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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
- Page 467 and 468: 13.3.1.3 Modelin~ Stratifications.
- Page 469 and 470: Figure 13-2. Two Thermal Siphon Nod
- Page 471 and 472: for the Sequoyah plant given in Cha
- Page 473 and 474: — uses CONTAIN. In any given anal
- Page 475 and 476: 0.4 0.3 0.2 0.1 (a) / ~ ..” ~ ●
- Page 477 and 478: Table 13-1 Summary of the CONTAIN S
- Page 479 and 480: 0.4 1J- 2 6.3 d# p“ RPV (13-1) He
- Page 481 and 482: 1. Use Equation (13-1) to define z~
- Page 483 and 484: In the standard prescription, the c
- Page 485 and 486: as small pipes, cabling, etc. Impac
- Page 487 and 488: esulting from homogenizing cool age
- Page 489 and 490: equivalent to that of the liquid wa
- Page 491 and 492: called “tarnping.” Since aeroso
- Page 493 and 494: Co-Eiected Primarv Svstem Water. Wa
- Page 495 and 496: .- If the initial atmosphere compos
- Page 497 and 498: hybrid solver was not available at
- Page 499 and 500: 13.3.2.3 RPV Models. When the RPV a
- Page 501 and 502: other governing input parameters. I
- Page 503 and 504: and Griffith. ~i196] In addition, t
- Page 505 and 506: several reasons, the assessment per
- Page 507 and 508: area. It is recommended that the us
- Page 509 and 510: 800 700 600 500 400 300 200 100 0 \
- Page 511 and 512: heat flow under conditions of nearl
- Page 513 and 514: dumped into a layer in a short time
- Page 515 and 516: Comments at the begiming of an inpu
- Page 517: — cannot be modeled directly. How
- Page 521 and 522: CONTROL NCELLS=ncellsNTZONE=ntzoneN
- Page 523 and 524: denotes the beginning ofadifferent
- Page 525 and 526: The ordering requirements within an
- Page 527 and 528: KEY 31.02 .03.0 OPTION2 OPTION1 EOI
- Page 529 and 530: NSECTN = nsectn NAC = nac NUMTBG =
- Page 531 and 532: NDHGRP = ndhgrp thenumber ofdebris
- Page 533 and 534: (nchlib) an optional keyword follow
- Page 535 and 536: ***********************************
- Page 537 and 538: nvisc the number of temperature-vis
- Page 539 and 540: keyword. Note that the number of ma
- Page 541 and 542: ***********************************
- Page 543 and 544: means that the corresponding cell a
- Page 545 and 546: The following keywords are optional
- Page 547 and 548: VELEVF = velevf a pool path. The ma
- Page 549 and 550: gives a time constant for the openi
- Page 551 and 552: The user may choose either of two a
- Page 553 and 554: COLEFF = coleff DENSTY = rho CHI =
- Page 555 and 556: tables in setting the “numtbg”
- Page 557 and 558: These “amean” and “avar” va
- Page 559 and 560: NFPCHN nfpchn FPNAME fpname HFLIFE
- Page 561 and 562: fpliq the transport efllciency fact
- Page 563 and 564: -. EOI Eoq [TSTOP=tstop] [vRPvu=vrp
- Page 565 and 566: DENDRP = dendrp SURTEN = surten RAD
- Page 567 and 568: TRAPRATE = trprat RPVCAV CAVITY = n
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HYDDIA = hyddia DSUBS = dsubs RHDEB
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CCENF the value of the cavity coeff
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ctmfr the ratio of the maximum allo
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and a CORCON edit time regadless of
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ncls PLAUTO a list of cell numbers.
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EOI GASMASS 0.02 0.0 0.0 FPMASS 0.0
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Upper Cell AtmosDhere Initial Condi
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NSOFP = nsof@ NSPFP = nspfp NAENSY
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. The cell title forms the heading
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“icello.” The atmosphere is mix
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The following three keywords, QUAIJ
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to the FDISTR input (see the DHEAT
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R O [SLAREA=slarea] [SLHITE=slhite]
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EOIl EOI) *************************
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TH20E tlohoe thihoe TH20B tlohob th
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— NAME = name TYPE = type SHAPE =
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. CONCDATA H20ENODE = (h20enode) H2
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The user is reminded that the defau
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invoked for the structure surface,
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FRAc = frac NAME = snarne NUMBER =
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TSURF = tsurf QSURF = qsurf if the
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With nondefault forced convection m
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Two options are available for chara
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as opposed to Modak, when using the
- Page 617 and 618:
— The discussion below refers to
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MFOHZ = mfohz MFSHZ = mfshz MFCUP =
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SRRATE = srrate inflow to a cell, a
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HOST i CHAIN = j the keyword to spe
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masses S-HOST fname mass TARGET fpn
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elements that are named “fpname.
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FROMCELL indicates the regular flow
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COOLFRAC the fraction of trapped de
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NOTE: The cell OVERFLOW option shou
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course of the calculations (or thro
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ROPT the reactor operating time pri
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TEMP = ctemp DELTA-Z = cdzin PHYSIC
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EOI the keyword used to terminate t
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e assumed to be present in the conc
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dtrnin dtmax dedit timdt GEOMETRY r
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METAL oflag nem tortm emrn SURRND o
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HX.BOTCOR ahtb bhtb chtb HXBOTMUL =
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2 the multiplier for the bubble siz
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aername the name of an aerosol comp
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cmelt Ovfp = vfpm initial oxide and
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***********************************
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EOI EOIl [TOFSD=tofsdc] or DKPOWER
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CORESTAT the keyword to begin the s
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COMPOS nma omat pmass TEMP = ptemp
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EOI [FANCOOL {CONDENSE [FCQR=fcqr]
- Page 667 and 668:
14.3.3.2 Fan Cooler. Two fan cooler
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HITICI = hitici TMSICI = tmsici CIF
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EOI the keyword used to terminate i
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VALVE the keyword to initiate the s
- Page 675 and 676:
flovht the height above pool bottom
- Page 677 and 678:
RATIO the ratio of major axis to mi
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SRVSOR input example: SRVSOR ELESRV
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T ival times MAss masses TEMP if
- Page 683 and 684:
In the input for global and cell le
- Page 685 and 686:
— in the initial run can be invok
- Page 687 and 688:
EOF EOI)] [H-BURN (data) [EOIl] [DC
- Page 689 and 690:
Example: PRFLOW OFF PRLOW-CL ON In
- Page 691:
Here they must all be specified tog
- Page 694 and 695:
Table 15-1 Grand Gulf Input File &&
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Table 15-1 Grand Gulf Input File (C
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The recommended implicit flow solve
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400 390 380 370 a) L 350 s ~ w 340
- Page 702 and 703:
w.— .5 -1 -E 3’ 120 100 80 60 4
- Page 704 and 705:
6.5 6.0 5.5 5.0 4.5 ~40 . -c -a 3.5
- Page 706 and 707:
Table 15-2 Sun-y Input File && ****
- Page 708 and 709:
Table 15-2 Surry Input File (Contin
- Page 710 and 711:
cellhist=l 0.166147309 35.3 9.53385
- Page 712 and 713:
&& 0.2 10.0 5.00 25 10 emisiv oxide
- Page 714 and 715:
Table 15-2 Surry Input File (Contin
- Page 716 and 717:
Table 15-2 Surry Input File (Contin
- Page 718 and 719:
Table 15-2 Surry Input File (Contin
- Page 720 and 721:
Table 15-2 Surry Input File (Contin
- Page 722 and 723:
Table 15-2 Sun-y Input File (Contin
- Page 724 and 725:
Table 15-2 Sun-y Input File (Contin
- Page 726 and 727:
mass= O.0 0.05103 0.0 0.0 eoi cs=4
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t t o 3 + =’ o 4 DOME ANNULUS :0
- Page 730 and 731:
n : x 350 I I I I I 1 I i I I I I I
- Page 732 and 733:
650 600 550 500 450 400 350 300 ,1
- Page 734 and 735:
o w 120 100 -20 80 60 40 20 0 I I I
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n s? 10 0 w u) a) O-J rn z La) % -!
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Except for molybdenum, masses of ai
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2.25 2.20 2.15 2.10 2.05 2.00 1.95
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esolvhd eoi Table 15-3 Sequoyah Inp
- Page 744 and 745:
2.1500e+03 2.2000e+03 2.4000e+03 2.
- Page 746 and 747:
5.8900e+03 5.8900e+03 5.8900e+03 5.
- Page 748 and 749:
eoi 2.4000e+03 2.6500e+03 condt 4.3
- Page 750 and 751:
eoi eoi 6.1613e+05 7.8267e+05 9.503
- Page 752 and 753:
mass= 0.0 471.9254 471.9254 temp= 2
- Page 754 and 755:
Table 15-3 Sequoyah Input File (Con
- Page 756 and 757:
Table 15-3 Sequoyah Input File (Con
- Page 758 and 759:
eoi 1.32323e+06 1.32591e+06 1.33000
- Page 760 and 761:
Table 15-3 Sequoyah Input File (Con
- Page 762 and 763:
Table 15-3 Sequoyah Input File (Con
- Page 764 and 765:
‘l’able 15-3 Sequoyah Input Fil
- Page 766 and 767:
Table 15-3 Sequoyah Input File (Con
- Page 768 and 769:
eoi Table 15-3 Sequoyah Input File
- Page 770 and 771:
Table 15-3 Sequoyah Input File (Con
- Page 772 and 773:
Table 15-3 Sequoyah Input File (Con
- Page 774 and 775:
dch-cell sdeven=l. O trapping tofku
- Page 776 and 777:
Table 15-3 Sequoyah Input File (Con
- Page 778 and 779:
Hydrogen combustion models are enab
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Table 15-4 Sequoyah Restart Input F
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Table 15-4 Sequoyah Restart Input F
- Page 784 and 785:
Table 15-4 Sequoyah Restart Input F
- Page 786 and 787:
400 375 350 325 300 275 250 225 200
- Page 788 and 789:
-lo 20 15 10 -5 -15 -20 5 0 I ‘?
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a) 5 (n rn al & 1.0 0.9 0.8 0.7 0.6
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600 550 500 450 400 350 300 250 200
- Page 794 and 795:
c .- j!j + -c m .- 2 16 14 12 10 8
- Page 796 and 797:
0pltfil , I t oinput 1 CONTAIN -1
- Page 798 and 799:
[Sum95] and is capable of generatin
- Page 800 and 801:
Parentheses ( ) imply that the encl
- Page 802 and 803:
Table 16-1 Item Keywords Flag Descr
- Page 804 and 805:
Table 16-1 Item Keywords (Continued
- Page 806 and 807:
Table 16-1 Item Keywords (Continued
- Page 808 and 809:
Table 16-1 Item Keywords (Continued
- Page 810 and 811:
Table 16-1 Item Keywords (Concluded
- Page 812 and 813:
organized into single columns of x-
- Page 814 and 815:
programmakeplt c c this programcrea
- Page 816 and 817:
16.4.2 Renaming Input and Output Fi
- Page 818 and 819:
timax exercised as described below.
- Page 820 and 821:
tstop UNIT idno ouname confac tcoff
- Page 822 and 823:
16.6.2 Table Definition Block Input
- Page 824 and 825:
(a) Atmospheric Masses: MATERIAL=N2
- Page 826 and 827:
2. Vector names used in expressions
- Page 828 and 829:
1. Definin~ intermediate vectors. T
- Page 830 and 831:
containtest ht02 Page O heat transf
- Page 832 and 833:
Pagel Snapshot Profile Table: Struc
- Page 834 and 835:
pltfil=plotl pvec=pvecl pmix=pmixl
- Page 836 and 837:
pltfil=pltfj pout=poutfp pvec=pvecf
- Page 838 and 839:
file in a variety of combinations.
- Page 841 and 842:
— AAF72 Al191 Al192a Al192b Al194
- Page 843 and 844:
Brg81 Bro84 Bro90 Ces76 Cha39 Cha65
- Page 845 and 846:
Ge191 Gid77 Gid84 Gid91 G0173 Gre90
- Page 847 and 848:
Ker72 KOC81 Kre58 Kre73 Kum84 Kum85
- Page 849 and 850:
NRC90 NRC92 Owc85a 0wc85b Per73 Pet
- Page 851 and 852:
Ric61 Roh52 Roh73 Roh85 Rus90a Rus9
- Page 853 and 854:
Tou79 Tut90 Tut91 Uch65 va188 Van78
- Page 855:
Wi196 Win83 Won88 WO080 WO083 Yea38
- Page 858 and 859:
For purposes of the present discuss
- Page 860 and 861:
atmosphere and atmosphere-to-struct
- Page 862 and 863:
A number of reference elevations ar
- Page 864 and 865:
= hi,, (for enthalpy tables, k(n) =
- Page 866 and 867:
The energy balance condition that w
- Page 868 and 869:
the first seven variables in the co
- Page 870 and 871:
of -1 implies an irreversible press
- Page 872 and 873:
discussed in Section 4.2 prior to s
- Page 874 and 875:
nhc ehnames nfpchn fpnames hl FGPPW
- Page 876 and 877:
nxslab nsopl nsppl nsoatm nspatm ns
- Page 878 and 879:
SOURCE keyword to initiate input of
- Page 880 and 881:
B.2.4 Alternative STRUC Input Block
- Page 882 and 883:
This example implies at least two t
- Page 884 and 885:
(Because of their unwieldy nature,
- Page 886 and 887:
● Direct containment heating (DCH
- Page 888 and 889:
C.3.3 Direct Containment Heating Th
- Page 890 and 891:
C.4 Overall CV&A Summarv This secti
- Page 892 and 893:
Table C-1 CONTAIN Code Release Hist
- Page 894 and 895:
Table C-2 Containment Test Faciliti
- Page 896 and 897:
Table C-3 Validation Matrix for Atm
- Page 898 and 899:
Table C-3 Validation Matrix for Atm
- Page 900 and 901:
Table C-3 Validation Matrix for Atm
- Page 902 and 903:
Table C-3 Validation Matrix for Atm
- Page 904 and 905:
Table C-3 Validation Matrix for Atm
- Page 906 and 907:
Table C-4 Validation Matrix for Hea
- Page 908 and 909:
Table C-5 Validation Matrix for Hea
- Page 910 and 911:
Table C-5 Validation Matrix for Hea
- Page 912 and 913:
Table C-6 Validation Matrix for DCH
- Page 914 and 915:
Table C-6 Validation Matrix for DCH
- Page 916 and 917:
Table C-6 Validation Matrix for DCH
- Page 918 and 919:
Table C-7 Validation Matrix for Aer
- Page 920 and 921:
Validation Type/Basis DEMONA/ A9 Fa
- Page 922 and 923:
Table C-9 Validation Matrix for Pre
- Page 924 and 925:
Figure C-1. 15 10 5 0 I I I I 1 I 7
- Page 926 and 927:
Figure C-3. 5000 4000 1000 0 A o CO
- Page 928 and 929:
0 Experiment — Blind Post-test =-
- Page 930 and 931:
Alm93 Amb95 Ber85 Boy95 Bra93 Din86
- Page 932 and 933:
Ka192 Kim90 Kro68 Kro78 Lan88a Lan8
- Page 934 and 935:
Sei90 Sla87 smi91 Srni92 Smi92a Smi
- Page 936 and 937:
Wi188 D. C. Williams, and D. L.Y. L
- Page 938 and 939:
The primary functions within the or
- Page 940 and 941:
up to CONTAIN 1.11, the code develo
- Page 942 and 943:
Test Problem Anomalies ~n uPROBLEM
- Page 944 and 945:
documents the proposed correction o
- Page 946 and 947:
CONTAIN Code and/or Code Manual Cha
- Page 948 and 949:
could consist either of significant
- Page 950 and 951:
Internal Beta Tester’s Report (me
- Page 952 and 953:
Key P: Complete Plan F: Freeze Code
- Page 954 and 955:
In addition to simpler calculations
- Page 956 and 957:
Table D-2 CONTAIN 2.0 Standard Test
- Page 958:
\il$FORU335 U.S. NUCLEAR REGULATORY