4 - Memorial University of Newfoundland DAI

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and maintain a minimum reflection coefficient. Wwo filter plittrs nllirrd directly to the 1-1 of the wave gcncralor are urd lo rdnro ll~c prrsww 01 cmaa tank weillation in the Lank. 5.1.2 Instrumentation of the Model The experimental model was bolled onlo s 152.1 cm diamctcr, 2.54 ctln thick, circular water-pmoled plywood plate-which inn turn was boltcrl to the hot- tom of lhe wave lank-and levelled in plncc by the apcciillly rlc.sigtnc.cl Ihi~*c mntteetors mentioned earlier in section 1.1; rcfer to i*igolrc .1.!1. 'I'l~c. tn~odvl was installed at a distance of about 12.8 m from llte lrero lroxilinlt ol lhr w i ~ a board. Threo capacitnnco type wnvc probes wcrc uxcvl to nr?uan, tito itwant- ing wavea; tl!cse were designalml PI to P3 for em of rrlrmrwc!. llileh prolrc is equipped with a cnpacitnnm rnctcr lo convcrl tho cllu~yc. is cnpiwitiotr,c (resulting as lhe waves interact wit19 tilo probc) lo n r1.c. vnll.rge. '1'1wlpmi,r~8 were calibrated in "nib of dirtanm in contimetem Ipcr voll. 'I'Bcrc.k,w, 1.l~. changes in waveelevation above or bolow the mean water levci msid iw t:ona- puled. Probe P I was located about 1 "1 in fmut al lho sode el; that is, idr,sg the ~cntedine or the broad sido of the scuelure. I'mhra 1'2 i~tlcl I':l w#.a, installed adjacent lo the narmw sideat distances 0.6 and 1.2 m, n.apr:rlir.ly, from tho wall 01 the tank shown enrlier in Figan: 6.1. 'I'lte~: two pmhca won. used to determine if tllccc wen! my emss.tnsk ascillntion elk:cl.*, 'Vhi* wcllrld bc shown by any major dissimilnrilies between tlm ~ignnls ~w;ilaarcrl wil.11 thr firal pmbc and with t hw mciuurcd will, the sccoad nncl lltir
LEGEND FI B F2 FREE VlBllTlDN INITIhTION POINTS HI TO "6 lMPAC7 LOCATIONS AI TO ACCELEROMETERS 1 "' "4- - FZ B HZ FIG. 5.6 INSTRUMENTATION. FREE VlBRATlON AND IMPACT LOCATIONS.
Page 5 and 6:
NOTICE The quallty of this microfor
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I*I Et"" :lbL="*"" k.. bpilmsa7d Di
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Acknowledgements I should like lo t
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Abstract As a result of the increas
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Contents List of Figures xii List o
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4.6.3 Fnbrieatiox of tllc Rcduced M
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A Selected Algoilthma 278 A.1 Diago
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4.5 Member Configuration at level #
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7.21 Dynamic Mode # 6 (Intact Model
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7.49 Typical Measured lnput Wnve Sp
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7.66 hulls fmm Accelerometer A2 due
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D.ll DynamicMode # I (Intact Model)
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List of Tables 4.1 Symbols, Units a
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8.9 Pacent Changes in Resonant Frrq
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List of Symbols d(k) .i(k) A A(L1 1
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autosp~trni density of r(t) cms-spe
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0,1,2
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[@I a Pu. P. P:,," P.. o2(k) instan
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een recorded, then it is beneficial
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Associated with every vibration mod
Page 46 and 47:
Such s model is called a dynamicall
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presenlcd. Chapter 3 contains the t
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al frequcncic. occurred when member
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detwM from the data roeorded (later
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y Duggan d a!. [a]. This study inve
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~~lidity of the results war rompsro
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nic~~~aan:immcdiateiyuseful, they a
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tlncayatem hehavior oftrusswork pla
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Chapter 3 Theoretical Modelling Tll
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3.2 Wave Theories Works by earlier
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F;-RY% WAVE THEORY) 1/20 I "w/Lw DE
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DIRECTION OF WAVE PROPAGATION FIG.
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liero, d and ita wlocity component
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and and a+ "=-. OY = wA~inl~IW(1+ s
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FIG.3.4 ARBITRARILY ORIENTED CYLIND
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~i n long c mtd wave is being conai
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inrther. Ultimately, the resulting
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equcncia and mode shapes, equalion
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Toestablish tho relationship betwee
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Furthermore, from equation (3.56),
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lG.3.6 SIMULATED 3-D AND STICK MODE
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1. priam&tic heam members, 5. sir d
Page 92 and 93: The equation of motion for each ele
Page 94: From tho ~tatic dispiaeemont muita,
Page 97 and 98: instance, the non-dimensional equal
Page 99 and 100: functional relationship relating th
Page 101 and 102: whcre F, 't iinstantanmua force at
Page 103 and 104: Table 4.1 Symbols, Unit. and Dimens
Page 105 and 106: thc Buckinghm r-Thmrem (i.c., I2 te
Page 107 and 108: That is, equations (4.28) and (4.29
Page 109 and 110: C. Ilence, if the dynamic amplifica
Page 111 and 112: where (2) is the general gmmdric or
Page 113 and 114: the prolotype. Damping is dcfincd b
Page 115 and 116: 2 LEVEL # 7 1 28956DO NOTE: ALL DIM
Page 117: Mataial= Structural Steel, E = 206.
Page 122 and 123: LEVEL C6 NOTE: ALL DlMENStONS IN m
Page 124 and 125: Table 4.5 Relevant Materiel Propert
Page 128 and 129: FlG.4.9 COMPLETED STRUCTURE. 89
Page 132 and 133: Since the de& sertioo of the struct
Page 134 and 135: % FINITE ELEMENT ANALYSIS (COMPUTER
Page 136 and 137: 3 53 I CONTROL RM SECTION A-D. MEZZ
Page 139: I I SERVO CONTROLLER MODEL 408.1% j
Page 144 and 145: 5.1.4 Response Circuit Data acquisi
Page 146 and 147: I ~T.UG~U~E LEGEND: DYIIYT I., 10 A
Page 150 and 151: the basis upon which the irregular
Page 152 and 153: then manipulated by the computer ro
Page 154 and 155: ,.. G STRUCTURE IN STILL WATER STRU
Page 156 and 157: dter every set of hen wave excitati
Page 158 and 159: To gather spectral information fmm
Page 160 and 161: is the timelag between silrnplev~l~
Page 162 and 163: ics, with a lew notable exceptions,
Page 164 and 165: If bath aides of the dove cguntion
Page 166 and 167: Conversely, r(1) can be estimated b
Page 168 and 169: quires ahout N(M + 1) + 9Y1 arithme
Page 170 and 171: So equation (6.18) become: I, i = C
Page 172 and 173: At each resonant frequency, the hdl
Page 176: 6.5 Impact Testing Impact testa wer
Page 179 and 180: Chapter 7 Theoretical and Experimen
Page 181 and 182: Table 7.1 Natural Wequeney Comparis
Page 188: Therefore, with the natural freluen
Page 199:
Pi7 Be: kD! SF:& iid id . -5 i#@ Ba
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(i.o., at noder 6, 12, 18, 22 and 2
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tirne dntn;lis reprcsez~lnlioti of
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-CUI~IW~~~ anstmr 9~1sn-mmu3n DL um
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the posilivc and nogntivr peaks. Re
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Table 7.7 X-Direction Results From
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2 GEhEnnlEO FRDM TdE WrllTE hOISE l
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FIG. 7.53 MEASURED INPUT WRVE FROM
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'IUnU133dS 3SIR1 31IHI 9NISn--91 30
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Table 7.9 MEM Damping Estimates fro
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7.2.3 Impact Test Results In Chsptc
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(K 01 0 01- OZ- DE- 0,- OBI (KI 09
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Chapter 8 Discussion of Results In
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of rnemhcr removal can he visually
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emoved is a cancellation offecl, an
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Force Variation Along the Jacket. P
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fi~t on the lower rrequency end of
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pond approximately to thasc which c
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'Ikble 8.1 Measured Resonant Rsquen
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Table 8.6 Measured Resonant Wequenc
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After a close look at the measured
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Table 8.11 Percent Changes in Reson
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Table 8.16 Percent Changes in Reson
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apprmiably. Since the tmnsa of the
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'*~+12 \5 \8 h4 h7 $0 FREOUENCY IHz
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8.2.4 Impact Test Results 'l'incobj
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I able 8.20 Comparison of the Reson
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'Phc invalidity of thc lumped mass
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Chapter 9 Concluding Remarks and Re
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general agreement. 5. An investigat
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mode, br example, might have been e
Page 303 and 304:
References K I'o,lnt~n~. 'A Sludy o
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[21] .I.K. Vandiver, "Structo~ral D
Page 307 and 308:
1431 D.J. Kartewcg and G. d-Vria "O
Page 309 and 310:
1671 I..S. Marplo, "A NCW Autorepes
Page 311 and 312:
(111 J. Zhou "Ocean Wave Simulation
Page 313 and 314:
[Ill M.C. Ilallsm, N.J. Hcaf and L.
Page 315 and 316:
Appendix A Selected Algorithms Tllr
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- M = the total mass of the slructu
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Suhrtituting qualion (A.5) in equal
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..3 Longuet-Higgins and Cokelet Smo
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Appendix B Sample Calculations Typi
Page 325 and 326:
The dcnsity of ABS plsstic (p.,,) i
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C.l Calibration and Instrumentation
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D.l Mode Shape (Members 70 and 68 R
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D.2 Results for an Impact Initiated
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i W 4 P Li I 2: 5: E B '5 2- d :" i
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oa m 01 o or- QZ- oe- om Q Z ~ oo a
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D.3 MEM Damping Estimates for the D
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Table D.4 MEM Damping Estimate. fro
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4 - Memorial University of Newfoundland DAI

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