Code Manual for CONTAIN 2.0 - Federation of American Scientists

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14.3 Cell Level Input The cell is the basic calculational unit used in the code. A CONTAIN cell is intended to model an entire room, vault, compartment, etc. Difficulties may arise if the user tries to represent such a volume by more than one cell. In particular, the flow equations are not intend~d to model a continuum, and thus unrealistic flow patterns may occur within the volume. Each cell can consist of two parts: an upper cell portion containing the cell atmosphere and a number of heat transfer structures, and a lower cell portion that may include a pool, fuel debris, concrete, and various other layers. Various physical and chemical processes can occur in both the upper and lower portions of a cell. The geometry and elevation of the cell are determined by the CELLHIST input described in Section 14.3.1.1. The cell volume is assumed to be shared by the atmosphere and lower cell pool, if any. Specific input descriptions for cell level input are found in Sections 14.3.1 through 14.3.4. Upper Cell Model$. The upper cell is the collection of models that determine the behavior of the cell. Every cell must have an upper cell, though there are many situations in which a lower cell need not be specified. Heat transfer structures are optional in the upper cell, but the atmosphere is not. There are two ways to specify a floor in a cell. It can be treated as a heat transfer structure, or it can be treated as a layer in the lower cell, where it can be in contact with the atmosphere, a coolant pool, or other layers. Atmosphere source tables provide a way for the user to introduce external sources into the cell atmosphere. These source tables typically represent phenomena not modeled by CONTAIN, e.g., ~ releases from the primary system, or from core-concrete interactions if the user prefers not to use the internal CORCON/VANESA module. The quantities that can be introduced through tables include mass, heat, aerosols, and fission products. Also discussed in this section are the models for heat transfer to structures. Condensation of coolant vapor onto structures maybe modeled, along with normal dry convective heat transfer. Two levels of modeling are available regarding radiative heat transfer among the structures and the atmosphere. In conjunction with the radiation models, there are also two options available for modeling the emissivity of gas mixtures in the atmosphere. Finally, the hydrogen and carbon monoxide combustion models are discussed. Der Cel1Geometry. The upper cell geometry is determined by the CELLHIST input discussed in Section 14.3.1.1. The atmosphere volume is determined by the total volume, minus the pool volume. Note that only the coolant volume in the lower cell pool is considered to affect the free volume, even though other lower cell layers may be present and other materials may be present in the pool. Various heat transfer structures can be included to simulate roofs, walls, floors, and internal structures and equipment. The basic cell does not include any such structures automatically. They must be separately specified for each cell (see Section 14.3.1.3). If specified with an elevation, the structures’ submergence below the pool surface is treated. Rev O 14 62 6/30/97
Upper Cell AtmosDhere Initial Conditions and Sources. The user must specify the initial conditions for the atmosphere in each cell. These initial conditions can be different from one cell to the next. Given the cell atmosphere mole fractions, pressure, temperature, and volume, the code calculates the mass of each gas present. Alternatively, the user may specify the constituent masses and temperature. External sources of mass and energy can be provided to a cell atmosphere. Such sources can be useful for representing phenomena such as the blowdown of coolant from the reactor coolant system into the containment. External mass and energy source rates are specified as a function of time through tables. Atmosphere sources may consist of three types of materials: gases, coolant, dispersed debris particles (in DCH calculations). Other dispersed solids or liquids are no longer allowed except as aerosols or fission products. Materials of all three types contribute enthalpy to the atmosphere, but the ways in which their masses affect atmosphere physics are different. Gases, coolant, and debris particles are considered in both the intercell flow calculation and the atmosphere thermodynamics. In the atmosphere, the coolant is treated as a two-phase material. Therefore, sources of coolant may be either H20V or H20L. The user is cautioned not to use atmosphere source tables for aerosol materials. Aerosol sources should be specified in the cell-level aerosol AEROSOL input discussed in Section 14.3.1.8. The input needed to activate and control models that operate at the cell level in CONTAIN is addressed in the following sections. The structure of the cell input for one cell is illustrated in Figure 14-3. The entire cell level input set is repeated “ncells” times, one set for each cell defined for the problem. The present section discusses the CELL keyword and the cell level CONTROL block, which are given first and second, respectively, in the cell level input for each cell. In addition, the optional TITLE option for the cell is discussed. ***** ***** ***** ***** ***** ************************************************ CELL ncell ***** ***** ***** ***** ***** ************************************************ CELL the number of the cell to which the following input data blocks apply. = ncell The cell number is followed by the CONTROL keyword and the cell CONTROL information block. The cell CONTROL block is used to allocate storage space based on the models invoked in the cell. The storage allocation parameters should be set to reflect the models that will be used at any time in the calculation, not just what might be used at the initiation of the problem. For example, if a lower cell is specified for the cell, and it does not initially have a pool layer, but it is anticipated that Rev O 14 63 6/30/97
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Code Manual for CONTAIN 2.0: A Comp
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ABSTRACT The CONTAIN 2.0 computer c
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TABLE OF CONTENTS (CONTINUED) 4.0 A
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R O TABLE OF CONTENTS (CONTINUED) 6
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TABLE OF CONTENTS (CONTINUED) 9.1.3
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TABLE OF CONTENTS (CO NTINUED) 13.0
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TABLE OF CONTENTS (CONTINUED) 14.2.
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TABLE OF CONTENTS (CONTINUED) 16.3.
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TABLE OF CONTENTS (CONCLUDED) C.2Va
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LIST OF FIGURES (CO NTINUED) Figure
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LIST OF FIGURES (CONCLUDED) Figure
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LIST OF TABLES (CONCLUDED) Table 9-
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1.0 INTRODUCTION The CONTAIN code i
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. respond under accident conditions
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This code manual includes documenta
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The intent of this document is to p
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Table 1-3 Major New Models and Feat
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Deposition/ Agglomeration Rates Hea
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For completeness, the environment o
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ilobal Loop zstart I Input * Loed N
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Table 2-1 lists the internal timest
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where p is the structure density, C
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material definitions are given in t
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water vapor, noncondensable gases (
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2.7 Aerosol Behavior Events occurri
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In addition to these models, fissio
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2.10 Heat and Mass Transfer Through
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diffusion of water and the released
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primary system through a large ice
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Gas Liquid ● argon ● nitrogen
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Table 3-2 References for CONTAIN Ma
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● A common reference temperature,
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where u$T,P) = h$T) = ~~TcP,f(T)dT
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Table 3-3 The Coefficients Aij in E
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To ensure that the extrapolation ha
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4. AssumWion of saturated intermedi
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output after a run is completed, th
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4.0 ATMOSPHERIVPOOL THERMODYNAMIC A
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o 0 *0-0 o +F-ooo 0000 Atmosphere G
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Am An HW ❑ Ht AI * HI= Hb Figure
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connected to the respective cells.
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A side-connected path is defined as
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4.3 ~ tion The flow modeling option
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FLOW option for overcoming the gas
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Table 4-2 Conservation of Momentum
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4.4.3 User-Specified Flow Rates The
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4.4.5 Gravitational Head Modeling T
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gas center-of-volume elevations, in
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crossover parameter y always select
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interface, since in CONTAIN materia
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where dmi ~ Table 4-3 Conservation
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where Table 4-3 Conservation of Mas
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Table 4-4 Conservation of Energy Eq
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Table 4-5 Conservation of Mass Equa
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Table 4-6 Conservation of Energy Eq
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architecture. A gas-pool equilibrat
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Finally, the mass transfer rate of
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where Ap~jis the area of the atmosp
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The FIX-FLOW option may be useful i
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exit losses and other fictional los
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. Pressure: where Pi = 2 k=l Table
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CCIS are modeled through an embedde
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~ Boiling \t/ o 0: O.” 0°0000 .O
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the pool layer should lie on top of
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modeled will include the scrubbing
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ebar using the RBRCOMP keyword. Con
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aerosol release model. The allowabl
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Keyword Chemical Symbol Table 5-4 M
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The coolant pool layer is unique in
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water and regarding heat transfer a
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options is directed to the fwst nod
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5.6.2 External Lower Cell Material
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CONTAIN Code Main Modules CONTAIN I
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5.7.5 Restrictions in Mass and Ener
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Both gas-phase and condensed-phase
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decay power calculated in the DECAY
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5.8.15 Energy Conservation (2.3.12
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4. 5. 6. 7. 8. 9. imposed on it by
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6.0 DIRECT CONTAINMENT HEATING (DCH
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● ● ● “. . . . . ● ☞✍
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evolve independently of the other d
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The combined mass flow rate of gas
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where ,=W Ipgu+wi Note that when al
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‘ig,i,k _ — — ~‘jiwji$ ‘g
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entering directly into the atmosphe
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airborne particles can be neglected
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1. Conventional atmospheric source
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ecommended that the user review Ref
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The heat transfer coefficient betwe
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other versions of the Whalley-Hewit
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6.2.10.2 Entrained Fraction Correla
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and [) y+l y+l f(y) = yo”s ~ 2 (y
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ecause the desired fraction of debr
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pdv; NWe=— C! (6-71) where NW.is
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Equations (6-73) and (6-74) may all
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dmd’ ,, ~ +[+” rpv,s [1 ‘t en
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Tin = v.=— g,ln Z ‘g,ji6jiTg,jc
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An important aspect of the CONTAIN
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6.3.6 TOF/KU Trapping Model Like th
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whose default value is 0.32, p~jis
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The flight time and average velocit
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If slip is ignored completely, then
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Zr +2HZ0 + Z@z+2Hz L Fe+ H20 “ zr
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The Reynolds and Schmidt dimensionl
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D H20 = 4.40146 X 10-6 (T~~)2334 P
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.. 1-exp -~ = 0.5 [} ‘d where t~o
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AN~~, = N& 1- exp -— ‘re [{IIAt
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(AI-120)i,n= (~)~oAtC Am,j,.,,=-((A
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where ~~,i,. = (AO&hO~P&i,n) + (AH2
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calculated intercell mass flow rate
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The total radiative energy loss fro
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The velocity for non-airborne debri
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UK ~ DSolid Aerosol Water [ A Spray
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● particle scrubbing from gases v
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too small by evaporation of water.
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(7-3) where d(&(t)/dt is the time r
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This constraint thus reduces the nu
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particles can combine at a time. Th
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Except when they include significan
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Table 7-1 Comparison Between Fixed-
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Figure 7-3. Model for Water Condens
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The condensation Reference Pru78: r
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DiffusioDhoresi$. When water conden
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the user may specify these paramete
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The settling area ~ is the sum of a
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The effective cylindrical diameter
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where St is the Stokes number, the
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100 1 ()-1 10-2 1()-3 10-4 ‘\ Tot
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and Potential Flow: ELP E ll,p = =
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The efilciency E of a spray drop ch
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with enhanced scrubbing) or a small
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As an example of difficulties that
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,. - 137c~ / \ P- w 137M Ba 1 137Ba
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user. From this information, the co
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No. 7 No. 8 No. 9 No. 10 No. 11 No.
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~- ~- No. 19 l~R” —> 106Rh~ 106
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No. 28 No. 29 No. 30 No. 31 No. 32
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with the host. In such cases, the f
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103Rhbranch as in the second chain
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and B2, respectively, differing onl
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Table 8-3 Fission Product Library -
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inventory and for time-dependent so
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[Lee80] Note that array space for t
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I GAS UC Atmosphere Heat +%.OOO 00
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where t is the problem time in seco
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where V~ is the drop volume, which
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supplied by the library. Such inven
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The governing equation for the chan
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s DFB is assumed to occur whenever
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The chemical reactions that occur d
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up before ignition occurs. For exam
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delay factor is too small, the tota
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The deflagration model assumes that
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The above correlations assume only
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to occur in the bum model at a reas
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where At~,is the remaining bum time
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Specifically, for DFB to occur, the
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where NtOti= N~ + N~o + ~ is the to
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wheres, is the user-specified spont
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—’ - ● *4 / hMl Outgassing St
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prior to CONTAIN 1.2, there is cons
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except for the error introduced by
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0.1 0.08 0.06 0.04 ~ 0.02 h G o s .
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Nk = ~BLcp,BLABL h = kB~N~u/L (10-1
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unsubmerged surface of the structur
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‘=4Hpi-Hb’iF$l (10-15) e where
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to simulate forced convection throu
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10.1.3 Generalized Gas-Structure Co
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Note that the default correlations
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Because the heat and mass transfer
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0.01 0.001 0.0001 0.00001 temperatu
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0.01 0.001 0.0001 0.00001 ~emperatu
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default correlations with ones of t
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The film tracking model is discusse
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this limit would correspond to a fi
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follows the standard recommendation
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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
Page 530 and 531: NENGV = nengv NWDUDM = nwdudm NMTRA
Page 532 and 533: table may be specified after the CO
Page 534 and 535: COMPOUND keyword. Such names need n
Page 536 and 537: RHOT density values, paired with th
Page 538 and 539: correspond to the species as they a
Page 540 and 541: 14.2.4 Intercell Flows be considere
Page 542 and 543: nat the number of cell atmospheres
Page 544 and 545: cellfr the number of the cell from
Page 546 and 547: VTOPEN = vtopen TYPE = {GAS or POOL
Page 548 and 549: RVAREA-P the keyword for initiating
Page 550 and 551: NWET the number of the cell contain
Page 552 and 553: (NAME=aname [FLAG=iflag] X=n (x) VA
Page 554 and 555: keyword will result in the oversize
Page 556 and 557: SURTEN the surface tension of a wet
Page 558 and 559: newcof = 2: Coefficients are reques
Page 560 and 561: FINVT = (finvt) (8-5). If FGPPWR is
Page 562 and 563: In the input block description of t
Page 564 and 565: FDISTR = (fdistr) FDEVEN GRPLIM = g
Page 566 and 567: DIFH20 the multiplier on the mass t
Page 568 and 569: AHOLE1 the initial hole size in the
Page 570 and 571: IENFRA = ienfra AFLOW = aflow AHENF
Page 572 and 573: WESIG the natural logarithm of the
Page 574 and 575: The EDMULT keyword is useful for re
Page 576 and 577: PRBURN a keyword which invokes the
Page 578 and 579: tfac exactly “ncells”values spe
Page 582 and 583: a pool layer will form in the cours
Page 584 and 585: NSOSAT the number of safety relief
Page 586 and 587: GASVOL = gasvol CELLHIST n hl, area
Page 588 and 589: Presently, DCH and other nongaseous
Page 590 and 591: xmass the mass of species “oname
Page 592 and 593: ATMOS=3 EOI PGAS=l.0E5 TGAS=335 SAT
Page 594 and 595: [INIDEPTH=indpth] [MINDEPTH=rnndpth
Page 596 and 597: STRUC CRANK = crank OUTGAS TRANGE t
Page 598 and 599: kco2 eco2 QH20E = qh20e QH20B = qh2
Page 600 and 601: cYLHn-’E the axial length of a cy
Page 602 and 603: FORCOR1 =a3b3c3 d3 FORCOR2 =a4b4c4
Page 604 and 605: VELOCITY, REY-NUM, and NUS-FORC are
Page 606 and 607: whether net condensation or evapora
Page 608 and 609: cylinder. Here, RI is the cylinder
Page 610 and 611: istr hgap ICELL = icell TGAS = tgas
Page 612 and 613: 14.3.1.5 Radiation. The radiation m
Page 614 and 615: eaml EOI GASWAL = gaswal GEOBL geob
Page 616 and 617: Table 14-1 Types of Bums Allowed fo
Page 618 and 619: 0.0376. Thekeyword CFRMNGserves the
Page 620 and 621: DEBCONC the concentration of debris
Page 622 and 623: 14.4.1. The particle size distribut
Page 624 and 625: 14.3.1.10 Fission Product Initial C
Page 626 and 627: FROM = marne TO = aname “mame”
Page 628 and 629: The following keywords and associat
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LENGFT = xleng KU1 = xku 1 KU2 = xk
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and the DIATR4P, VELTRAP, and IL4.D
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(data) EOIl [CONCRETE (data) EOIl (
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EOI [Q235U=q235u] [Q238U=q238u] [Q2
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EOI EOIl T=(times) MASS=(masses) {T
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HT-COEF NAME olay oxopt nh xhtval h
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EOI EOI [USERSENS [{HXBOTCOR ahtb b
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RBRCOMP ometl fmfrac EOI cmass TEMP
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w the outside radius of the cylinde
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SLAGSIDE a keyword which enables th
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HBOILFLX = nhb dtsat bflx HBOILMUL
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RHOOMUL = rhomul TSOMLT = tsomlt XE
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DETAIL nvcons ovnam nfp ofpnam wfra
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into CONTAIN. The obsolete VANESA k
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SOURCE nso Q-VOL HT-COEF the keywor
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smo TMETAL = tmi TOXIDE = toi LAYER
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METALPWR the keyword to begin speci
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14.3.3 Engineered Safety Systems Th
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iclin iclout delev now automaticall
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FCFLAR the frontal area of the fan
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DIAMDIF the effective wire cylindri
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hxarea the effective heat transfer
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PIPE the keyword to specify a pipe
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EOI (oaer=na [IFLAG=ival] [AMEAN=(m
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SOURCE nsosfp Ofp nf HOST = nhost C
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with standard keywords. Thus the pr
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encountered. Aerosol suspended mass
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EOI the keyword used to terminate e
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[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
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. 2 190 PO o - 170 aJ L 3 In (n a)
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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
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15.2 Surry Plant In the second samp
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Table 15-2 Surry Input File (Contin
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Page 711 and 712:
Page 713 and 714:
Page 715 and 716:
Page 717 and 718:
Page 719 and 720:
Page 721 and 722:
Page 723 and 724:
Page 725 and 726:
mass= O.OOOOOe+OO 1.45045e+Ol 1.438
Page 727 and 728:
3.05000e-01 eoi Table 15-2 Surry In
Page 729 and 730:
concrete in the cavity and thus the
Page 731 and 732:
500 450 400 350 300 250 200 150 100
Page 733 and 734:
-. The amount of water boiled and e
Page 735 and 736:
.- 1.0 0.9 0.8 0.7 0.6 0.5 0.4 0.3
Page 737 and 738:
c .— s o .- rn (J-J K 1 0+2 10-3
Page 739 and 740:
5.0 4.8 4.6 4.4 4.2 4.0 3.8 3.6 3.4
Page 741 and 742:
Table 15-3 Sequoyah Input File && -
Page 743 and 744:
Table 15-3 Sequoyah Input File (Con
Page 745 and 746:
2.8000e+Ol 2.8000e+Ol 2.8000e+Ol en
Page 747 and 748:
8.0500e+02 8.0650e+02 eoi feed debr
Page 749 and 750:
eoi 1.0000e+Ol 1.0000e+Ol 1.0000e+O
Page 751 and 752:
Page 753 and 754:
eoi Table 15-3 Sequoyah Input File
Page 755 and 756:
Page 757 and 758:
Page 759 and 760:
Page 761 and 762:
Page 763 and 764:
eoi 4.30918e+06 4.34125e+06 4.52691
Page 765 and 766:
Page 767 and 768:
eoi 1.55497e+07 1.58464e+07 1.65145
Page 769 and 770:
Page 771 and 772:
var-y=diatrap eoi trapping to fku &
Page 773 and 774:
Page 775 and 776:
Page 777 and 778:
o 8 w s H I E 5 UP Co L I D 3’ 4
Page 779 and 780:
Table 15-4 Sequoyah Restart Input F
Page 781 and 782:
.. Table 15-4 Sequoyah Restart Inpu
Page 783 and 784:
eoi dch-cell sdeven= 1.0 && default
Page 785 and 786:
Table 15-4 Sequoyah Restart Input F
Page 787 and 788:
compartment. The subsequent upward
Page 789 and 790:
350 I I I I I I I i I I I i 325 300
Page 791 and 792:
80 70 60 50 40 30 20 10 ? i I i / /
Page 793 and 794:
combustion as calculated by the hyd
Page 795 and 796:
16.1 Introduction 16.0 OUTPUT FILES
Page 797 and 798:
will report conditions that might h
Page 799 and 800:
To achieve this objective, POSTCON
Page 801 and 802:
typically very undescriptive, a sho
Page 803 and 804:
Table 16-1 Item Keywords (Continued
Page 805 and 806:
Page 807 and 808:
Page 809 and 810:
Page 811 and 812:
Table 16-2 Default Conversion Facto
Page 813 and 814:
16.3.4.1 Simzle Pass. For simple pr
Page 815 and 816:
16.4.1.3 Bin ary Plot File (PLTFIL)
Page 817 and 818:
16.5 COntrol Block The general stru
Page 819 and 820:
MAXSNI? keyword that initiates inpu
Page 821 and 822:
EOI termination for the entire cont
Page 823 and 824:
VECTOR ovname keyword that initiate
Page 825 and 826:
EOF keyword thatterminates theendof
Page 827 and 828:
POSTCON routine, and possibly writi
Page 829 and 830:
Three units are converted in this e
Page 831 and 832:
pltfil=plotl pout=poutl pvec=pvecl
Page 833 and 834:
&& poet snapshot vector for flag: 5
Page 835 and 836:
Figure 16-9. PMIX1 File from Exampl
Page 837 and 838:
cell=2 vector=mettmp layer=3 type=t
Page 839:
16.10.3 Output Handling When a user
Page 842 and 843:
Ben84 Ber85a Ber85b Ber86 Bi193 Bin
Page 844 and 845:
Dhi78 Din86 Dui89 Dun84 Edw73 E1w62
Page 846 and 847:
Hin82 H068 H0168 Hot67 HUS88 Ide60
Page 848 and 849:
Low82 Lui83 Lut91 Mak70 Mar86 Mas58
Page 850 and 851:
Pi195 Pi196 Pit89 Pon90 POW86 POW93
Page 852 and 853:
Sum95 Ta180 Tam85 Tarn87 Tam88 Tar8
Page 854 and 855:
was95 Wea85 Web92 Wei72 Wha78 Wi187
Page 857 and 858:
A. 1 Introduction APPENDIX A DETAIL
Page 859 and 860:
thermodynamic states. However, the
Page 861 and 862:
= h~(T) (for non-coolant liquids, s
Page 863 and 864:
(A-4) where N~X~j is the number of
Page 865 and 866:
.. in the liquid and vapor enthalpi
Page 867 and 868:
APPENDIX B 1 ALTERNATE INPUT FORMAT
Page 869 and 870:
.- AREA,i,j = area AVL,i,j = avl CF
Page 871 and 872:
n x PDAFLAG keyword discussed above
Page 873 and 874:
parameter string, the redefined val
Page 875 and 876:
RELEASE specifies nontargeted relea
Page 877 and 878:
nraycc number of rays used to model
Page 879 and 880:
ishape nslab ibc tint Chrl vufac bc
Page 881 and 882:
keywords FLAG, X, and Y are given i
Page 883 and 884:
C. 1 Introduction APPENDIX C VALIDA
Page 885 and 886:
Validation is considered outside th
Page 887 and 888:
2) Medium = prediction of prime qua
Page 889 and 890:
C.3.4 Aerosol Behavior Table C-7 pr
Page 891 and 892:
product behavior, it can be used to
Page 893 and 894:
Table C-1 CONTAIN Code Release Hist
Page 895 and 896:
Table C-3 Validation Matrix for Atm
Page 897 and 898:
Page 899 and 900:
Page 901 and 902:
Page 903 and 904:
Page 905 and 906:
Table C-4 Validation Matrix for Hea
Page 907 and 908:
Table C-5 Validation Matrix for Hea
Page 909 and 910:
I Validation Type/Basis Separate ef
Page 911 and 912:
Table C-6 Validation Matrix for DCH
Page 913 and 914:
Table C-6 Validation Matrix for DCH
Page 915 and 916:
Experiment (Test Facility) SNLJIET-
Page 917 and 918:
(Footnotes for Table C-6 Continued)
Page 919 and 920:
Table C-7 Validation Matrix for Aer
Page 921 and 922:
Table C-8 Validation Matrix for Hyd
Page 923 and 924:
Table C-10 Validation Matrix for Mi
Page 925 and 926:
n 400 ) 300 % $ 200 ~ * o 6 100 * z
Page 927 and 928:
~ ~ 0.10 0.08 g 0.06 a fn g n g 0.0
Page 929 and 930:
g 403 393 383 373 363 353 343 333 3
Page 931 and 932:
Has96b Hei86 Huh93 Jac89 Jon87 Jon8
Page 933 and 934:
Mur83b Mur88 Mur89 Mur96 0wc85 Pet9
Page 935 and 936:
Ti191 Ti196 Uch65 Va183 va188 Ver87
Page 937 and 938:
D. 1 Introduction APPENDIX D QUALIT
Page 939 and 940:
L==I-----F -—— - L I I I Desk M
Page 941 and 942:
Ir Lo! (o) Releases \ II T ata chan
Page 943 and 944:
the difilculty, resolving the issue
Page 945 and 946:
When the review is complete, the up
Page 947 and 948:
● ensures that modifications will
Page 949 and 950:
-. . ---ula GMF Program Library \ O
Page 951 and 952:
instruction set that creates the va
Page 953 and 954:
experimental results. The objective
Page 955 and 956:
D.2.6.4 Test Doc umentation. In eve
Page 957 and 958:
REFERENCES Bi194 S. C. Billups et a
Page 960:
4 QPrinted on recycled paper Federa
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