Code Manual for CONTAIN 2.0 - Federation of American Scientists

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Hydrogen combustion models are enabled in the H-BURN block, including the options. Igniters are assumed to be operationalbut they are presentonly in Cells2, 5, and 6; bums initiated in these cells may propagate into other cells if conditions are suitable. Although the igniters are assumed to be operating, it is also assumed that no igniter is suftlciently close to the incoming hydrogen sources to ignite the incoming flows and hence a diffusion flame burn (DFB) is assumed to occur only if the incoming flow is sufficiently hot to autoignite (DFT’EMP = 1000). In Cell 2, the DFB model is suppressed prior to vessel breach by specifying an impossible ignition criterion (MFOCB = 0.9) because the DFTEMP temperature threshold is not applied to source tables; i. e., it only applies to incoming flows from another computational cell. After vessel breach, hydrogen bum parameters are reset to values appropriate for DCH, as noted previously. For DCH calculations, the user must specify the names and properties of core debris materials that can be present. These parameters are given in the USERDEF and USERDAT options block. Global specifications for DCH are given in the DHEAT block. The drop diameter for each debris field is specified individually following the DIABIN keyword. The mass distribution to bins is specified in the FDISTR block. The remaining input keywords in the DHEAT block apply to radiative and convective heat transfer, mass transfer, and irordsteam chemical equilibrium. The values specified in the DHEAT block are used for all cells since they are not overridden in the cell-level DCH-CELL blocks. Other DCH parameters that are specific to each cell are specified under the DCH-CELL blocks. In this sample problem, vessel breach is assumed to occur at 33,000s. Because the hydrogen bum parameters appropriate prior to vessel breach are not appropriate during DCH, the calculations were stopped at the time of vessel breach and restarted with the hydrogen bum parameters set to values considered to be suitable for the DCH calculation. Though there are some minor variations, the DCH-related input closely follows the standardized DCH input prescription summarized in Section 13.3.2.2. Although the DCH event begins at 33,000s, debris sources are also specified in the initial input file to reserve the arrays for the restart run. The debris sources defined in the restart input file are the ones actually used in the calculation. The accompanying restart input file for the initial input file is listed in Table 15-4. With the exception of the primary system cell, all the cells start with a saturated steam/air mixture in the atmosphere at 100 kpa. The primary system is pressurized to 8.0 MPa at a temperature of 1000 K. Pools defined in Cells 1,2,4, and 6 are initially dry. In the present accident scenario, it is assumed that 10,000 kg of water overlie the melt in the RPV. CONTAIN cannot model this configuration explicitly. However, some of the potential effects of the water being co-ejected with the debris are modeled by introducing a user-defined source of H20V with the appropriate enthalpy in parallel with the airborne debris sources. Pressure-time histories for the containment cells are plotted in Figure 15-19 for the time period prior to vessel breach. There are many small pressure spikes and two larger ones corresponding to hydrogen bums. Aside from the hydrogen bums, there is an initial fairly rapid pressure rise at approximately 5000 s as steam enters the lower compartment and forces the air into the upper Rev. O 15-86 6/30/97
Table 15-4 Sequoyah Restart Input File restart && Restart deck for restarting at vessel breach (33000 s) with && hydrogen burn pareuneters changed to values appropriate && for DCH && && Ice Condenser and DCH Sample Input Deck && _____edit tlme~-----------------------------------------times l.Oe10 33000.0 && standard restart time --- 2.0 500.0 1000.0 && 5.0 500.0 6000.0 && 5.0 200.0 20000.0 5.0 200.0 32995.0 5.0 5.0 33000.0 0.0010 0.10 33001.0 0.0010 0.20 33009.0 0.002 0.2 33015.0 0.005 0.5 33020.0 0.01 1.0 33030.0 && --------------------------------------------------------- 1.00 1.00 1.00 1.00 1.00 1.00 1.00 1.00 1.00 trestart 5 10000.0 23000.0 33000.0 33005.0 33009.0 && fewer restarts edmult=10000O.O && avoid excessive output from h-burns during DCH shortedt=ll && ----------------------------------------------------------- && dheat block is not changed in this restart, except ‘gassur’ && ----------------------------------------------------------- dheat diabin && Log-normal, geom. std. dev=4, 5 size group 0.1692e-3 0.4834e-3 1.e-3 2.069e-3 5.911e-3 fdistr && species assignment to bins && fed zrd feed zro2d uo2d crd croxd nid 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.4 0.4 0.4 0.4 0.4 0.4 0.4 0.4 0.2 0.2 0.2 0.2 0.2 0.2 0.2 0.2 0.2 0.2 0.2 0.2 0.2 0.2 0.2 0.2 0.2 0.2 0.2 0.2 0.2 0.2 0.2 0.2 radgas=O.8 && radiation blackbody multiplier between the debris and && the atmosphere in all cells, std. (standard) input radmul=O.O && radiation blackbody multiplier between the debris and && the structure surfaces in all cells, std. dch input difo2=l.O && multiplier on the mass transfer coeff. for oxygen tranport && to surfaces of drops, default difh20=l.O && multiplier on the mass transfer coeff. for steam tranport && to surfaces of drops, default htcmul=l.O && multiplier on the convective heat transfer between drops && and the atmosphere, default ieqopt=2 && standard treatment for iron/steam equilibrium && default, 2 : evaluate using the mole fraction of Feo thresh=273.15 && temperature cutoff for chemical reactions, std. dch input rcomh2=on && hydrogen recombination, default gassur=O.8 && gas to surface emissivity to use on restart eoi cell=l atmos && ----–------direct heat sources--------------------------- && debris source source=17 Rev O 15 87
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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
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12.0 ENGINEERED SAFETY FEATURE MODE
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~ Spray Flow Path ~~ Reinforced Con
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Inlet Manifold Cold Side Hot Side C
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other than air or superheated condi
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Because the total heat transferred
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7 Plenum t Ice Compartment 1 Accumu
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spring or gravity-controlled motion
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conditions. If “citlex” does no
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where p~is the atmosphere gas mixtu
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In these equations, N~~is the drop
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Figure 12-8. Th,o ~b Cold Leg (Outl
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The capacity-rate ratio CR is defin
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Note that the user-specified pump m
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13.0 USER GUIDANCE AND PRACTICAL AN
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small flow areas. Also, in the mome
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13.2.4 Aerosol Modeling ~t. The aer
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~s. The heat given off by many radi
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concentration in the cell maybe hig
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In comparisons with experimental re
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It is normally considered inappropr
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0.00016 0.00014 0.00012 0.0001 8E-0
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13.2.9 Calculational Sequence Effec
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13.3.1.3 Modelin~ Stratifications.
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Figure 13-2. Two Thermal Siphon Nod
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for the Sequoyah plant given in Cha
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— uses CONTAIN. In any given anal
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0.4 0.3 0.2 0.1 (a) / ~ ..” ~ ●
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Table 13-1 Summary of the CONTAIN S
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0.4 1J- 2 6.3 d# p“ RPV (13-1) He
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1. Use Equation (13-1) to define z~
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In the standard prescription, the c
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as small pipes, cabling, etc. Impac
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esulting from homogenizing cool age
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equivalent to that of the liquid wa
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called “tarnping.” Since aeroso
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Co-Eiected Primarv Svstem Water. Wa
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.- If the initial atmosphere compos
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hybrid solver was not available at
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13.3.2.3 RPV Models. When the RPV a
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other governing input parameters. I
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and Griffith. ~i196] In addition, t
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several reasons, the assessment per
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area. It is recommended that the us
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800 700 600 500 400 300 200 100 0 \
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heat flow under conditions of nearl
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dumped into a layer in a short time
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Comments at the begiming of an inpu
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— cannot be modeled directly. How
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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
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SURTEN the surface tension of a wet
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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
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The EDMULT keyword is useful for re
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PRBURN a keyword which invokes the
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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
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NSOSAT the number of safety relief
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GASVOL = gasvol CELLHIST n hl, area
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Presently, DCH and other nongaseous
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xmass the mass of species “oname
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ATMOS=3 EOI PGAS=l.0E5 TGAS=335 SAT
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[INIDEPTH=indpth] [MINDEPTH=rnndpth
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STRUC CRANK = crank OUTGAS TRANGE t
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kco2 eco2 QH20E = qh20e QH20B = qh2
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cYLHn-’E the axial length of a cy
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FORCOR1 =a3b3c3 d3 FORCOR2 =a4b4c4
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VELOCITY, REY-NUM, and NUS-FORC are
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whether net condensation or evapora
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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
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eaml EOI GASWAL = gaswal GEOBL geob
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Table 14-1 Types of Bums Allowed fo
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0.0376. Thekeyword CFRMNGserves the
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DEBCONC the concentration of debris
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14.4.1. The particle size distribut
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14.3.1.10 Fission Product Initial C
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FROM = marne TO = aname “mame”
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The following keywords and associat
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LENGFT = xleng KU1 = xku 1 KU2 = xk
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and the DIATR4P, VELTRAP, and IL4.D
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(data) EOIl [CONCRETE (data) EOIl (
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EOI [Q235U=q235u] [Q238U=q238u] [Q2
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EOI EOIl T=(times) MASS=(masses) {T
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HT-COEF NAME olay oxopt nh xhtval h
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EOI EOI [USERSENS [{HXBOTCOR ahtb b
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RBRCOMP ometl fmfrac EOI cmass TEMP
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w the outside radius of the cylinde
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SLAGSIDE a keyword which enables th
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HBOILFLX = nhb dtsat bflx HBOILMUL
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RHOOMUL = rhomul TSOMLT = tsomlt XE
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DETAIL nvcons ovnam nfp ofpnam wfra
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into CONTAIN. The obsolete VANESA k
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SOURCE nso Q-VOL HT-COEF the keywor
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smo TMETAL = tmi TOXIDE = toi LAYER
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METALPWR the keyword to begin speci
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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
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DIAMDIF the effective wire cylindri
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hxarea the effective heat transfer
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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
Page 693 and 694:
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 753 and 754: eoi Table 15-3 Sequoyah Input File
Page 763 and 764: eoi 4.30918e+06 4.34125e+06 4.52691
Page 767 and 768: eoi 1.55497e+07 1.58464e+07 1.65145
Page 771 and 772: var-y=diatrap eoi trapping to fku &
Page 777: o 8 w s H I E 5 UP Co L I D 3’ 4
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 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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