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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
- Page 24 and 25:
LIST OF TABLES (CONCLUDED) Table 9-
- Page 27 and 28: 1.0 INTRODUCTION The CONTAIN code i
- Page 29 and 30: . respond under accident conditions
- Page 31 and 32: This code manual includes documenta
- Page 33 and 34: The intent of this document is to p
- Page 35: Table 1-3 Major New Models and Feat
- Page 38 and 39: Deposition/ Agglomeration Rates Hea
- Page 40 and 41: For completeness, the environment o
- Page 42 and 43: ilobal Loop zstart I Input * Loed N
- Page 44 and 45: Table 2-1 lists the internal timest
- Page 46 and 47: where p is the structure density, C
- Page 48 and 49: material definitions are given in t
- Page 50 and 51: water vapor, noncondensable gases (
- Page 52 and 53: 2.7 Aerosol Behavior Events occurri
- Page 54 and 55: In addition to these models, fissio
- Page 56 and 57: 2.10 Heat and Mass Transfer Through
- Page 58 and 59: diffusion of water and the released
- Page 60 and 61: primary system through a large ice
- Page 62 and 63: Gas Liquid ● argon ● nitrogen
- Page 64 and 65: Table 3-2 References for CONTAIN Ma
- Page 66 and 67: ● A common reference temperature,
- Page 68 and 69: where u$T,P) = h$T) = ~~TcP,f(T)dT
- Page 70 and 71: Table 3-3 The Coefficients Aij in E
- Page 72 and 73: To ensure that the extrapolation ha
- Page 74 and 75: 4. AssumWion of saturated intermedi
- Page 76 and 77: output after a run is completed, th
- Page 80 and 81: The intercell flow of pool coolant
- Page 82 and 83: The cell geometries assumed in CONT
- Page 84 and 85: GasFlowPath PoolFlowPath Figure 4-3
- Page 86 and 87: “/ %! a—
- Page 88 and 89: Table 4-1 Definition of Inventory F
- Page 90 and 91: calculated from the terminal settli
- Page 92 and 93: Table 4-2 Conservation of Momentum
- Page 94 and 95: Table 4-2 Conservation of Momentum
- Page 96 and 97: Cell i Pi P = pressure L Aij Cell j
- Page 98 and 99: Cell 1 Cell 2 Figure 4-6. Position
- Page 100 and 101: Metastable ~ Unstable ~ ~ Stable ~
- Page 102 and 103: In the VDI model, if MSTABLE is not
- Page 104 and 105: The reader should note that the gra
- Page 106 and 107: Table 4-3 Conservation of Mass Equa
- Page 108 and 109: Table 4-4 Conservation of Energy Eq
- Page 110 and 111: ivhere Table 4-4 Conservation of En
- Page 112 and 113: where Table 4-6 Conservation of Ene
- Page 114 and 115: where Table 4-6 Conservation of Ene
- Page 116 and 117: outflow associated with the equilib
- Page 118 and 119: discussed in Section 4.4.7; and (3)
- Page 120 and 121: Ti, total gas mass W, and free volu
- Page 122 and 123: AT. = -(dT~,/dt)@l - S)/S (4-33) Th
- Page 124 and 125: 4tmosphere Internal Ener~: Table 4-
- Page 127 and 128: 5.0 LOWER CELL AND CAVITY MODELS Th
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CORCON Mod2 is used. That model doe
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. Condensate, Sprays, Melted Ice, \
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Condensate, Sprays, Melted Ice, Wat
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Table 5-1 Properties of CORCON Pred
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4 LMX Heterogeneous mixture oflight
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Table 5-3 CORCON Fission Product De
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Table 5-5 VANESA Constituent Names
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(multiple nodes are present only in
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Heat transfer between layers can be
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of the core debris in different cel
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with a discussion of the implementa
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5.7.4 Interfacing CONTAIN Aerosols
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lock. In implementations of CORCON
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● activity coefficient models for
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cell-to-structure radiation model c
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tables) is also incorporated in the
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10. 11. the melting range of the me
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the user-defined source table capab
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Table 6-1 Overview of DCH Processes
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Mass distribution provided by user
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different slip factors will not be
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where the ji sum includes only unsu
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where Ui is the internal energy in
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~‘j dU~ ,,= i “ [1 ‘ji ~j‘d
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Note that only gas is considered in
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6.2.9 Reactor Pressure Vessel (RPV)
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a~ =1- —NFr D (6-25) and N = 0.6.
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each entrainment rate model. The en
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The area term is determined from A
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[F=-lIIFWI Y ‘ log [F+IIF%+lII 1
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Table 6-2 Constants for the Tutu-Gi
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where ‘hest=[’%+’dv c1 ‘ pd
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of flow velocities in the cavity ar
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The trapping rate for the different
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6.3.2 Average Velocities The relati
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The user-specified trapping rate is
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Qualitatively, this is based on the
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considered in the TOF/KU model. The
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If the RHODG = MIX option is specif
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In calculating v~,,v~as used here,
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to the cell height if one is given
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the model is described in the third
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P~~ M~ ~ PEQ = ~T 2 BL PEQ = P H20,
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where N~~tis the amount of metal in
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drop-side limited reaction rate is
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It can be shown from Equation (6-12
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Table 6-3 DCH Chemistry Energies of
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assumed to bum instantaneously if o
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6.5.2 Radiative Heat Transfer Debri
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By default this diameter is not def
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7.0 AEROSOL BEHAVIOR MODELS The aer
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L///// 123456”7 “8” 9-10-11-1
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not taken into account.) Aerosol de
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To obtain the initial or source dis
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2b~i,t ‘F!,! 4Pi,l addition of co
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— For any sectional coefficient ~
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and J 8KTg vi=— ‘Inn1 The gravi
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therefore may not be totally conclu
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combination of the two within a giv
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is used during evaporation, the sol
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(7-17) where v~is the downward sett
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included in vtiPti The definition o
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7.5 ~ Ice The ice condenser provide
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Steel Strip (6.35mm x 1.91mm) Impac
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Kp,fL — = 0.037 N::LN;:P B P (7-3
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2. Inertial impaction, which occurs
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atmosphere very small during most o
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diffusivity being replaced by the p
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ubble wall during bubble rise can a
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the effects of the perpendicular co
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8.1 Introduction 8.0 FISSION PRODUC
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Table 8-1 Makeup of Volatility Grou
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— No. 3 No. 4 No. 5 No. 6 60mc0 9
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No. 14 No. 15 No. 16 No. 17 No. 18
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No. 25 No.26 No.27 o4 93.2% 133mT~
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Figure 8-2. No. 35 142L= ~ 142ce No
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- group number fortheradionuclide -
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1. 2. 3. Figure 8-3. / f&l Al —>
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. Note that the above example is re
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dml —=-klml+SI dt dm. ~=~ -hjmj+S
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dmi dm. — = - ri-j mi, ~ = ri-j m
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Table 8-4 Illustrative Fission Prod
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. aerosols or to the wall of the st
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CONTAIN models iodine removal from
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D12,a= DMI,a= 2.064 x 10-4T 15 P 0.
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— where the sum extends over all
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9.0 COMBUSTION MODELS The CONTAIN c
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Flame Front Propagation _/” Figur
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Table 9-1 Default Ignition and Prop
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fraction of initial combustible “
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x Planar Flame Front ----------- +!
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.. With sprays on, With sprays o~,
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of the gas ahead of the flame front
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ANco = Nco - Fco (9-18) F 02 = Nfin
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2. 3. 4. 5. 6. Sufficient oxygen is
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where the sum includes all flows en
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2. The debris temperature and mass
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10.0 HEAT AND MASS TRANSFER MODELS
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It should be noted that steam conde
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When condensation is occurring, fW.
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a cell will, in general, have a dif
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After corrections are made for temp
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o 0 Cell i 8 0 o Structure 1 ql ,Tl
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This requirement of continuous beha
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Tin = ~ Ci~,jiejilWjilTucP,u .. ‘
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As discussed in Section 10.1.3, the
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c, = 0.13 N~22 (1 + o.61N:;81p For
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N = N;u ~ + N;u Nu ( , ~1’3 ) (10
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where B,,ti, is the diffusivity (m2
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Helium is included because it frequ
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In the CONTAIN implementation, the
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Structure k Structure j Upper “Ha
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structure. Note that the film depth
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Surface 1 Film Interface 4 ( ~ Diff
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[1 ay cnc+l acne c, J, =-B,— —
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cases in which only water vapor is
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structure is invoked through the VU
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10.3.3 Radiative Properties Both th
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otherwise. The parameter ~ is defin
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Table 10-3 Coefficients for the Ces
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.— This coefficient has been fit
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When the temperature of the core de
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Figure 10-3. (Figure 10-3 shows the
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surface of a structure in another c
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fmt applied to the structure in the
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%m = %,eff (%Tlm +(’ - CW-l - G
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10.5.3 Heat Conduction Model This s
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where c is the user-specifiable imp
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For the spherical geometry where ~-
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The node effective specific heat cP
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Ji Node i xi x~ Xi+l 1 I I I I I I
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—. The bound water release is cal
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surface of a heat transfer structur
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then expanded to first order around
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11.0 BOILING WATER REACTOR MODELS T
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of flow paths. For example, the sup
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volume must be assigned to a cell.
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acceleration rates. Note that the t
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Although the number of individual v
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. For additional loss terms express
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Figure 11-5 displays various quanti
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Dtywell HOf Figure 11-6. Computatio
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where iw is the time to equilibrium
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11.2 Safetv Relief Valve (SRV) Mode
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Stage 2 accounts for the flashing b
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w _ %,out + ‘mf + ‘nc SRV,g - A
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Lii ///l\\ 41\\41\\ Sprays HI Fan C
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tables. It is activated by the keyw
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Coolant Cooled 1 Water In Atmospher
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Mechanistic Model. The mechanistic
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.=* g RTavdc Xv g - Xv ~ [. J (12-8
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Upper Plenum Ice Basket L AZ@ w Low
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upstream cell. F is equal to 1 for
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As the containment spray water drop
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where h, is the convective heat tra
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a) b) i s shell Fluid Single-pass S
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where q is the heat transfer rate,
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Counterflow Heat Exchanger Effectiv
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12.5.4 Pipes The keyword PIPE with
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Ne~lect of Momentum Convection. The
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the model for nonchoked flow when c
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No Aeroso1Deposition in Flow Paths.
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Tem~erature Dependence of Burn Para
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included in the model. The availabl
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Furthermore, the composition limits
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stagnant corners are not properly r
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Code versions earlier than CONTAIN
- Page 466 and 467:
The user should be aware that there
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introducing large “integration”
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user may find that choking arises a
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e “compartmentalized” if the pr
- Page 474 and 475:
The experiments that were analyzed
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13.3.2.2.2 Standard Prescription In
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Table 13-1 (Continued) Summary of t
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characteristic time for blowdown, ~
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10.0 8.0 6.0 4.0 2.0 .--— - PRpv,
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compartment. Hence it was judged th
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DCH Heat Transfer. In the model for
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d = 0.0464s ‘3 nad d = 0.0928 S
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@ @ Figure 13-5. @ @ @ @ @\ @ Debri
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insofar as the integral & and hydro
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Any attempt to model the effects of
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Before leaving the subject of gas c
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Examples include the annulus betwee
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13.3.2.4 Cavity Models. When using
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Levy Tutu-Ginsberg Tutu Table 13-2
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13.3.2.4.5 Discharge Coefficient. T
- Page 506 and 507:
Table 13-4 Standard Values Used in
- Page 508 and 509:
13.3.2.5.11 ENTFR. The parameter EN
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concluded that the CONTAIN mass tra
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determined from the definition of t
- Page 514 and 515:
Temperature-dependent release rates
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● Modify all global input in the
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14.0 INPUT DESCRIPTION The input ne
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CONTROL NCELLS=ncellsNTZONE=ntzoneN
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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
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NSECTN = nsectn NAC = nac NUMTBG =
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NDHGRP = ndhgrp thenumber ofdebris
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(nchlib) an optional keyword follow
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***********************************
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nvisc the number of temperature-vis
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keyword. Note that the number of ma
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***********************************
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means that the corresponding cell a
- Page 545 and 546:
The following keywords are optional
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VELEVF = velevf a pool path. The ma
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gives a time constant for the openi
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The user may choose either of two a
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COLEFF = coleff DENSTY = rho CHI =
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tables in setting the “numtbg”
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These “amean” and “avar” va
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NFPCHN nfpchn FPNAME fpname HFLIFE
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fpliq the transport efllciency fact
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-. EOI Eoq [TSTOP=tstop] [vRPvu=vrp
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DENDRP = dendrp SURTEN = surten RAD
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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
- Page 575 and 576:
and a CORCON edit time regadless of
- Page 577 and 578:
ncls PLAUTO a list of cell numbers.
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EOI GASMASS 0.02 0.0 0.0 FPMASS 0.0
- Page 581 and 582:
Upper Cell AtmosDhere Initial Condi
- Page 583 and 584:
NSOFP = nsof@ NSPFP = nspfp NAENSY
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. The cell title forms the heading
- Page 587 and 588:
“icello.” The atmosphere is mix
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The following three keywords, QUAIJ
- Page 591 and 592:
to the FDISTR input (see the DHEAT
- Page 593 and 594:
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,
- Page 607 and 608:
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
- Page 619 and 620:
MFOHZ = mfohz MFSHZ = mfshz MFCUP =
- Page 621 and 622:
SRRATE = srrate inflow to a cell, a
- Page 623 and 624:
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
- Page 637 and 638:
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
- Page 643 and 644:
e assumed to be present in the conc
- Page 645 and 646:
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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***********************************
- Page 659 and 660:
EOI EOIl [TOFSD=tofsdc] or DKPOWER
- Page 661 and 662:
CORESTAT the keyword to begin the s
- Page 663 and 664:
COMPOS nma omat pmass TEMP = ptemp
- Page 665 and 666:
EOI [FANCOOL {CONDENSE [FCQR=fcqr]
- Page 667 and 668:
14.3.3.2 Fan Cooler. Two fan cooler
- Page 669 and 670:
HITICI = hitici TMSICI = tmsici CIF
- Page 671 and 672:
EOI the keyword used to terminate i
- Page 673 and 674:
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
- Page 679 and 680:
SRVSOR input example: SRVSOR ELESRV
- Page 681 and 682:
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 &&
- Page 696 and 697:
Table 15-1 Grand Gulf Input File (C
- Page 698 and 699:
The recommended implicit flow solve
- Page 700 and 701:
400 390 380 370 a) L 350 s ~ w 340
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w.— .5 -1 -E 3’ 120 100 80 60 4
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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
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650 600 550 500 450 400 350 300 ,1
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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.
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5.8900e+03 5.8900e+03 5.8900e+03 5.
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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
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Table 15-3 Sequoyah Input File (Con
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Table 15-3 Sequoyah Input File (Con
- Page 758 and 759:
eoi 1.32323e+06 1.32591e+06 1.33000
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Table 15-3 Sequoyah Input File (Con
- Page 762 and 763:
Table 15-3 Sequoyah Input File (Con
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‘l’able 15-3 Sequoyah Input Fil
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Table 15-3 Sequoyah Input File (Con
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eoi Table 15-3 Sequoyah Input File
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Table 15-3 Sequoyah Input File (Con
- Page 772 and 773:
Table 15-3 Sequoyah Input File (Con
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dch-cell sdeven=l. O trapping tofku
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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
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Table 15-4 Sequoyah Restart Input F
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400 375 350 325 300 275 250 225 200
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-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
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c .- j!j + -c m .- 2 16 14 12 10 8
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0pltfil , I t oinput 1 CONTAIN -1
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[Sum95] and is capable of generatin
- Page 800 and 801:
Parentheses ( ) imply that the encl
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Table 16-1 Item Keywords Flag Descr
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Table 16-1 Item Keywords (Continued
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Table 16-1 Item Keywords (Continued
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Table 16-1 Item Keywords (Continued
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Table 16-1 Item Keywords (Concluded
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organized into single columns of x-
- Page 814 and 815:
programmakeplt c c this programcrea
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16.4.2 Renaming Input and Output Fi
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timax exercised as described below.
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tstop UNIT idno ouname confac tcoff
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16.6.2 Table Definition Block Input
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(a) Atmospheric Masses: MATERIAL=N2
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2. Vector names used in expressions
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1. Definin~ intermediate vectors. T
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containtest ht02 Page O heat transf
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Pagel Snapshot Profile Table: Struc
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pltfil=plotl pvec=pvecl pmix=pmixl
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pltfil=pltfj pout=poutfp pvec=pvecf
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file in a variety of combinations.
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— AAF72 Al191 Al192a Al192b Al194
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Brg81 Bro84 Bro90 Ces76 Cha39 Cha65
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Ge191 Gid77 Gid84 Gid91 G0173 Gre90
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Ker72 KOC81 Kre58 Kre73 Kum84 Kum85
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NRC90 NRC92 Owc85a 0wc85b Per73 Pet
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Ric61 Roh52 Roh73 Roh85 Rus90a Rus9
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Tou79 Tut90 Tut91 Uch65 va188 Van78
- Page 855:
Wi196 Win83 Won88 WO080 WO083 Yea38
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For purposes of the present discuss
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atmosphere and atmosphere-to-struct
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A number of reference elevations ar
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= hi,, (for enthalpy tables, k(n) =
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The energy balance condition that w
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the first seven variables in the co
- Page 870 and 871:
of -1 implies an irreversible press
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discussed in Section 4.2 prior to s
- Page 874 and 875:
nhc ehnames nfpchn fpnames hl FGPPW
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nxslab nsopl nsppl nsoatm nspatm ns
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SOURCE keyword to initiate input of
- Page 880 and 881:
B.2.4 Alternative STRUC Input Block
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This example implies at least two t
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(Because of their unwieldy nature,
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● Direct containment heating (DCH
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C.3.3 Direct Containment Heating Th
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C.4 Overall CV&A Summarv This secti
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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
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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
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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