Code Manual for CONTAIN 2.0 - Federation of American Scientists

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e “compartmentalized” if the principal path for debris dispersal from the cavity communicates with a compartmentalized lower containment, the structures of which present additional barriers to debris transport to the main volumes of the containment; the geometry is said to be “open” if the principal path for debris dispersal communicates directly with the containment dome. To date, there is considerably more experience with analyzing DCH scenarios in compartmentalized geometries than in open geometries. The impact of any given uncertainty on the results of DCH calculations can depend strongly upon the initial and boundary conditions of the scenario of interest. It is therefore impossible to give a quantitative estimate of the magnitudes of these uncertainties that would be applicable to all DCH analyses. In some cases, therefore, the discussion in Section 13.3.2.2 includes suggested sensitivity calculations. These recommendations are designed to provide the user with a reasonable understanding of the uncertainty for the particular case at hand. To date, there has been only limited application of the approaches suggested hereto nuclear power plant (NPP) analyses. Hence, some of the suggestions offered must be considered tentative. 13.3.2.2 The Standard Input Prescription for DCH Calculations. This section presents the standardized input prescription for DCH analysis that was reported in References Wi195 and Pi195. It discusses how to define debris source tables to simulate RPV ejection and cavity entrainment processes. 13.3.2.2.1 Philosophical Basis and Purpose of the Standard Prescription. As elsewhere in CONTAIN, the design philosophy for DCH modeling has been to provide mechanistic modeling for ~ phenomena which are sufficiently well understood to justify a defensible mechanistic model, and to provide simpler or parametric models with flexible input options for phenomena that are not well understood, or that cannot be represented fully within the limitations imposed by the basic lumpedpararneter, control-volume architecture of the CONTAIN code. When combined with the complexity of DCH phenomenology, this philosophy has led to provision of a large number of input and modeling options for DCH analysis. This flexibility in CONTAIN DCH modeling is currently viewed as being essential in order to permit the user to study uncertainties in the results of DCH calculations, as well as to permit the user to take advantage of any fiture refinements in DCH understanding. However, it obviously presents problems with respect to quality control and consistency, if some type of control on DCH input is not available. Hence an important goal of the CONTAIN DCH assessment effort was to develop a standardized input prescription for DCH calculations. The standardized input prescription was defined for a number of purposes. These include providing guidance for code users and providing a means for allowing investigators working independently to obtain comparable results when consistency is desired. On the other hand, the standard prescription definitely is not offered as a “cookbook” that must be followed, or that will guarantee good results if it is followed; it is not an “official” prescription endorsed by the United States Nuclear Regulatory Commission or any other standard-setting body. It is only being offered by the CONTAIN project as a suggested starting point or guideline. The standard prescription has potentially important limitations, and sensitivity studies to explore uncertainties are likely to be a part of any study that Rev O 13 24 6/30/97
— uses CONTAIN. In any given analysis, there maybe specific features that justify a departure from the standard prescription. One recommended use is to take the standard prescription as a starting point and to document any deviations from the standard prescription when reporting results. Where possible, the standard inputs have been based upon separate-effects measurements obtained in the DCH experiments and/or stand-alone modeling. Separate effects measurements for phenomena such as hydrogen behavior obtained from DCH experiments were preferred to results of non-DCH experiments because the conditions of the latter often differ sufficiently from DCH conditions that applicability to DCH is doubtfil in many instances. Parameters were not chosen by tuning directly to the integral results themselves (i.e., tuning to AP or hydrogen production results), with the partial exception of the non-airborne debris parameter ~a~ discussed in Section 6.6 of this manual. Another principle guiding the specification of the standard prescription was the desire to be mildly conservative when applying the prescription to scenarios differing from those that have been studied experimentally, especially in scenarios thought likely to be more severe than those studied experimentally. By “mildly conservative” is meant that, when available options appear to be equally defensible, the option expected to result in more conservative extrapolations is selected. The standard prescription should not be thought of as bounding, however. For example, when the more conservative choice is considered to be distinctly less plausible than a less conservative choice, the conservative choice is generally not taken to be the standard even if this choice cannot be rigorously ruled out. The methodology applied for developing the standard prescription was as follows: 1. Using previously available information and some initial exploratory calculations, a standard input prescription for analysis of DCH experiments was defined. 2. The standard prescription was then “frozen” and applied to analyze a total of 22 experiments that have been performed using high-temperature melts generated by the iron-oxide aluminum therrnite reaction. 3. A large number of sensitivity cases were performed, with all parameters remaining frozen at the standard values except those explicitly identified as being assigned to different values. These sensitivity studies were performed for many different reasons: to demonstrate that uncertainties in many of the input parameters actually matter little to the results, to explore the sensitivity of the results to those input parameters and modeling assumptions that do matter, to determine how important certain specific phenomena such as atmosphere-structure heat transfer are to the results, to examine model behavior and compare (as best possible) the model behavior with the behavior observed in the experiments, and to examine the degree to which alternative explanations exist for the experimental trends. 4. Using lessons learned from the results of the study, some modifications were introduced into the standard prescription for application to NPP analysis. O 13 25 6/30/97
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Code Manual for CONTAIN 2.0: A Comp
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ABSTRACT The CONTAIN 2.0 computer c
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TABLE OF CONTENTS (CONTINUED) 4.0 A
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R O TABLE OF CONTENTS (CONTINUED) 6
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TABLE OF CONTENTS (CONTINUED) 9.1.3
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TABLE OF CONTENTS (CO NTINUED) 13.0
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TABLE OF CONTENTS (CONTINUED) 14.2.
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TABLE OF CONTENTS (CONTINUED) 16.3.
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TABLE OF CONTENTS (CONCLUDED) C.2Va
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LIST OF FIGURES (CO NTINUED) Figure
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LIST OF FIGURES (CONCLUDED) Figure
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LIST OF TABLES (CONCLUDED) Table 9-
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1.0 INTRODUCTION The CONTAIN code i
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. respond under accident conditions
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This code manual includes documenta
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The intent of this document is to p
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Table 1-3 Major New Models and Feat
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Deposition/ Agglomeration Rates Hea
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For completeness, the environment o
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ilobal Loop zstart I Input * Loed N
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Table 2-1 lists the internal timest
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where p is the structure density, C
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material definitions are given in t
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water vapor, noncondensable gases (
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2.7 Aerosol Behavior Events occurri
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In addition to these models, fissio
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2.10 Heat and Mass Transfer Through
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diffusion of water and the released
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primary system through a large ice
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Gas Liquid ● argon ● nitrogen
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Table 3-2 References for CONTAIN Ma
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● A common reference temperature,
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where u$T,P) = h$T) = ~~TcP,f(T)dT
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Table 3-3 The Coefficients Aij in E
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To ensure that the extrapolation ha
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4. AssumWion of saturated intermedi
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output after a run is completed, th
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4.0 ATMOSPHERIVPOOL THERMODYNAMIC A
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o 0 *0-0 o +F-ooo 0000 Atmosphere G
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Am An HW ❑ Ht AI * HI= Hb Figure
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connected to the respective cells.
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A side-connected path is defined as
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4.3 ~ tion The flow modeling option
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FLOW option for overcoming the gas
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Table 4-2 Conservation of Momentum
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4.4.3 User-Specified Flow Rates The
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4.4.5 Gravitational Head Modeling T
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gas center-of-volume elevations, in
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crossover parameter y always select
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interface, since in CONTAIN materia
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where dmi ~ Table 4-3 Conservation
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where Table 4-3 Conservation of Mas
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Table 4-4 Conservation of Energy Eq
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Table 4-5 Conservation of Mass Equa
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Table 4-6 Conservation of Energy Eq
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architecture. A gas-pool equilibrat
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Finally, the mass transfer rate of
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where Ap~jis the area of the atmosp
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The FIX-FLOW option may be useful i
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exit losses and other fictional los
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. Pressure: where Pi = 2 k=l Table
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CCIS are modeled through an embedde
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~ Boiling \t/ o 0: O.” 0°0000 .O
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the pool layer should lie on top of
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modeled will include the scrubbing
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ebar using the RBRCOMP keyword. Con
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aerosol release model. The allowabl
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Keyword Chemical Symbol Table 5-4 M
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The coolant pool layer is unique in
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water and regarding heat transfer a
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options is directed to the fwst nod
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5.6.2 External Lower Cell Material
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CONTAIN Code Main Modules CONTAIN I
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5.7.5 Restrictions in Mass and Ener
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Both gas-phase and condensed-phase
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decay power calculated in the DECAY
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5.8.15 Energy Conservation (2.3.12
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4. 5. 6. 7. 8. 9. imposed on it by
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6.0 DIRECT CONTAINMENT HEATING (DCH
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● ● ● “. . . . . ● ☞✍
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evolve independently of the other d
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The combined mass flow rate of gas
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where ,=W Ipgu+wi Note that when al
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‘ig,i,k _ — — ~‘jiwji$ ‘g
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entering directly into the atmosphe
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airborne particles can be neglected
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1. Conventional atmospheric source
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ecommended that the user review Ref
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The heat transfer coefficient betwe
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other versions of the Whalley-Hewit
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6.2.10.2 Entrained Fraction Correla
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and [) y+l y+l f(y) = yo”s ~ 2 (y
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ecause the desired fraction of debr
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pdv; NWe=— C! (6-71) where NW.is
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Equations (6-73) and (6-74) may all
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dmd’ ,, ~ +[+” rpv,s [1 ‘t en
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Tin = v.=— g,ln Z ‘g,ji6jiTg,jc
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An important aspect of the CONTAIN
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6.3.6 TOF/KU Trapping Model Like th
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whose default value is 0.32, p~jis
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The flight time and average velocit
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If slip is ignored completely, then
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Zr +2HZ0 + Z@z+2Hz L Fe+ H20 “ zr
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The Reynolds and Schmidt dimensionl
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D H20 = 4.40146 X 10-6 (T~~)2334 P
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.. 1-exp -~ = 0.5 [} ‘d where t~o
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AN~~, = N& 1- exp -— ‘re [{IIAt
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(AI-120)i,n= (~)~oAtC Am,j,.,,=-((A
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where ~~,i,. = (AO&hO~P&i,n) + (AH2
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calculated intercell mass flow rate
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The total radiative energy loss fro
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The velocity for non-airborne debri
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UK ~ DSolid Aerosol Water [ A Spray
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● particle scrubbing from gases v
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too small by evaporation of water.
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(7-3) where d(&(t)/dt is the time r
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This constraint thus reduces the nu
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particles can combine at a time. Th
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Except when they include significan
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Table 7-1 Comparison Between Fixed-
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Figure 7-3. Model for Water Condens
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The condensation Reference Pru78: r
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DiffusioDhoresi$. When water conden
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the user may specify these paramete
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The settling area ~ is the sum of a
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The effective cylindrical diameter
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where St is the Stokes number, the
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100 1 ()-1 10-2 1()-3 10-4 ‘\ Tot
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and Potential Flow: ELP E ll,p = =
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The efilciency E of a spray drop ch
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with enhanced scrubbing) or a small
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As an example of difficulties that
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,. - 137c~ / \ P- w 137M Ba 1 137Ba
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user. From this information, the co
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No. 7 No. 8 No. 9 No. 10 No. 11 No.
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~- ~- No. 19 l~R” —> 106Rh~ 106
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No. 28 No. 29 No. 30 No. 31 No. 32
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with the host. In such cases, the f
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103Rhbranch as in the second chain
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and B2, respectively, differing onl
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Table 8-3 Fission Product Library -
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inventory and for time-dependent so
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[Lee80] Note that array space for t
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I GAS UC Atmosphere Heat +%.OOO 00
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where t is the problem time in seco
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where V~ is the drop volume, which
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supplied by the library. Such inven
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The governing equation for the chan
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s DFB is assumed to occur whenever
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The chemical reactions that occur d
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up before ignition occurs. For exam
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delay factor is too small, the tota
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The deflagration model assumes that
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The above correlations assume only
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to occur in the bum model at a reas
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where At~,is the remaining bum time
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Specifically, for DFB to occur, the
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where NtOti= N~ + N~o + ~ is the to
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wheres, is the user-specified spont
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—’ - ● *4 / hMl Outgassing St
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prior to CONTAIN 1.2, there is cons
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except for the error introduced by
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0.1 0.08 0.06 0.04 ~ 0.02 h G o s .
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Nk = ~BLcp,BLABL h = kB~N~u/L (10-1
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unsubmerged surface of the structur
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‘=4Hpi-Hb’iF$l (10-15) e where
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to simulate forced convection throu
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10.1.3 Generalized Gas-Structure Co
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Note that the default correlations
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Because the heat and mass transfer
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0.01 0.001 0.0001 0.00001 temperatu
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0.01 0.001 0.0001 0.00001 ~emperatu
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default correlations with ones of t
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The film tracking model is discusse
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this limit would correspond to a fi
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follows the standard recommendation
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In Equation (10-54) the relation 6
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where N is the number of the surfac
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X= XO-b At, AT (lo-66) where X“is
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The ernissivity of each of the abov
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The term ~ in Equation (10-80) is t
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coolant subcooling. The various cor
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If boiling is occurring at the inte
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‘TL.eid,s.b = ATbid + 8 AT,ub (10
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Concrete Air Figure 10-8. Cylindric
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where k is the thermal conductivity
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T 2,eff = T2 h I,eff = hlz whereas
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extrapolated temperature as defined
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Distance ~ ~ Surface Node ~ Nodei F
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The interface temperature Oihas sti
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to be reduced in proportion to this
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fde, TAPE17, to the effect that the
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The outgassing of evaporable water
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Gas Film Boundary Layer Bulk \& I A
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interface temperature. Note that co
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● heat transfer between the atmos
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Reactor Pressure Vessel Drywell Sou
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Figure 11-2. CONTAIN Multi-Node Ven
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L“ ●LO n ‘n I ,a ,rn n I I I
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Table 11-1 Example Solution for Flo
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IDrywell Water Vapor and Gas Source
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—= dx — dt F Pq 1 2[pd - ‘w +
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Drywell, Pd Ii P(f> Pw Vent Vd =
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For flow from wetwell to drywell, a
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Aeff =4 for AP > APU where ~ is the
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the component hosting the fission p
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noncondensable gases multiplied by
Page 423 and 424: 12.0 ENGINEERED SAFETY FEATURE MODE
Page 425 and 426: ~ Spray Flow Path ~~ Reinforced Con
Page 427 and 428: Inlet Manifold Cold Side Hot Side C
Page 429 and 430: other than air or superheated condi
Page 431 and 432: Because the total heat transferred
Page 433 and 434: 7 Plenum t Ice Compartment 1 Accumu
Page 435 and 436: spring or gravity-controlled motion
Page 437 and 438: conditions. If “citlex” does no
Page 439 and 440: where p~is the atmosphere gas mixtu
Page 441 and 442: In these equations, N~~is the drop
Page 443 and 444: Figure 12-8. Th,o ~b Cold Leg (Outl
Page 445 and 446: The capacity-rate ratio CR is defin
Page 447 and 448: Note that the user-specified pump m
Page 449 and 450: 13.0 USER GUIDANCE AND PRACTICAL AN
Page 451 and 452: small flow areas. Also, in the mome
Page 453 and 454: 13.2.4 Aerosol Modeling ~t. The aer
Page 455 and 456: ~s. The heat given off by many radi
Page 457 and 458: concentration in the cell maybe hig
Page 459 and 460: In comparisons with experimental re
Page 461 and 462: It is normally considered inappropr
Page 463 and 464: 0.00016 0.00014 0.00012 0.0001 8E-0
Page 465 and 466: 13.2.9 Calculational Sequence Effec
Page 467 and 468: 13.3.1.3 Modelin~ Stratifications.
Page 469 and 470: Figure 13-2. Two Thermal Siphon Nod
Page 471: for the Sequoyah plant given in Cha
Page 475 and 476: 0.4 0.3 0.2 0.1 (a) / ~ ..” ~ ●
Page 477 and 478: Table 13-1 Summary of the CONTAIN S
Page 479 and 480: 0.4 1J- 2 6.3 d# p“ RPV (13-1) He
Page 481 and 482: 1. Use Equation (13-1) to define z~
Page 483 and 484: In the standard prescription, the c
Page 485 and 486: as small pipes, cabling, etc. Impac
Page 487 and 488: esulting from homogenizing cool age
Page 489 and 490: equivalent to that of the liquid wa
Page 491 and 492: called “tarnping.” Since aeroso
Page 493 and 494: Co-Eiected Primarv Svstem Water. Wa
Page 495 and 496: .- If the initial atmosphere compos
Page 497 and 498: hybrid solver was not available at
Page 499 and 500: 13.3.2.3 RPV Models. When the RPV a
Page 501 and 502: other governing input parameters. I
Page 503 and 504: and Griffith. ~i196] In addition, t
Page 505 and 506: several reasons, the assessment per
Page 507 and 508: area. It is recommended that the us
Page 509 and 510: 800 700 600 500 400 300 200 100 0 \
Page 511 and 512: heat flow under conditions of nearl
Page 513 and 514: dumped into a layer in a short time
Page 515 and 516: Comments at the begiming of an inpu
Page 517: — cannot be modeled directly. How
Page 520 and 521: CELL, must follow the global input.
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CELL 1 && beginning of input for ce
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In the following input descriptions
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A sub-block thus can begin with a l
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The global CONTROL block is used to
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NENGV = nengv NWDUDM = nwdudm NMTRA
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table may be specified after the CO
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COMPOUND keyword. Such names need n
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RHOT density values, paired with th
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correspond to the species as they a
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14.2.4 Intercell Flows be considere
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nat the number of cell atmospheres
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cellfr the number of the cell from
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VTOPEN = vtopen TYPE = {GAS or POOL
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RVAREA-P the keyword for initiating
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NWET the number of the cell contain
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(NAME=aname [FLAG=iflag] X=n (x) VA
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keyword will result in the oversize
Page 556 and 557:
SURTEN the surface tension of a wet
Page 558 and 559:
newcof = 2: Coefficients are reques
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FINVT = (finvt) (8-5). If FGPPWR is
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In the input block description of t
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FDISTR = (fdistr) FDEVEN GRPLIM = g
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DIFH20 the multiplier on the mass t
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AHOLE1 the initial hole size in the
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IENFRA = ienfra AFLOW = aflow AHENF
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WESIG the natural logarithm of the
Page 574 and 575:
The EDMULT keyword is useful for re
Page 576 and 577:
PRBURN a keyword which invokes the
Page 578 and 579:
tfac exactly “ncells”values spe
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14.3 Cell Level Input The cell is t
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a pool layer will form in the cours
Page 584 and 585:
NSOSAT the number of safety relief
Page 586 and 587:
GASVOL = gasvol CELLHIST n hl, area
Page 588 and 589:
Presently, DCH and other nongaseous
Page 590 and 591:
xmass the mass of species “oname
Page 592 and 593:
ATMOS=3 EOI PGAS=l.0E5 TGAS=335 SAT
Page 594 and 595:
[INIDEPTH=indpth] [MINDEPTH=rnndpth
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STRUC CRANK = crank OUTGAS TRANGE t
Page 598 and 599:
kco2 eco2 QH20E = qh20e QH20B = qh2
Page 600 and 601:
cYLHn-’E the axial length of a cy
Page 602 and 603:
FORCOR1 =a3b3c3 d3 FORCOR2 =a4b4c4
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VELOCITY, REY-NUM, and NUS-FORC are
Page 606 and 607:
whether net condensation or evapora
Page 608 and 609:
cylinder. Here, RI is the cylinder
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istr hgap ICELL = icell TGAS = tgas
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14.3.1.5 Radiation. The radiation m
Page 614 and 615:
eaml EOI GASWAL = gaswal GEOBL geob
Page 616 and 617:
Table 14-1 Types of Bums Allowed fo
Page 618 and 619:
0.0376. Thekeyword CFRMNGserves the
Page 620 and 621:
DEBCONC the concentration of debris
Page 622 and 623:
14.4.1. The particle size distribut
Page 624 and 625:
14.3.1.10 Fission Product Initial C
Page 626 and 627:
FROM = marne TO = aname “mame”
Page 628 and 629:
The following keywords and associat
Page 630 and 631:
LENGFT = xleng KU1 = xku 1 KU2 = xk
Page 632 and 633:
and the DIATR4P, VELTRAP, and IL4.D
Page 634 and 635:
(data) EOIl [CONCRETE (data) EOIl (
Page 636 and 637:
EOI [Q235U=q235u] [Q238U=q238u] [Q2
Page 638 and 639:
EOI EOIl T=(times) MASS=(masses) {T
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HT-COEF NAME olay oxopt nh xhtval h
Page 642 and 643:
EOI EOI [USERSENS [{HXBOTCOR ahtb b
Page 644 and 645:
RBRCOMP ometl fmfrac EOI cmass TEMP
Page 646 and 647:
w the outside radius of the cylinde
Page 648 and 649:
SLAGSIDE a keyword which enables th
Page 650 and 651:
HBOILFLX = nhb dtsat bflx HBOILMUL
Page 652 and 653:
RHOOMUL = rhomul TSOMLT = tsomlt XE
Page 654 and 655:
DETAIL nvcons ovnam nfp ofpnam wfra
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into CONTAIN. The obsolete VANESA k
Page 658 and 659:
SOURCE nso Q-VOL HT-COEF the keywor
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smo TMETAL = tmi TOXIDE = toi LAYER
Page 662 and 663:
METALPWR the keyword to begin speci
Page 664 and 665:
14.3.3 Engineered Safety Systems Th
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iclin iclout delev now automaticall
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FCFLAR the frontal area of the fan
Page 670 and 671:
DIAMDIF the effective wire cylindri
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hxarea the effective heat transfer
Page 674 and 675:
PIPE the keyword to specify a pipe
Page 676 and 677:
EOI (oaer=na [IFLAG=ival] [AMEAN=(m
Page 678 and 679:
SOURCE nsosfp Ofp nf HOST = nhost C
Page 680 and 681:
with standard keywords. Thus the pr
Page 682 and 683:
encountered. Aerosol suspended mass
Page 684 and 685:
EOI the keyword used to terminate e
Page 686 and 687:
[PRFLOW [{ON or OFF}]] [PRAER [{ON
Page 688 and 689:
14.5.1.1 The TIMES Block in a Resta
Page 690 and 691:
AEROSOL a keyword sequence to speci
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15.0 SAMPLE PLANT CALCULATIONS In t
Page 695 and 696:
Table 15-1 Grand Gulf Input File (C
Page 697 and 698:
— o1 DRYWELL t o2 ANNULUS Figure
Page 699 and 700:
. 2 190 PO o - 170 aJ L 3 In (n a)
Page 701 and 702:
3 0 r w.- 3 0- .- _d 120 100 80 60
Page 703 and 704:
8 7 1 0 % :k I I i I I I I I I I 1
Page 705 and 706:
15.2 Surry Plant In the second samp
Page 707 and 708:
Table 15-2 Surry Input File (Contin
Page 709 and 710:
Page 711 and 712:
Page 713 and 714:
Page 715 and 716:
Page 717 and 718:
Page 719 and 720:
Page 721 and 722:
Page 723 and 724:
Page 725 and 726:
mass= O.OOOOOe+OO 1.45045e+Ol 1.438
Page 727 and 728:
3.05000e-01 eoi Table 15-2 Surry In
Page 729 and 730:
concrete in the cavity and thus the
Page 731 and 732:
500 450 400 350 300 250 200 150 100
Page 733 and 734:
-. The amount of water boiled and e
Page 735 and 736:
.- 1.0 0.9 0.8 0.7 0.6 0.5 0.4 0.3
Page 737 and 738:
c .— s o .- rn (J-J K 1 0+2 10-3
Page 739 and 740:
5.0 4.8 4.6 4.4 4.2 4.0 3.8 3.6 3.4
Page 741 and 742:
Table 15-3 Sequoyah Input File && -
Page 743 and 744:
Table 15-3 Sequoyah Input File (Con
Page 745 and 746:
2.8000e+Ol 2.8000e+Ol 2.8000e+Ol en
Page 747 and 748:
8.0500e+02 8.0650e+02 eoi feed debr
Page 749 and 750:
eoi 1.0000e+Ol 1.0000e+Ol 1.0000e+O
Page 751 and 752:
Page 753 and 754:
eoi Table 15-3 Sequoyah Input File
Page 755 and 756:
Page 757 and 758:
Page 759 and 760:
Page 761 and 762:
Page 763 and 764:
eoi 4.30918e+06 4.34125e+06 4.52691
Page 765 and 766:
Page 767 and 768:
eoi 1.55497e+07 1.58464e+07 1.65145
Page 769 and 770:
Page 771 and 772:
var-y=diatrap eoi trapping to fku &
Page 773 and 774:
Page 775 and 776:
Page 777 and 778:
o 8 w s H I E 5 UP Co L I D 3’ 4
Page 779 and 780:
Table 15-4 Sequoyah Restart Input F
Page 781 and 782:
.. Table 15-4 Sequoyah Restart Inpu
Page 783 and 784:
eoi dch-cell sdeven= 1.0 && default
Page 785 and 786:
Table 15-4 Sequoyah Restart Input F
Page 787 and 788:
compartment. The subsequent upward
Page 789 and 790:
350 I I I I I I I i I I I i 325 300
Page 791 and 792:
80 70 60 50 40 30 20 10 ? i I i / /
Page 793 and 794:
combustion as calculated by the hyd
Page 795 and 796:
16.1 Introduction 16.0 OUTPUT FILES
Page 797 and 798:
will report conditions that might h
Page 799 and 800:
To achieve this objective, POSTCON
Page 801 and 802:
typically very undescriptive, a sho
Page 803 and 804:
Table 16-1 Item Keywords (Continued
Page 805 and 806:
Page 807 and 808:
Page 809 and 810:
Page 811 and 812:
Table 16-2 Default Conversion Facto
Page 813 and 814:
16.3.4.1 Simzle Pass. For simple pr
Page 815 and 816:
16.4.1.3 Bin ary Plot File (PLTFIL)
Page 817 and 818:
16.5 COntrol Block The general stru
Page 819 and 820:
MAXSNI? keyword that initiates inpu
Page 821 and 822:
EOI termination for the entire cont
Page 823 and 824:
VECTOR ovname keyword that initiate
Page 825 and 826:
EOF keyword thatterminates theendof
Page 827 and 828:
POSTCON routine, and possibly writi
Page 829 and 830:
Three units are converted in this e
Page 831 and 832:
pltfil=plotl pout=poutl pvec=pvecl
Page 833 and 834:
&& poet snapshot vector for flag: 5
Page 835 and 836:
Figure 16-9. PMIX1 File from Exampl
Page 837 and 838:
cell=2 vector=mettmp layer=3 type=t
Page 839:
16.10.3 Output Handling When a user
Page 842 and 843:
Ben84 Ber85a Ber85b Ber86 Bi193 Bin
Page 844 and 845:
Dhi78 Din86 Dui89 Dun84 Edw73 E1w62
Page 846 and 847:
Hin82 H068 H0168 Hot67 HUS88 Ide60
Page 848 and 849:
Low82 Lui83 Lut91 Mak70 Mar86 Mas58
Page 850 and 851:
Pi195 Pi196 Pit89 Pon90 POW86 POW93
Page 852 and 853:
Sum95 Ta180 Tam85 Tarn87 Tam88 Tar8
Page 854 and 855:
was95 Wea85 Web92 Wei72 Wha78 Wi187
Page 857 and 858:
A. 1 Introduction APPENDIX A DETAIL
Page 859 and 860:
thermodynamic states. However, the
Page 861 and 862:
= h~(T) (for non-coolant liquids, s
Page 863 and 864:
(A-4) where N~X~j is the number of
Page 865 and 866:
.. in the liquid and vapor enthalpi
Page 867 and 868:
APPENDIX B 1 ALTERNATE INPUT FORMAT
Page 869 and 870:
.- AREA,i,j = area AVL,i,j = avl CF
Page 871 and 872:
n x PDAFLAG keyword discussed above
Page 873 and 874:
parameter string, the redefined val
Page 875 and 876:
RELEASE specifies nontargeted relea
Page 877 and 878:
nraycc number of rays used to model
Page 879 and 880:
ishape nslab ibc tint Chrl vufac bc
Page 881 and 882:
keywords FLAG, X, and Y are given i
Page 883 and 884:
C. 1 Introduction APPENDIX C VALIDA
Page 885 and 886:
Validation is considered outside th
Page 887 and 888:
2) Medium = prediction of prime qua
Page 889 and 890:
C.3.4 Aerosol Behavior Table C-7 pr
Page 891 and 892:
product behavior, it can be used to
Page 893 and 894:
Table C-1 CONTAIN Code Release Hist
Page 895 and 896:
Table C-3 Validation Matrix for Atm
Page 897 and 898:
Page 899 and 900:
Page 901 and 902:
Page 903 and 904:
Page 905 and 906:
Table C-4 Validation Matrix for Hea
Page 907 and 908:
Table C-5 Validation Matrix for Hea
Page 909 and 910:
I Validation Type/Basis Separate ef
Page 911 and 912:
Table C-6 Validation Matrix for DCH
Page 913 and 914:
Table C-6 Validation Matrix for DCH
Page 915 and 916:
Experiment (Test Facility) SNLJIET-
Page 917 and 918:
(Footnotes for Table C-6 Continued)
Page 919 and 920:
Table C-7 Validation Matrix for Aer
Page 921 and 922:
Table C-8 Validation Matrix for Hyd
Page 923 and 924:
Table C-10 Validation Matrix for Mi
Page 925 and 926:
n 400 ) 300 % $ 200 ~ * o 6 100 * z
Page 927 and 928:
~ ~ 0.10 0.08 g 0.06 a fn g n g 0.0
Page 929 and 930:
g 403 393 383 373 363 353 343 333 3
Page 931 and 932:
Has96b Hei86 Huh93 Jac89 Jon87 Jon8
Page 933 and 934:
Mur83b Mur88 Mur89 Mur96 0wc85 Pet9
Page 935 and 936:
Ti191 Ti196 Uch65 Va183 va188 Ver87
Page 937 and 938:
D. 1 Introduction APPENDIX D QUALIT
Page 939 and 940:
L==I-----F -—— - L I I I Desk M
Page 941 and 942:
Ir Lo! (o) Releases \ II T ata chan
Page 943 and 944:
the difilculty, resolving the issue
Page 945 and 946:
When the review is complete, the up
Page 947 and 948:
● ensures that modifications will
Page 949 and 950:
-. . ---ula GMF Program Library \ O
Page 951 and 952:
instruction set that creates the va
Page 953 and 954:
experimental results. The objective
Page 955 and 956:
D.2.6.4 Test Doc umentation. In eve
Page 957 and 958:
REFERENCES Bi194 S. C. Billups et a
Page 960:
4 QPrinted on recycled paper Federa
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