Code Manual for CONTAIN 2.0 - Federation of American Scientists

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—= dx — dt F Pq 1 2[pd - ‘w + g PI(I + ~)x] 1/2 [ where F is equal to ~2- 1 + (1-~)2 + IQW. By defining the integration of Equation (11-18) is carried out in the form (11-18) (11-19) where XOis the initial value of x at the beginning of the timestep, ~ is the time at the beginning of the timestep, Xq is the (non-isobaric) equilibrium position, and tw is the time to attain such an equilibrium position from the initial position. Note that equilibrium may not be attainable in the ~ present timestep. Therefore, the time to attain equilibrium tw from a non-equilibrium position XOis P ‘1P tq Pd-Pw = 2F + gpt(l + p)xo ‘2 - Pd-Pw 2F + gpl(l + fl)xq n P&32(1 +102 P& 2(1 + P)2 ‘1 At equilibrium ptg Hd + Pd = plg Hw + Pw and therefore Pw - Pd Xq = (1 + P)Pjg (1 1-20) (11-21) By applying Equation (11-21) to the second term of Equation (11-20), the time to attain equilibrium tq becomes 2F[pd - pW + g Pt(l + b)xO] 112 tq = (1 1-22) [ P@2(1 + P)z 1 Rev O 11 12 6/30/97
Figure 11-5 displays various quantities to help in understanding the logic behind the vent clearing calculation. At the beginning of the system timestep At,, the code calculates the effect of pool sources added to the suppression pool. Readjustment of H~and ~ is done, if possible, so that H~ is bounded within F$ and ~f, and so that a lies above N; where M is defined as the vent clearing height and HO~is defined as the overflow height. ~ the isobaric equilibrium height HOiSless than ~, then a bypass situation is assumed; the vent clearing calculation is bypassed; and the information is passed to the flow model with a flag indicating the bypass state. (Such a bypass state is not necessarily a likely one for typical BWR geometries and inventories.) The vent clearing time KCfor flow from drywell to wetwell is determined from Equation (11-22). The time t~~is the total time it takes to reach equilibrium from the beginning-of-timestep water levels. If this time is greater than At,, that means equilibrium is not reached at the end of the timestep. However, if H, > Xq + ~, the vent may clear before the end of the timestep. If neither happens, and the flow is from drywell to wetwell, an equation similar to Equation (11-19) is integrated over At, to determine the displacement x at the end of the timestep. This x is used as the XOfor the next timestep. To compute the vent clearing time ~,, refer to Figure 11-6a. If ~~ is above H,, and ~ > H,, then t = tq - top Vc where tOPis the time to achieve equilibrium starting at the vent opening height, and calculated by Equation (11-22), but with ~ equal to ~ - ~. Note that tOPis really fictitious because liquid flow between the @well and wetwell stops tier the drywell level drops below H,. The fraction F,Oof time during the system timestep At, that the vents are cleared is given by FVO= (( min max tO+At~- tvC,o), 1) A+ 4UL s where ~ is the time at the beginning of the timestep. (11-23) The vent clearing time when the flow is from wetwell to drywell is determined from two sets of equations. The first set describes the vent flow up to the point of overflow and the second set describes the vent flow while overflow is occurring. The effect of overflow is, of course, to remove the gravitational head of the column of liquid on the drywell side above the overflow height. The calculations t.~,tOP,and ~Cfor the case of a decreasing wetwell level are similar to those used for a decreasing drywell level. The liquid that overflows is placed in the drywell sump if modeled; otherwise it is lost from the problem. Rev O 11 13 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
Page 360 and 361: In Equation (10-54) the relation 6
Page 362 and 363: where N is the number of the surfac
Page 364 and 365: X= XO-b At, AT (lo-66) where X“is
Page 366 and 367: The ernissivity of each of the abov
Page 368 and 369: The term ~ in Equation (10-80) is t
Page 370 and 371: coolant subcooling. The various cor
Page 372 and 373: If boiling is occurring at the inte
Page 374 and 375: ‘TL.eid,s.b = ATbid + 8 AT,ub (10
Page 376 and 377: Concrete Air Figure 10-8. Cylindric
Page 378 and 379: where k is the thermal conductivity
Page 380 and 381: T 2,eff = T2 h I,eff = hlz whereas
Page 382 and 383: extrapolated temperature as defined
Page 384 and 385: Distance ~ ~ Surface Node ~ Nodei F
Page 386 and 387: The interface temperature Oihas sti
Page 388 and 389: to be reduced in proportion to this
Page 390 and 391: fde, TAPE17, to the effect that the
Page 392 and 393: The outgassing of evaporable water
Page 394 and 395: Gas Film Boundary Layer Bulk \& I A
Page 396 and 397: interface temperature. Note that co
Page 398 and 399: ● heat transfer between the atmos
Page 400 and 401: Reactor Pressure Vessel Drywell Sou
Page 402 and 403: Figure 11-2. CONTAIN Multi-Node Ven
Page 404 and 405: L“ ●LO n ‘n I ,a ,rn n I I I
Page 406 and 407: Table 11-1 Example Solution for Flo
Page 408 and 409: IDrywell Water Vapor and Gas Source
Page 412 and 413: Drywell, Pd Ii P(f> Pw Vent Vd =
Page 414 and 415: For flow from wetwell to drywell, a
Page 416 and 417: Aeff =4 for AP > APU where ~ is the
Page 418 and 419: the component hosting the fission p
Page 420 and 421: 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
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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
Page 481 and 482:
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
Page 501 and 502:
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 \
Page 511 and 512:
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
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
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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
Page 582 and 583:
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
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xmass the mass of species “oname
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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
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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
Page 612 and 613:
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
Page 656 and 657:
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
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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
Page 670 and 671:
DIAMDIF the effective wire cylindri
Page 672 and 673:
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
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with standard keywords. Thus the pr
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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
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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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