Code Manual for CONTAIN 2.0 - Federation of American Scientists

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Figure C-1. 15 10 5 0 I I I I 1 I 7 8 9 10 11 12 13 Time (100 rein) Comparison <strong>of</strong> the Predicted Light Gas Concentrations in the Dome (Cell 9) in the 15- Cell Base Case with the Experimental Measurements [Mur96] Rev O C42 6/30/97
n 400 ) 300 % $ 200 ~ * o 6 100 * z -100 o ~ 101 ●* ●* — LA-4 Exp. ..- Best Estimate 1 2 3 4 5 6 1 I I 1 I I 1 I I 1 1 I lCP DAS Time+ 60 (minutes) Figure C-2. Estimated Total Heat Transfer Coefficients <strong>for</strong> the LA-4 Vessel at Location WCC2 [Ge190] R O c43 6/30/97 7 103
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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
Page 670 and 671:
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
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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
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
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14.5.1.1 The TIMES Block in a Resta
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AEROSOL a keyword sequence to speci
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15.0 SAMPLE PLANT CALCULATIONS In t
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Table 15-1 Grand Gulf Input File (C
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— 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
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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
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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:
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mass= O.OOOOOe+OO 1.45045e+Ol 1.438
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3.05000e-01 eoi Table 15-2 Surry In
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concrete in the cavity and thus the
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500 450 400 350 300 250 200 150 100
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-. The amount of water boiled and e
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.- 1.0 0.9 0.8 0.7 0.6 0.5 0.4 0.3
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c .— s o .- rn (J-J K 1 0+2 10-3
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5.0 4.8 4.6 4.4 4.2 4.0 3.8 3.6 3.4
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Table 15-3 Sequoyah Input File && -
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Table 15-3 Sequoyah Input File (Con
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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
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Page 757 and 758:
Page 759 and 760:
Page 761 and 762:
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eoi 4.30918e+06 4.34125e+06 4.52691
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Page 767 and 768:
eoi 1.55497e+07 1.58464e+07 1.65145
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var-y=diatrap eoi trapping to fku &
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Page 775 and 776:
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o 8 w s H I E 5 UP Co L I D 3’ 4
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Table 15-4 Sequoyah Restart Input F
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.. Table 15-4 Sequoyah Restart Inpu
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eoi dch-cell sdeven= 1.0 && default
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Table 15-4 Sequoyah Restart Input F
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compartment. The subsequent upward
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350 I I I I I I I i I I I i 325 300
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80 70 60 50 40 30 20 10 ? i I i / /
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combustion as calculated by the hyd
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16.1 Introduction 16.0 OUTPUT FILES
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will report conditions that might h
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To achieve this objective, POSTCON
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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 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: Table C-10 Validation Matrix for Mi
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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Code Manual for CONTAIN 2.0 - Federation of American Scientists

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