing Aq50 and FeB32 steel typologies,the most widely spread in Italy during 1960s and 1970s, respectively(Verderame et al., 2010b). In simulated design procedure, allowable stress forsteel is assumed equal to 160 MPa for both typologies (Circolare 1472, 1957;DM 30/5/1972).As far as seismic input is concerned, soil type C and 2 nd topographiccategory are assumed (DM 14/1/2008).<strong>Seismic</strong> safety assessment is carried with an input elastic spectrumcorrespon<strong>di</strong>ng to a 5 % probability <strong>of</strong> exceedance in a time window <strong>of</strong> 50 years.For the sake <strong>of</strong> brevity, only results in transversal <strong>di</strong>rection are reported.Uniformly infilled frameMain equivalent parameters <strong>of</strong> the equivalent SDOF systems are reported inTable 5.2.8.1. As expected, an increase in T eff with the number <strong>of</strong> storeys isobserved; nevertheless, due to the considerable contribution <strong>of</strong> infills (whosecharacteristics are equal for all the analyzed <strong>buil<strong>di</strong>ngs</strong>) both in terms <strong>of</strong> stiffnessand strength, T eff values <strong>of</strong> Gravity Load Designed (GLD) and <strong>Seismic</strong> LoadDesigned (SLD) <strong>buil<strong>di</strong>ngs</strong> are quite closer.For both GLD and SLD <strong>buil<strong>di</strong>ngs</strong> the storey collapse takes place at the 1 ststorey for 3- and 5-storey <strong>buil<strong>di</strong>ngs</strong> and at the 2 nd storey for 7-storey <strong>buil<strong>di</strong>ngs</strong>.The base shear strength <strong>of</strong> the <strong>RC</strong> frame alone can be observed looking atthe residual base shear C s,min , correspon<strong>di</strong>ng to the range <strong>of</strong> behaviour wheninfills are failed, thus practically not contributing to the lateral strength <strong>of</strong> thebuil<strong>di</strong>ng (infill residual resistance is assumed equal to 1 % <strong>of</strong> the maximumresistance). First, it is to be noted that C s,min in SLD <strong>buil<strong>di</strong>ngs</strong> is more than 2times higher than the base shear coefficient used in simulated design (= 0.10).This considerable overstrength, compared with the design prescription, ismainly due to the <strong>di</strong>fference between the material strength values used in designand in assessment (e.g., between the steel allowable stress σ s,adm = 160 MPaused in simulated design procedure and the me<strong>di</strong>an value <strong>of</strong> steel yield strengthf y = 426.9 MPa used in capacity assessment), but also to the conservatism in


328 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> Avellinodesign (e.g., the upper approximation used when determining the number and<strong>di</strong>ameter <strong>of</strong> bars correspon<strong>di</strong>ng to a certain amount <strong>of</strong> longitu<strong>di</strong>nalreinforcement). The importance in the use <strong>of</strong> a simulated design procedure alsolies in the capability to account for such effects, which, for instance, can bemodelled only very approximately (e.g., Giovinazzi, 2005), or are not modelledat all (e.g., Grant et al., 2006), when code prescription-based methods are usedto assess the seismic capacity <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>.As expected, C s,min in GLD <strong>buil<strong>di</strong>ngs</strong> is quite lower compared with the SLD<strong>buil<strong>di</strong>ngs</strong>. For this kind <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong>, which have not been designed to resistseismic forces, a simulated design procedure may be considered as the mosteffective and reliable alternative to evaluate their seismic capacity.As far as C s,max is concerned, it is observed how this coefficient decreaseswith the number <strong>of</strong> storeys. This was an expected result since, with the number<strong>of</strong> storeys increasing, the base shear strength <strong>of</strong> the buil<strong>di</strong>ng (not normalized toits effective mass) increases, whereas the contribution <strong>of</strong> infills to lateralstrength remains constant since, obviously, the characteristics <strong>of</strong> these elementsdo not change with the increasing height, opposite to <strong>RC</strong> column elements (inlower storeys) that show an increasing lateral strength. This is true both in SLD<strong>buil<strong>di</strong>ngs</strong> (where the increase in the strength <strong>of</strong> <strong>RC</strong> elements is clearly due tothe increase in the design shear demand with increasing mass) and in GLD<strong>buil<strong>di</strong>ngs</strong>, where, although not designed to resist any lateral load, <strong>RC</strong> columnsat lower storeys show an increase in section <strong>di</strong>mensions with the number <strong>of</strong>storeys, due to the increasing design axial load. Hence, given a certain amount<strong>of</strong> minimum prescribed longitu<strong>di</strong>nal reinforcement ratio, these elements alsoshow an increase in lateral strength.Hence, the specific contribution <strong>of</strong> infills to the overall lateral strengthdecreases (e.g., Far<strong>di</strong>s and Panagiotakos, 1997), thus lea<strong>di</strong>ng to a lower C s,max .The change in collapsed storey (from 1 st to 2 nd one for 7-storey <strong>buil<strong>di</strong>ngs</strong>)may also be explained accor<strong>di</strong>ng to this phenomenon <strong>of</strong> relative decrease ininfill contribution to the lateral strength (see Section 4.3.2.1).The increase in T eff and the decrease in C s,max are the main reasons for the


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 329the case study <strong>of</strong> Avellinodecrease in seismic capacity with the number <strong>of</strong> storeys, observed in bothbuil<strong>di</strong>ng typologies and for all the considered Limit States, see Table 5.2.8.2.As far as <strong>di</strong>splacement Demand to Capacity ratios for the assigned seismicinput are concerned, similar trends are observed, see Table 5.2.8.3.Nevertheless, at DL Limit State in GLD <strong>buil<strong>di</strong>ngs</strong> a decrease in this ratio isobserved with the number <strong>of</strong> storeys, thus interestingly highlighting how<strong>di</strong>fferent approaches to the evaluation <strong>of</strong> the Demand to Capacity ratio (e.g.,based on PGA rather than <strong>di</strong>splacement values) may yield slightly <strong>di</strong>fferentresults.ΓT eff C s,max C s,minTΓeff C s,max C s,min[sec] [g] [g][sec] [g] [g]N=3 1.22 0.15 0.53 0.14 1.22 0.15 0.56 0.24N=5 1.25 0.24 0.38 0.17 1.26 0.24 0.43 0.28N=7 1.27 0.31 0.31 0.17 1.28 0.34 0.39 0.28GLDSLDTable 5.2.8.1. Main equivalent SDOF parameters (Uniformly infilled <strong>buil<strong>di</strong>ngs</strong> – X <strong>di</strong>rection)DL SD CO DL SD CON=3 0.18 0.36 0.45 0.19 0.56 0.64N=5 0.13 0.32 0.40 0.13 0.46 0.53N=7 0.12 0.28 0.35 0.11 0.38 0.48GLDSLDTable 5.2.8.2. PGA capacities (expressed in g) (Uniformly infilled <strong>buil<strong>di</strong>ngs</strong> – X <strong>di</strong>rection)DL SD CO DL SD CON=3 5.17 0.42 0.32 1.84 0.17 0.13N=5 4.15 0.69 0.53 3.02 0.48 0.37N=7 3.66 0.86 0.67 3.40 0.62 0.50GLDSLDTable 5.2.8.3. Displacement Demand to Capacity ratios for a seismic input characterized by a5% probability <strong>of</strong> exceedance in 50 years (Uniformly infilled <strong>buil<strong>di</strong>ngs</strong> – X <strong>di</strong>rection)


330 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> AvellinoN=310.90.80.70.60.50.4capacity curveidealized capacity curveelastic demand spectruminelastic demand spectrumdemandDL capacitySD capacityCO capacity10.90.80.70.60.50.40.30.20.10.30.20.100 50 100 150 200 250 300 35000 50 100 150 200 250 300 35010.90.80.70.610.90.80.70.6N=50.50.40.50.40.30.20.100 50 100 150 200 250 300 3500.30.20.100 50 100 150 200 250 300 35010.90.80.70.610.90.80.70.6N=70.50.40.50.40.30.20.100 50 100 150 200 250 300 3500.30.20.100 50 100 150 200 250 300 350GLDSLDFigure 5.2.8.1. <strong>Seismic</strong> assessment for a seismic input characterized by a 5% probability <strong>of</strong>exceedance in 50 years (PGA = 0.2495 g) (Uniformly infilled <strong>buil<strong>di</strong>ngs</strong> – X <strong>di</strong>rection)


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 331the case study <strong>of</strong> AvellinoBy means <strong>of</strong> the described s<strong>of</strong>tware, fragility curves can be obtained too(see Section 5.2.6). In the following, such results are shown for curvesevaluated with 100 samplings <strong>of</strong> the considered Random Variables, see Figure5.2.8.2.Failure probabilities in 50 years are also calculated, showing the increase in<strong>vulnerability</strong> with the number <strong>of</strong> storeys and, as expected, the higher<strong>vulnerability</strong> <strong>of</strong> GLD <strong>buil<strong>di</strong>ngs</strong> compared with SLD <strong>buil<strong>di</strong>ngs</strong>.Nevertheless, the <strong>di</strong>fferences between these two buil<strong>di</strong>ng typologies aresignificantly lower at DL Limit State, compared with SD or NC. As a matter <strong>of</strong>fact, at DL Limit State the infill contribution has a relatively higher weight (seeSection 4.3.2.1), thus reducing the <strong>di</strong>fferences between <strong>vulnerability</strong> <strong>of</strong> GLDand SLD <strong>buil<strong>di</strong>ngs</strong>.DL SD CO DL SD CON=3 0.0129 0.0030 0.0023 0.0106 0.0014 0.0001N=5 0.0209 0.0050 0.0037 0.0189 0.0028 0.0019N=7 0.0247 0.0064 0.0047 0.0247 0.0043 0.0032GLDSLDTable 5.2.8.4. Failure probabilities in 50 years (Uniformly infilled <strong>buil<strong>di</strong>ngs</strong> – X <strong>di</strong>rection)


332 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> Avellino10.90.80.70.610.90.80.70.6N=3P f0.50.4P f0.50.40.30.2DL0.1SDNC00 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8PGA [g]0.30.20.100 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8PGA [g]10.90.80.70.610.90.80.70.6N=5P f0.50.4P f0.50.40.30.20.100 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8PGA [g]0.30.20.100 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8PGA [g]10.90.80.70.610.90.80.70.6N=7P f0.50.4P f0.50.40.30.20.10.30.20.100 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8PGA [g]00 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8PGA [g]GLDSLDFigure 5.2.8.2. Fragility curves (Uniformly infilled <strong>buil<strong>di</strong>ngs</strong> – X <strong>di</strong>rection)


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 333the case study <strong>of</strong> AvellinoPilotis frameThe same analyses are now carried out on Pilotis <strong>buil<strong>di</strong>ngs</strong>, in order toinvestigate the influence <strong>of</strong> a <strong>di</strong>fferent arrangement <strong>of</strong> infill elements on theseismic capacity. As expected, in all cases the collapse mechanism takes placein the bottom bare storey. Hence, the lateral response <strong>of</strong> the buil<strong>di</strong>ng may be<strong>di</strong>rectly interpreted based on the behaviour <strong>of</strong> 1 st storey <strong>RC</strong> columns.From a qualitative standpoint, two opposite effects influence the effectiveperiod T eff , counterbalancing each other.On a side, <strong>of</strong> course, the effective mass increases with the number <strong>of</strong>storeys; in Pilotis <strong>buil<strong>di</strong>ngs</strong>, due to peculiar stiffness <strong>di</strong>stribution, the modalparticipation factor is closer to 1 (and the effective mass is closer to the totalbuil<strong>di</strong>ng mass) compared with other buil<strong>di</strong>ng typologies. Nevertheless, thiseffect is much more pronounced for lower number <strong>of</strong> storeys, when the<strong>di</strong>mension <strong>of</strong> <strong>RC</strong> columns is smaller and, hence, the presence <strong>of</strong> infills in upperstoreys has a relatively higher weight in the lateral stiffness <strong>di</strong>stribution,compared with <strong>buil<strong>di</strong>ngs</strong> with higher number <strong>of</strong> storeys. Hence, effective massincreases approximately less than linearly with the number <strong>of</strong> storeys.On the other side, with increasing number <strong>of</strong> storeys the strength and thestiffness <strong>of</strong> 1 st storey <strong>RC</strong> columns increase too. In SLD <strong>buil<strong>di</strong>ngs</strong>, this is<strong>di</strong>rectly related to the design seismic shear demand in these elements, whichincreases linearly with the number <strong>of</strong> storeys, thus lea<strong>di</strong>ng to an approximatelylinear increase <strong>of</strong> the base shear strength (except for design approximations). InGLD <strong>buil<strong>di</strong>ngs</strong>, the interpretation <strong>of</strong> the increase in strength and the stiffness <strong>of</strong>1 st storey <strong>RC</strong> columns is not so straightforward; however, column section areadepends on the design axial load, which increases linearly with the number <strong>of</strong>storeys. As column section area increases, stiffness and strength increase too,obviously.On the whole, the latter effect tends to prevail on the former, thus lea<strong>di</strong>ng toa decrease in T eff with the number <strong>of</strong> storeys.Nevertheless, the <strong>di</strong>splacement capacity <strong>of</strong> 1 st storey columns also decreaseswith the number <strong>of</strong> storeys.


334 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> AvellinoFinally, the sum <strong>of</strong> these effects leads to a not clear tendency <strong>of</strong> seismiccapacity with the number <strong>of</strong> storeys, for both buil<strong>di</strong>ng typologies, whereas if arelative comparison is carried out between <strong>di</strong>fferent buil<strong>di</strong>ng typologies, thehigher strength and stiffness shown by SLD <strong>buil<strong>di</strong>ngs</strong> clearly leads to higherseismic capacities, as expected.T effΓC s,maxTΓeff C s,max[sec] [g][sec] [g]N=3 1.02 0.67 0.13 1.04 0.57 0.22N=5 1.09 0.59 0.15 1.14 0.48 0.24N=7 1.17 0.53 0.18 1.24 0.43 0.26GLDSLDTable 5.2.8.5. Main equivalent SDOF parameters (Pilotis <strong>buil<strong>di</strong>ngs</strong> – X <strong>di</strong>rection)DL SD CO DL SD CON=3 0.06 0.29 0.42 0.07 0.32 0.48N=5 0.06 0.26 0.36 0.07 0.32 0.48N=7 0.06 0.25 0.35 0.08 0.33 0.48GLDSLDTable 5.2.8.6. PGA capacities (expressed in g) (Pilotis <strong>buil<strong>di</strong>ngs</strong> – X <strong>di</strong>rection)DL SD CO DL SD CON=3 4.20 0.88 0.66 3.74 0.80 0.60N=5 4.76 0.98 0.73 3.80 0.79 0.60N=7 4.58 0.99 0.74 3.50 0.78 0.59GLDSLDTable 5.2.8.7. Displacement Demand to Capacity ratios for a seismic input characterized by a5% probability <strong>of</strong> exceedance in 50 years (Pilotis <strong>buil<strong>di</strong>ngs</strong> – X <strong>di</strong>rection)


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 335the case study <strong>of</strong> AvellinoN=310.90.80.70.60.50.4capacity curveidealized capacity curveelastic demand spectruminelastic demand spectrumdemandDL capacitySD capacityCO capacity10.90.80.70.60.50.40.30.20.10.30.20.100 50 100 150 200 250 300 35000 50 100 150 200 250 300 35010.90.80.70.610.90.80.70.6N=50.50.40.50.40.30.20.100 50 100 150 200 250 300 3500.30.20.100 50 100 150 200 250 300 35010.90.80.70.610.90.80.70.6N=70.50.40.50.40.30.20.100 50 100 150 200 250 300 3500.30.20.100 50 100 150 200 250 300 350GLDSLDFigure 5.2.8.3. <strong>Seismic</strong> assessment for a seismic input characterized by a 5% probability <strong>of</strong>exceedance in 50 years (PGA = 0.2495 g) (Pilotis <strong>buil<strong>di</strong>ngs</strong> – X <strong>di</strong>rection)


336 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> AvellinoFragility curves and the correspon<strong>di</strong>ng failure probabilities are evaluatedalso for Pilots <strong>buil<strong>di</strong>ngs</strong>. Again, seismic performance do not changesignificantly with the number <strong>of</strong> storeys, whereas the failure probability <strong>of</strong> SLD<strong>buil<strong>di</strong>ngs</strong> is systematically lower compared with GLD <strong>buil<strong>di</strong>ngs</strong>. Mostimportantly, a clear increase in failure probability, compared with thepreviously illustrated Uniformly infilled typology, is shown. As expected, thedetrimental effects <strong>of</strong> such an irregular infill <strong>di</strong>stribution can be <strong>di</strong>rectlyobserved, for all the considered Limit States, in terms <strong>of</strong> failure probability.DL SD CO DL SD CON=3 0.0456 0.0100 0.0065 0.0414 0.0093 0.0060N=5 0.0494 0.0113 0.0073 0.0418 0.0086 0.0056N=7 0.0480 0.0113 0.0076 0.0380 0.0077 0.0049GLDSLDTable 5.2.8.8. Failure probabilities in 50 years (Pilotis <strong>buil<strong>di</strong>ngs</strong> – X <strong>di</strong>rection)


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 337the case study <strong>of</strong> Avellino10.90.80.70.610.90.80.70.6N=3P f0.50.4P f0.50.40.30.2DL0.1SDNC00 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8PGA [g]0.30.20.100 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8PGA [g]10.90.80.70.610.90.80.70.6N=5P f0.50.4P f0.50.40.30.20.100 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8PGA [g]0.30.20.100 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8PGA [g]10.90.80.70.610.90.80.70.6N=7P f0.50.4P f0.50.40.30.20.10.30.20.100 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8PGA [g]00 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8PGA [g]GLDSLDFigure 5.2.8.4. Fragility curves (Uniformly infilled <strong>buil<strong>di</strong>ngs</strong> – X <strong>di</strong>rection)


338 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> Avellino5.3 URBAN SCALE VULNERABILITY ASSESSMENT: THE CASESTUDY OF AVELLINOAvellino is a city <strong>of</strong> the Campania region, in southern Italy, with more than55.000 people. It is in a high seismic area, and it was struck by the catastrophicIrpinia earthquake (M w = 6.9) on November 23 rd , 1980.The Italian Ministry <strong>of</strong> Education, University and Research has funded the“SIMURAI – Strumenti Integrati per il MUlti Risk Assessment territoriale inambienti urbani antropizzatI” (Integrated instruments for large scale multi riskassessment in urban anthropic environment) research project aimed at carryingout a case study multi risk assessment at urban scale on the Avellino city. As faras the seismic risk is concerned, buil<strong>di</strong>ng stock data have been collectedthrough a detailed field survey, aimed at a large scale <strong>vulnerability</strong> assessment.In this Section, this field survey will be described first, from the preparation <strong>of</strong>the survey form to the analysis <strong>of</strong> collected data (Section 5.3.1). Then, thepreviously illustrated simplified approach to the seismic <strong>vulnerability</strong>assessment <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> (see Section 5.2) will be applied to such data.Results will be illustrated in Section 5.3.2, showing the trend <strong>of</strong> estimatedfailure probability, at <strong>di</strong>fferent performance levels, among the analyzed buil<strong>di</strong>ngpopulation.5.3.1 Data collection and field survey resultsIn this Section, the form prepared to carry out the field survey on <strong>buil<strong>di</strong>ngs</strong>tock is presented first. Hence, the analysis <strong>of</strong> collected data is presented,particularly focused on <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>.5.3.1.1 Survey formPrepared survey form (Figures 5.3.1.7 to 5.3.1.10) was sub-<strong>di</strong>vided in<strong>di</strong>fferent sections:


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 339the case study <strong>of</strong> Avellino- Section 1 – Buil<strong>di</strong>ng identificationIn this section, data for the identification <strong>of</strong> the buil<strong>di</strong>ng were reported,consisting <strong>of</strong> the address, the assigned ID code and data concerning theexecution <strong>of</strong> the survey, i.e. the date and the survey team (each survey teamwas made up <strong>of</strong> two or three persons) and also the ID code <strong>of</strong> thephotographic image taken during the survey. In preparation <strong>of</strong> the survey, anID was assigned to each buil<strong>di</strong>ng identified through aerial photographs.Moreover, the survey was planned based on “census cells” determinedaccor<strong>di</strong>ng to ISTAT (Istituto Nazionale <strong>di</strong> Statistica, National Institute <strong>of</strong>Statistics) data. Census cells are the basic territory units considered byISTAT when carrying out a census survey. Figure 5.3.1.1 reports a detail <strong>of</strong>an aerial view where census cells are delimited by coloured lines and IDspre-assigned to each buil<strong>di</strong>ng shape are reported.Figure 5.3.1.1. Census cells and buil<strong>di</strong>ng IDsMoreover, the buil<strong>di</strong>ng position was identified as “isolated” or“adjacent” to other <strong>buil<strong>di</strong>ngs</strong>. In the latter case, the position <strong>of</strong> the buil<strong>di</strong>ngwith respect to the adjacent ones was reported (namely as internal, external


340 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> Avellinoor corner). It is to be noted that in many cases a single ID had been preassignedto a single “shape” that, actually, was composed <strong>of</strong> <strong>di</strong>fferentadjacent <strong>buil<strong>di</strong>ngs</strong>. In these cases, <strong>di</strong>fferent structural units were “generated”from a single pre-identified buil<strong>di</strong>ng (see Figures 5.3.1.2 and 5.3.1.3).Figure 5.3.1.2. Aerial view <strong>of</strong> a group <strong>of</strong> adjacent <strong>buil<strong>di</strong>ngs</strong> (Virtual Earth©)Figure 5.3.1.3. Ground detail view <strong>of</strong> the <strong>buil<strong>di</strong>ngs</strong> reported in Figure 5.3.1.2: separationbetween single structural units is highlighted with the red dashed lineA schematic representation <strong>of</strong> buil<strong>di</strong>ng plan view with the measured<strong>di</strong>mensions was reported, too.


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 341the case study <strong>of</strong> Avellino- Section 2 – Buil<strong>di</strong>ng descriptionIn section 2 main data necessary for describing the buil<strong>di</strong>ng werereported, i.e. the number <strong>of</strong> storeys (above and below the ground level), theaverage surface area, the age <strong>of</strong> construction and the main destination use.The latter may represent an useful data in view <strong>of</strong> a loos estimationprocedure.- Section 3 – Buil<strong>di</strong>ng morphologySection 3 reported a detailed representation <strong>of</strong> morphologic buil<strong>di</strong>ngcharacteristics. Hence, the plan shape was identified first, referring to sixmain typologies (see Figure 5.3.1.4).(a)(b)(c)(d)Figure 5.3.1.4. Aerial view <strong>of</strong> example L- (a), T- (b), C- (c) or sawtooth- (d) shaped <strong>buil<strong>di</strong>ngs</strong>(Virtual Earth©)


342 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> AvellinoThen, height <strong>di</strong>mensions were reported, also considering the possiblepresence <strong>of</strong> a mansard storey, the partial height above the ground level <strong>of</strong>the storey placed below the ground level (if present) and a possible<strong>di</strong>fference between the 1 st storey height and the upper storey height, <strong>of</strong>tendue to architectonic or functionality requirements. Finally, data about theregularity in elevation were reported, inclu<strong>di</strong>ng the number <strong>of</strong> storeyscharacterized by a reduction in surface area (if present), see Figure 5.3.1.5,and the ground slope.H 1H maxH maxH minFigure 5.3.1.5. Irregularity in elevation characterized by a decrease in surface area (see section4 <strong>of</strong> the survey form, Figure 5.3.1.9)- Section 4 – Structural typologySection 4 reported the identification <strong>of</strong> the structural typology, namelyreinforced concrete, masonry, steel or mixed typology. In the case <strong>of</strong>reinforced concrete, a further in<strong>di</strong>cation was provided, aimed at identifyingthe specific structural system, i.e. frame, shear wall or dual system.- Section 5 – InfillsSection 5 collected data about infill <strong>di</strong>stribution. In particular, thearrangement <strong>of</strong> infill panels at the bottom storey was described by reportingthe type <strong>of</strong> <strong>di</strong>stribution – regular infilling (infill panels present in each bay,see Figure 5.3.1.6a), irregular infilling (infill panels present only in a


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 343the case study <strong>of</strong> Avellinospecified proportion <strong>of</strong> the side length), pilotis (no infill panel, see Figure5.3.1.6b) or partial infilling (infill panels with a height lower than the height<strong>of</strong> adjacent columns) – and the respective number <strong>of</strong> sides characterized bysuch type <strong>of</strong> <strong>di</strong>stribution. Infill typology was also reported. In particular,survey teams had to identify the type <strong>of</strong> material (i.e., hollow clay, solidclay, tuff or concrete bricks) and the number <strong>of</strong> layers composing the infillpanels (one or two). Nevertheless, these characteristics <strong>of</strong>ten were not easyat all to be determined, for instance, due to the presence <strong>of</strong> the plaster.(a)(b)Figure 5.3.1.6. Examples <strong>of</strong> regular (a) and pilotis (b) infill <strong>di</strong>stributions- Section 6 – BaysIn section 6 the number <strong>of</strong> bays per each side (accor<strong>di</strong>ng to the planshape) was reported.- Section 7 – Stairs presence and positionSection 7 reported the number and the position (central or lateral) <strong>of</strong>staircases per each side <strong>of</strong> the buil<strong>di</strong>ng.


344 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> AvellinoFigure 5.3.1.7. Field survey form (1/4)


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 345the case study <strong>of</strong> AvellinoFigure 5.3.1.8. Field survey form (2/4)


346 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> AvellinoFigure 5.3.1.9. Field survey form (3/4)


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 347the case study <strong>of</strong> AvellinoFigure 5.3.1.10. Field survey form (4/4)It is to be noted that some <strong>of</strong> the illustrated sections (e.g., infill description)specifically fit reinforced concrete structural typology.The illustrated survey form includes the main parameters – among the onesthat can be reasonably collected during a field survey – that may have asignificant influence on buil<strong>di</strong>ng seismic capacity, addressing a particularattention to specific potential sources <strong>of</strong> seismic <strong>vulnerability</strong>. Some <strong>of</strong> theseparameters may not have a <strong>di</strong>rect and imme<strong>di</strong>ate usefulness for the firstassessment procedures carried out. Nevertheless, based on damage observationfrom past earthquakes and also on engineering judgement, the importance <strong>of</strong>collecting information about all the above described parameters wasrecognized, also considering the precious opportunity represented by such afield survey campaign.5.3.1.2 Analysis <strong>of</strong> buil<strong>di</strong>ng stock dataIn the following, main collected data about buil<strong>di</strong>ng stock characteristics areillustrated.On the whole, 1327 <strong>buil<strong>di</strong>ngs</strong> were surveyed. Among these, 1058 were <strong>RC</strong><strong>buil<strong>di</strong>ngs</strong> and 265 were masonry <strong>buil<strong>di</strong>ngs</strong>. Steel and mixed <strong>buil<strong>di</strong>ngs</strong> werepresent in negligible percentages (only 4 <strong>buil<strong>di</strong>ngs</strong> out <strong>of</strong> 1327), see Figure5.3.1.11.


348 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> Avellino90%80%70%60%50%40%30%20%10%0%<strong>RC</strong> Masonry Steel MixedFigure 5.3.1.11. Structural typology <strong>of</strong> surveyed <strong>buil<strong>di</strong>ngs</strong>As far as the age <strong>of</strong> construction is concerned, in 254 <strong>buil<strong>di</strong>ngs</strong> (almost 20%<strong>of</strong> the population) it was not determined. However, it is clearly observed how alarge part <strong>of</strong> masonry buil<strong>di</strong>ng stock was constructed at the beginning <strong>of</strong> the20 th century or before, or early after World War II, see Figure 5.3.1.12. Theperiod characterized by the highest growth <strong>of</strong> <strong>RC</strong> buil<strong>di</strong>ng stock is around1970s and 1980s, see Figure 5.3.1.13. It is noted that a quite large part <strong>of</strong> the<strong>RC</strong> buil<strong>di</strong>ng stock was constructed after the 1980 earthquake. Pre- and post-82<strong>buil<strong>di</strong>ngs</strong> respectively represent about the 56 and 44 % <strong>of</strong> the <strong>RC</strong> buil<strong>di</strong>ngpopulation whose age <strong>of</strong> construction was determined.50%40%30%20%10%0%pre-191919-4546-6162-7172-8182-9192-9798-01post-2002Figure 5.3.1.12. Age <strong>of</strong> construction <strong>of</strong> masonry <strong>buil<strong>di</strong>ngs</strong>nr


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 349the case study <strong>of</strong> Avellino50%40%30%20%10%0%pre-191919-4546-6162-7172-8182-9192-9798-01post-2002Figure 5.3.1.13. Age <strong>of</strong> construction <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>nrThe spatial <strong>di</strong>stribution <strong>of</strong> the age <strong>of</strong> construction <strong>of</strong> surveyed <strong>buil<strong>di</strong>ngs</strong> isreported in Figure 5.3.1.14: the presence <strong>of</strong> rather homogeneous areas isobserved; in particular, pre-1919 masonry <strong>buil<strong>di</strong>ngs</strong> are concentrated in thecentral-eastern area correspon<strong>di</strong>ng to the old centre <strong>of</strong> the city, whereas 1960sand 1970s <strong>buil<strong>di</strong>ngs</strong> are mainly located along East-West axis and in Northernarea, respectively. More recent <strong>buil<strong>di</strong>ngs</strong> are present also in the central cityarea, due to post-1980 earthquake reconstruction; this is shown in Figure5.3.1.15, where pre- and post-1981 <strong>buil<strong>di</strong>ngs</strong> are reported.


350 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> AvellinoFigure 5.3.2.14. Age <strong>of</strong> construction <strong>of</strong> surveyed <strong>buil<strong>di</strong>ngs</strong>pre-19191919-451946-611962-711972-811982-911992-971998-2001post-2002ns


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 351the case study <strong>of</strong> AvellinoFigure 5.3.2.15. Pre- and post-1981 surveyed <strong>buil<strong>di</strong>ngs</strong>pre-1981post-1981ns


352 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> Avellino70%60%50%40%30%20%10%0%RectangularL-shapedT-shapedC-shapedZ-shapedFigure 5.3.1.16. Plan morphology <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>sawtooth-shapedIf data about buil<strong>di</strong>ng morphology <strong>of</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> are observed, see Figure5.3.1.16, it can be noted that the Rectangular <strong>buil<strong>di</strong>ngs</strong>, in the number <strong>of</strong> 693,represent about 67% <strong>of</strong> the entire <strong>RC</strong> buil<strong>di</strong>ng stock. In Section 6.3 theproposed simplified methodology for seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>RC</strong><strong>buil<strong>di</strong>ngs</strong> (see Chapter V) will be applied to this group <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong>; hence,further data analyses will be focused on this typology.


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 353the case study <strong>of</strong> Avellino10%9%8%


354 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> Avellino30%25%20%15%10%5%0%Lx/Ly>4.5Figure 5.3.1.18. Ratio between plan <strong>di</strong>mensions <strong>of</strong> rectangular <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>Bay length (see Figure 5.3.1.19) essentially ranges between 3 and 6.5 m, andthe most common values are around 3.5 ÷ 5.5 m.30%25%20%15%10%5%0%lb>7Figure 5.3.1.19. Bay length in rectangular <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>Interstorey height at 1 st storey, as expected, is characterized by highervalues, on average, and also by a higher <strong>di</strong>spersion compared with upperstoreys, see Figure 5.3.1.20 and 5.3.1.21. In particular, in large part <strong>of</strong> thesurveyed <strong>buil<strong>di</strong>ngs</strong> the interstorey height at upper storeys is between 3 and 3.5m.


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 355the case study <strong>of</strong> Avellino90%80%70%60%50%40%30%20%10%0%h1


356 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> Avellinopercentage corresponds to Pilotis <strong>buil<strong>di</strong>ngs</strong>.25%20%15%10%5%0%%op=00


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 357the case study <strong>of</strong> Avellino- number <strong>of</strong> bays in X <strong>di</strong>rection:- number <strong>of</strong> bays in Y <strong>di</strong>rection;- interstorey height <strong>of</strong> the 1 st storey;- interstorey height <strong>of</strong> upper storeys;- infill average opening percentage at the 1 st storey (see Figure 5.3.1.20);- age <strong>of</strong> construction.Based on the age <strong>of</strong> construction, the following parameters weredetermined, as shown in Table 5.3.2.1:- Type <strong>of</strong> designAvellino was classified as seismic for the first time in 1981 (DM7/3/1981), following the 1980 Irpinia earthquake. It was in II seismiccategory, i.e., a seismic intensity parameter S = 9 was assumed. Hence,design base shear (see Section 2.5.2) was defined asS − 2F = C⋅ W = ⋅ W = 0.07 ⋅ W(5.3.2.1)100where W was the buil<strong>di</strong>ng weight. Therefore, a seismic (S) simulated designprocedure (see Section 5.2.2) was carried out accor<strong>di</strong>ng to such prescriptionfor buil<strong>di</strong>ng whose age <strong>of</strong> construction was determined as following 1981(see section 2 <strong>of</strong> the survey form, Figure 5.3.1.8).Vice versa, for older <strong>buil<strong>di</strong>ngs</strong> a simulated design procedure based ongravity loads only (G) was carried out. It is noted that in some cases (about20% <strong>of</strong> surveyed <strong>buil<strong>di</strong>ngs</strong>) the age <strong>of</strong> construction was not determined. Inthese cases, a weighted average <strong>of</strong> the ages <strong>of</strong> construction <strong>of</strong> other<strong>buil<strong>di</strong>ngs</strong> in the same census cell was calculated and this value was assumedalso for the buil<strong>di</strong>ng <strong>of</strong> interest.- Allowable stressesValues <strong>of</strong> allowable stresses for steel and concrete employed in thesimulated design procedure were also determined accor<strong>di</strong>ng to the age <strong>of</strong>construction. As far as concrete is concerned, a cubic compressive strength


358 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> Avellinoequal to 25 MPa was assumed in all cases, from which the allowableconcrete stress for ben<strong>di</strong>ng and for axial load combined with ben<strong>di</strong>ng werecalculated accor<strong>di</strong>ng to code formulations. Moreover, the concreteallowable stress used to determine column <strong>di</strong>mensions in the simulateddesign procedure was multiplied by a coefficient equal to 0.7 in the case <strong>of</strong>seismic design ((Pecce et al., 2004), see Section 5.2.2). Allowable steelstress (σ s,adm ) was calculated as the weighted average <strong>of</strong> the valuescorrespon<strong>di</strong>ng to <strong>di</strong>fferent steel typologies in time window correspon<strong>di</strong>ng tothe surveyed age <strong>of</strong> construction, depen<strong>di</strong>ng on the frequency <strong>of</strong> occurrence<strong>of</strong> each typology in this time window, accor<strong>di</strong>ng to the data reported in astatistical analysis <strong>of</strong> mechanical and typological characteristics <strong>of</strong>reinforcing steel used in Italy between 1950 and 1980 (Verderame et al.,2010b). For ages <strong>of</strong> construction above or below these limits, valuescorrespon<strong>di</strong>ng to the most widely spread steel typologies in 1950 and 1980were adopted, respectively.- ReinforcementReinforcing steel typology (smooth or ribbed bars) was also determinedas the most frequent typology in the time window correspon<strong>di</strong>ng to thesurveyed age <strong>of</strong> construction, accor<strong>di</strong>ng to the data reported in (Verderameet al., 2010b).- Steel and concrete material characteristicsConcrete compressive strength (f c ) was assumed equal to 25 MPa foreach age <strong>of</strong> construction. The Coefficient <strong>of</strong> Variation (CoV) for thisvariable was assumed equal to 31% up to 1981. The assumption <strong>of</strong> thesevalues was based on (Verderame et al., 2001). In the following years, a CoVequal to 25% was assumed, reflecting the improve in the reliability <strong>of</strong>concrete preparation. As far as steel yield strength (f y ) and the related CoVare concerned, again, average values from the data reported in (Verderameet al., 2010b) are used. Also in this case, for ages <strong>of</strong> construction before


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 359the case study <strong>of</strong> Avellino1950 or after 1980 the values correspon<strong>di</strong>ng to the most widely spread steeltypologies in these two years were adopted, respectively.Age Design Reinforcementσ s,adm f y CoV f c CoV[MPa] [MPa] [%] [MPa] [%]pre-1919 G smooth 140 325 20 25 311919-45 G smooth 140 325 20 25 311946-61 G smooth 173 336 22 25 311962-71 G smooth 203 399 18 25 311972-81 G ribbed 208 451 13 25 311982-91 S ribbed 240 466 11 25 251992-97 S ribbed 240 466 11 25 251998-01 S ribbed 240 466 11 25 25post-2002 S ribbed 240 466 11 25 25Table 5.3.2.1. Summary <strong>of</strong> data used in simulated design and in assessment depen<strong>di</strong>ng on theage <strong>of</strong> constructionTopographic (category T1 to T4) and stratigraphic (soil type A to E) data,accor<strong>di</strong>ng to the code classification (DM 14/1/2008), were needed in order todetermine the characteristics <strong>of</strong> seismic input spectra. Such characteristics weremade available and georeferenced in SIMURAI project. Topographic category,accor<strong>di</strong>ng to code definition, was determined depen<strong>di</strong>ng on ground slope,which was evaluated from a Digital Terrain Model (DTM), see Figures 5.3.2.1and 5.3.2.2. Soil type was determined from microzonation data, see Figure5.3.2.3. Census cells are also reported in Figures 5.3.2.2 and 5.3.2.3.Hence, to each buil<strong>di</strong>ng a topographic category and a soil type wereassociated. Among all the 693 considered <strong>buil<strong>di</strong>ngs</strong>, 484 were located on soiltype E, 200 on soil type B and 8 on soil type C, while 587 were in topographiccategory T1, 94 in T2 and 12 in T4.


360 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> AvellinoFigure 5.3.2.1. Digital Terrain Model <strong>of</strong> Avellino city


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 361the case study <strong>of</strong> AvellinoÜT1T2T40 250500 1 000 1 500 2 000MetersFigure 5.3.2.2. Distribution <strong>of</strong> topographic characteristics


362 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> AvellinoÜABCE0 250500 1 000 1 500 2 000MetersFigure 5.3.2.3. Distribution <strong>of</strong> stratigraphic characteristicsOpening percentage in upper storey infills was assumed equal to 20%,which can be considered as representative, on average, <strong>of</strong> window presence(Bal et al., 2007).


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 363the case study <strong>of</strong> AvellinoInfill typology, actually, was not surveyed in a large part <strong>of</strong> cases, and aquite high uncertainty anyhow affected this parameter also in the case when thisinformation was available. Hence, it was assumed to consider hollow clay brickpanels in all cases, and the material characteristics were derived from codeprescriptions (Circolare 617, 2009) assuming central values <strong>of</strong> the proposedranges, i.e. a shear elastic modulus equal to 1350 MPa, a Young’s elasticmodulus equal to 4500 MPa and a shear cracking strength equal to 0.35 MPa.Both parameters α and β (see Section 5.2.3) were assumed equal to 0.05.5.3.2.2 Analysis <strong>of</strong> resultsResults <strong>of</strong> seismic <strong>vulnerability</strong> assessment on <strong>RC</strong> buil<strong>di</strong>ng stock arereported in this Section. Vulnerability curves for <strong>di</strong>fferent buil<strong>di</strong>ng classes willbe shown first; then, the expected failure probability P f in a reference timewindow <strong>of</strong> 1 year will be illustrated. In particular, the attention will be focusedon Damage Limitation and Near Collapse Limit States.It is to be noted that the methodology for evaluating <strong>vulnerability</strong> curves inlongitu<strong>di</strong>nal or transversal <strong>di</strong>rection has been previously described (Section5.2.6), whereas in this Section, for each buil<strong>di</strong>ng and for each Limit State, asingle <strong>vulnerability</strong> curve is evaluated independent <strong>of</strong> the <strong>di</strong>rection; to this aim,for each <strong>of</strong> the N samplings =1000 sets <strong>of</strong> samplings, the correspon<strong>di</strong>ng PGAcapacity is evaluated as the minimum value between longitu<strong>di</strong>nal andtransversal <strong>di</strong>rections. Hence, the <strong>vulnerability</strong> curve <strong>of</strong> the buil<strong>di</strong>ng,independent <strong>of</strong> the <strong>di</strong>rection, is obtained as the cumulative frequency<strong>di</strong>stribution <strong>of</strong> these PGA capacity values. Failure probabilities at DL and NCLimit States are calculated for each buil<strong>di</strong>ng, accor<strong>di</strong>ng to the proceduredescribed in Section 5.2.7, based on the correspon<strong>di</strong>ng <strong>vulnerability</strong> curvesobtained accor<strong>di</strong>ng to this procedure and the seismic hazard described by thePGA excee<strong>di</strong>ng probability in 1 year, obtained from (INGV-DPC S1, 2007) forthe site <strong>of</strong> interest (Lon.: 14.793, Lat.: 40.915), see Figure 5.3.2.4.


364 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> Avellino10.90.8Excee<strong>di</strong>ng probability in 1 year0.70.60.50.40.30.20.100 0.02 0.04 0.06 0.08 0.1 0.12 0.14 0.16 0.18 0.2PGA [g]Figure 5.3.2.4. <strong>Seismic</strong> hazard for Avellino city (Lon.: 14.793, Lat.: 40.915), accor<strong>di</strong>ng to(INGV-DPC S1, 2007)Fragility curves will be illustrated in the following not referring to single<strong>buil<strong>di</strong>ngs</strong>, but to population <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong>. A fragility curve for a population <strong>of</strong><strong>buil<strong>di</strong>ngs</strong> is evaluated as the cumulative frequency <strong>di</strong>stribution <strong>of</strong> PGA capacityvalues obtained for all <strong>buil<strong>di</strong>ngs</strong> in the population; the number <strong>of</strong> these valuesis equal to Nsamplings × N<strong>buil<strong>di</strong>ngs</strong>, where N samplings (=1000) is the number <strong>of</strong> analysescarried out for each buil<strong>di</strong>ng and N <strong>buil<strong>di</strong>ngs</strong> is the number <strong>of</strong> <strong>buil<strong>di</strong>ngs</strong> in theconsidered population.Figures 5.3.2.5 and 5.3.2.6 report fragility curves at NC and DL LimitStates, respectively, for <strong>buil<strong>di</strong>ngs</strong> from 1 to 8 storeys. An increase in seismic<strong>vulnerability</strong> with the number <strong>of</strong> storeys is clearly observed in both cases. AtDL Limit State, in particular, fragility curves for <strong>buil<strong>di</strong>ngs</strong> with more than 3storeys are very close to each other.


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 365the case study <strong>of</strong> AvellinoP f10.90.80.70.60.50.40.30.20.1N storeys= 1N storeys= 2N storeys= 3N storeys= 4N storeys= 5N storeys= 6N storeys= 7N storeys= 800 0.5 1 1.5 2 2.5 3PGA [g]Figure 5.3.2.5. Fragility curves at NC Limit State for <strong>di</strong>fferent number <strong>of</strong> storeysP f10.90.80.70.60.50.40.30.20.1N storeys= 1N storeys= 2N storeys= 3N storeys= 4N storeys= 5N storeys= 6N storeys= 7N storeys= 800 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1PGA [g]Figure 5.3.2.6. Fragility curves at DL Limit State for <strong>di</strong>fferent number <strong>of</strong> storeys


366 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> AvellinoThe influence <strong>of</strong> the age <strong>of</strong> construction can be observed by reporting thefragility curves, at both DL and NC Limit States, <strong>of</strong> pre-1981 and post-1981<strong>buil<strong>di</strong>ngs</strong>. As a matter <strong>of</strong> fact, the major change represented by the introduction<strong>of</strong> seismic load prescriptions took place in 1981. As an example, Figures5.3.2.7 and 5.3.2.8 report fragility curves for pre-1981 (i.e., gravity loaddesigned) and post-1981 (i.e., seismic load designed) five-storey <strong>buil<strong>di</strong>ngs</strong>. Asexpected, a lower seismic <strong>vulnerability</strong> is observed in post-1981 <strong>buil<strong>di</strong>ngs</strong>, atboth Limit States.P f10.90.80.70.60.50.40.30.20.1DL - GDL - S00 0.02 0.04 0.06 0.08 0.1 0.12 0.14 0.16 0.18 0.2PGA [g]Figure 5.3.2.7. Fragility curves at DL Limit State for pre-1981 (gravity load designed - G) andpost-1981 (seismic load designed - S) five-storey <strong>buil<strong>di</strong>ngs</strong>


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 367the case study <strong>of</strong> AvellinoP f10.90.80.70.60.50.40.30.20.1NC - GNC - S00 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8 2PGA [g]Figure 5.3.2.8. Fragility curves at NC Limit State for pre-1981 (gravity load designed - G) andpost-1981 (seismic load designed - S) five-storey <strong>buil<strong>di</strong>ngs</strong>


368 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> Avellino<strong>Seismic</strong> <strong>vulnerability</strong> <strong>of</strong> analyzed <strong>buil<strong>di</strong>ngs</strong> can be also observed in terms <strong>of</strong>annual failure probability, at both Limit States. First, evaluated failureprobability at NC Limit State can be reported as a function <strong>of</strong> the number <strong>of</strong>storeys (see Figure 5.3.2.9). Mean values <strong>of</strong> P f are reported as red squares. Asexpected, a clear trend is observed, showing the higher <strong>vulnerability</strong> <strong>of</strong> taller<strong>buil<strong>di</strong>ngs</strong> (see Section 5.2.8).5.00E-044.00E-04P f,NC3.00E-042.00E-041.00E-040.00E+00N storeys0 2 4 6 8 10 12Figure 5.3.2.9. Annual failure probability at NC Limit State depen<strong>di</strong>ng on the number <strong>of</strong> storeysFailure probability at DL Limit State is reported in Figure 5.3.2.10. Onaverage, these probabilities are lower by an order <strong>of</strong> magnitude with respect tothe correspon<strong>di</strong>ng probabilities at NC. Also in this case, as expected, the failureprobability increases with the number <strong>of</strong> storeys; nevertheless, this increase isnot as uniform as for NC Limit State, rather highlighting a sudden increasewhen the number <strong>of</strong> storeys changes from the range <strong>of</strong> values N storeys ≤ 3 toN storeys ≥ 4.


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 369the case study <strong>of</strong> Avellino5.00E-034.00E-03P f,DL3.00E-032.00E-031.00E-030.00E+00N storeys0 2 4 6 8 10 12Figure 5.3.2.10. Annual failure probability at DL Limit State depen<strong>di</strong>ng on the number <strong>of</strong>storeysFigures 5.3.2.11 and 5.3.2.12 report mean failure probabilities at DL andNC Limit State in pre- and post-1981 <strong>buil<strong>di</strong>ngs</strong>. If a relative comparison iscarried out for equal values <strong>of</strong> N storeys , a higher failure probability in pre-1981<strong>buil<strong>di</strong>ngs</strong>, as expected, can be observed, particularly at NC Limit State.More clear observations can be made if a comparison is carried outassuming the same stratigraphic and topographic con<strong>di</strong>tions for all thecompared <strong>buil<strong>di</strong>ngs</strong>. In particular, soil type E and T1 topographic category areassumed, representing the most common con<strong>di</strong>tions. Moreover, the comparisonis carried out between <strong>buil<strong>di</strong>ngs</strong> built during 1972-81 and 1982-91 decades,right before and after the introduction <strong>of</strong> seismic load prescriptions. Three- toeight-storey <strong>buil<strong>di</strong>ngs</strong> are observed, inclu<strong>di</strong>ng the large part <strong>of</strong> the <strong>buil<strong>di</strong>ngs</strong>tock. In this case, the decrease in failure probability due to the introduction <strong>of</strong>seismic prescriptions can be more clearly observed. In particular, this <strong>di</strong>fferenceis more pronounced at NC Limit State. However, most clear is the dependenceon the number <strong>of</strong> storeys.


370 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> Avellino3.00E-033.00E-042.50E-032.50E-042.00E-032.00E-041.50E-031.00E-035.00E-040.00E+00pre-1981post-19811234567 81.50E-041.00E-045.00E-050.00E+00pre-1981post-19811234567 8(a)(b)Figure 5.3.2.11. Comparison between annual failure probabilities at DL (a) and NC (b) LimitStates in pre- and post-1981 <strong>buil<strong>di</strong>ngs</strong>3.00E-033.00E-042.50E-032.50E-042.00E-032.00E-041.50E-031.50E-041.00E-03781.00E-04785.00E-04565.00E-05560.00E+0040.00E+00472-8182-91372-8182-913(a)(b)Figure 5.3.2.12. Comparison between annual failure probabilities at DL (a) and NC (b) LimitStates in 1972-81 and 1982-91 <strong>buil<strong>di</strong>ngs</strong> (soil type E and topographic category T1)


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 371the case study <strong>of</strong> AvellinoThe influence <strong>of</strong> infills on the seismic <strong>vulnerability</strong> can be observed lookingat the trends <strong>of</strong> failure probability with the percentage <strong>of</strong> infill openings at thebottom storey, for the same <strong>buil<strong>di</strong>ngs</strong> reported in Figures 5.3.2.13 and 5.3.2.14.At both Limit States, the detrimental effect <strong>of</strong> a decrease in the amount <strong>of</strong>infills at this storey is clearly reflected by the increase in failure probability.4.00E-03P f,DL3.00E-032.00E-031.00E-030.00E+00infill openingpercentage0 20 40 60 80 100Figure 5.3.2.13. Annual failure probability at DL Limit State depen<strong>di</strong>ng on the infill openingpercentage at the bottom storey (soil type E and topographic category T1)4.00E-04P f,NC3.00E-042.00E-041.00E-040.00E+00infill openingpercentage0 20 40 60 80 100Figure 5.3.2.14. Annual failure probability at NC Limit State depen<strong>di</strong>ng on the infill openingpercentage at the bottom storey (soil type E and topographic category T1)


372 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> Avellino<strong>Seismic</strong> <strong>vulnerability</strong> can also be analyzed by observing the spatial<strong>di</strong>stribution <strong>of</strong> main considered parameters and <strong>of</strong> failure probability at DL andNC Limit States. In particular, the spatial <strong>di</strong>stribution can be referred to singlecensus cells reporting correspon<strong>di</strong>ng average values among <strong>buil<strong>di</strong>ngs</strong>.Figures 5.3.2.13 to 5.3.2.15 report the average number <strong>of</strong> storeys, theaverage age <strong>of</strong> construction (pre- and post-1981 <strong>buil<strong>di</strong>ngs</strong>) and the mostwidespread soil type per census cell, respectively. It can be noted that highervalues <strong>of</strong> the average number <strong>of</strong> storeys are generally observed close to the citycentre, while, as far as the age <strong>of</strong> construction is concerned, no homogeneousareas can be clearly identified, probably due to the post-1980 earthquakereconstruction. Soil types B and E are most widely spread in Western andCentral-Eastern areas, respectively.Figures 5.3.2.16 and 5.3.2.17 report the average annual failure probability atDL and NC Limit States per census cell; generally higher values are observed incentral and North-Western areas, at both Limit States. In ad<strong>di</strong>tion to the number<strong>of</strong> storeys and the age <strong>of</strong> construction, which have been previously <strong>di</strong>scussed, aclear influence <strong>of</strong> the <strong>di</strong>fference in seismic hazard due to a <strong>di</strong>fferent soil typecan be recognized, see Figure 5.3.2.15, lea<strong>di</strong>ng, as expected, to higher failureprobabilities, on average, for <strong>buil<strong>di</strong>ngs</strong> located on soil type E.


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 373the case study <strong>of</strong> AvellinoFigure 5.3.2.13. Average number <strong>of</strong> storeys <strong>of</strong> rectangular <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> per census cell7


374 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> Avellinopre-1981post-1981Figure 5.3.2.14. Average age <strong>of</strong> construction <strong>of</strong> rectangular <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> per census cell


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 375the case study <strong>of</strong> AvellinoFigure 5.3.2.15. Most widespread soil type for rectangular <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> per census cellBCE


376 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> Avellino1.5e-004 - 8.7e-0048.8e-004 - 1.5e-0031.6e-003 - 2.0e-0032.1e-003 - 2.4e-0032.5e-003 - 3.3e-003Figure 5.3.2.16. Average annual failure probability <strong>of</strong> rectangular <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> at DL per census cell


Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>: 377the case study <strong>of</strong> Avellino1.3e-005 - 8.4e-0058.5e-005 - 1.5e-0041.6e-004 - 1.8e-0041.9e-004 - 2.2e-0042.3e-004 - 2.9e-004Figure 5.3.2.17. Average annual failure probability <strong>of</strong> rectangular <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong> at NC per census cell


378 Chapter V – Simplified approach to the seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>existing</strong> <strong>RC</strong> <strong>buil<strong>di</strong>ngs</strong>:the case study <strong>of</strong> Avellino5.4 FUTURE RESEA<strong>RC</strong>HThe proposed approach – based on a simulated design procedure and on asimplified modelling <strong>of</strong> the structural response through the Shear Typeassumption – can provide a large scale seismic <strong>vulnerability</strong> assessment <strong>of</strong> <strong>RC</strong><strong>buil<strong>di</strong>ngs</strong> based on relatively poor input data, also taking into account importantparameters such as the presence <strong>of</strong> infill elements and the age <strong>of</strong> construction.However, further developments are foreseen; for instance, assessmentmethodologies more advanced than the spectral method, such as nonlineardynamic analyses, may be employed on such simplified models, which presentthe advantage <strong>of</strong> a high reduction in computational demand (e.g., Mollaioli etal., 2009).The illustrated procedure should also be integrated with a reliable estimate<strong>of</strong> the influence <strong>of</strong> brittle failure mechanisms – also due to local interactionmechanisms between structural and non-structural elements – on the seismic<strong>vulnerability</strong>. Moreover, other parameters such as the irregularity in plan and/orin elevation should be taken into account. As a matter <strong>of</strong> fact, post-earthquakeobserved damage <strong>of</strong>ten demonstrated how a reliable seismic <strong>vulnerability</strong>assessment cannot <strong>di</strong>sregard these factors.


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