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Code Manual for CONTAIN 2.0 - Federation of American Scientists
Code Manual for CONTAIN 2.0 - Federation of American Scientists
Code Manual for CONTAIN 2.0 - Federation of American Scientists
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Concrete<br />
Air<br />
Figure 10-8. Cylindrical Structure Consisting <strong>of</strong> a Steel Liner, Air Gap, and Thick Concrete Wall<br />
R O 10 52 6/30/97
Concrete Air Figure 10-8. Cylindrical Structure Consisting <strong>of</strong> a Steel Liner, Air Gap, and Thick Concrete Wall R O 10 52 6/30/97
surface <strong>of</strong> a structure in another cell, with a conduction boundary condition, as discussed in Section 10.5.2. It maybe also be in a different cell or be isolated from all containment cells. None <strong>of</strong> these choices allows the outer surface to be treated with the full suite <strong>of</strong> models available <strong>for</strong> inner surfaces. Of the allowed models <strong>for</strong> inner surfaces, only the models <strong>for</strong> convection, condensation/evaporation, direct atnmsphere-to-stmcture radiation, specified film depth parameter, and aerosol deposition apply to those outer surfaces that are in the same cell. A structure with an outer surface in the same cell also cannot be submerged in the pool in that cell. Other modeling limitations apply to the outer surfaces that are exposed to a different cell or isolated from all cells. Such surfaces will be denoted as “external.” An external surface will be present, <strong>for</strong> example, when one structure represents the physical boundary between two compartments and each compartment is modeled as a different <strong>CONTAIN</strong> cell. A number <strong>of</strong> processes are not modeled <strong>for</strong> external surfaces: (1) surface condensation and evaporation, (2) aerosol deposition, (3) radiative heat transfer, and (4) the presence <strong>of</strong> condensate films, and (5) submergence in the pool. Finally, although convective heat transfer is modeled <strong>for</strong> external surfaces the modeling does not use the Nusselt-number correlations available <strong>for</strong> other surfaces. Instead, the heat transfer coefllcient is either specified by the user or set by default to 6.08 W/m*-K. Note that this default is a typical wall heat transfer coefficient in the turbulent natural convection regime. However, other options are available <strong>for</strong> external surface boundary conditions. These include (1) an adiabatic boundary condition or (2) a gas temperature boundary condition. (A gas temperature boundary condition simulates a surface exposed to a gas at the specified temperature.) Additional boundary conditions include (3) a heat flux boundary condition and (4) a surface temperature (as opposed to gas temperature) boundary condition. If the above outer surface modeling limitations are believed to have a significant impact, such as when condensation occurs on both surfaces <strong>of</strong> a wall that separates two cells, then it maybe better to divide the structure in half and put one half in each cell. Either an adiabatic boundary condition can be used <strong>for</strong> the outer surface <strong>of</strong> each half or a conduction boundary condition can be used. If the adiabatic boundary condition is used, no conduction <strong>of</strong> heat from one half to the other is allowed. However, if the conduction boundary condition is used, concrete outgassing presently may not be modeled (see Section 10.5.2). For many severe accident scenarios, the structures that divide compartments are sufficiently thick that the time scale <strong>of</strong> interest in the problem is much shorter than the time required <strong>for</strong> appreciable conduction <strong>of</strong> heat between compartments through walls; there<strong>for</strong>e, the limitations <strong>of</strong> an adiabatic boundary condition may not be significant. If the time scale <strong>of</strong> interest is relatively long, then a conduction boundary condition maybe used, as long as the modeling <strong>of</strong> outgassing is not required. Proper nodalization <strong>of</strong> each structure is the responsibility <strong>of</strong> the user. To determine how finely the structure should be nodalized, it maybe useful to consider the thermal diffusion length 5 defined as 5 =(4kAt/pcp~ (10-106) O 10-53 6/30/97
- Page 1 and 2:
Code Manual for CONTAIN 2.0: A Comp
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ABSTRACT The CONTAIN 2.0 computer c
- Page 6 and 7:
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
- Page 40 and 41:
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
- 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
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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
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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 79 and 80:
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
- Page 93 and 94:
Table 4-2 Conservation of Momentum
- Page 95 and 96:
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
- Page 101 and 102:
crossover parameter y always select
- Page 103 and 104:
interface, since in CONTAIN materia
- Page 105 and 106:
where dmi ~ Table 4-3 Conservation
- Page 107 and 108:
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
- Page 117 and 118:
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
- Page 132 and 133:
the pool layer should lie on top of
- Page 134 and 135:
modeled will include the scrubbing
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ebar using the RBRCOMP keyword. Con
- Page 138 and 139:
aerosol release model. The allowabl
- Page 140 and 141:
Keyword Chemical Symbol Table 5-4 M
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The coolant pool layer is unique in
- Page 144 and 145:
water and regarding heat transfer a
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options is directed to the fwst nod
- Page 148 and 149:
5.6.2 External Lower Cell Material
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CONTAIN Code Main Modules CONTAIN I
- Page 152 and 153:
5.7.5 Restrictions in Mass and Ener
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Both gas-phase and condensed-phase
- Page 156 and 157:
decay power calculated in the DECAY
- Page 158 and 159:
5.8.15 Energy Conservation (2.3.12
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4. 5. 6. 7. 8. 9. imposed on it by
- Page 163 and 164:
6.0 DIRECT CONTAINMENT HEATING (DCH
- Page 165 and 166:
● ● ● “. . . . . ● ☞✍
- Page 167 and 168:
evolve independently of the other d
- Page 169 and 170:
The combined mass flow rate of gas
- Page 171 and 172:
where ,=W Ipgu+wi Note that when al
- Page 173 and 174:
‘ig,i,k _ — — ~‘jiwji$ ‘g
- Page 175 and 176:
entering directly into the atmosphe
- Page 177 and 178:
airborne particles can be neglected
- Page 179 and 180:
1. Conventional atmospheric source
- Page 181 and 182:
ecommended that the user review Ref
- Page 183 and 184:
The heat transfer coefficient betwe
- Page 185 and 186:
other versions of the Whalley-Hewit
- Page 187 and 188:
6.2.10.2 Entrained Fraction Correla
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and [) y+l y+l f(y) = yo”s ~ 2 (y
- Page 191 and 192:
ecause the desired fraction of debr
- Page 193 and 194:
pdv; NWe=— C! (6-71) where NW.is
- Page 195 and 196:
Equations (6-73) and (6-74) may all
- Page 197 and 198:
dmd’ ,, ~ +[+” rpv,s [1 ‘t en
- Page 199 and 200:
Tin = v.=— g,ln Z ‘g,ji6jiTg,jc
- Page 201 and 202:
An important aspect of the CONTAIN
- Page 203 and 204:
6.3.6 TOF/KU Trapping Model Like th
- Page 205 and 206:
whose default value is 0.32, p~jis
- Page 207 and 208:
The flight time and average velocit
- Page 209 and 210:
If slip is ignored completely, then
- Page 211 and 212:
Zr +2HZ0 + Z@z+2Hz L Fe+ H20 “ zr
- Page 213 and 214:
The Reynolds and Schmidt dimensionl
- Page 215 and 216:
D H20 = 4.40146 X 10-6 (T~~)2334 P
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.. 1-exp -~ = 0.5 [} ‘d where t~o
- Page 219 and 220:
AN~~, = N& 1- exp -— ‘re [{IIAt
- Page 221 and 222:
(AI-120)i,n= (~)~oAtC Am,j,.,,=-((A
- Page 223 and 224:
where ~~,i,. = (AO&hO~P&i,n) + (AH2
- Page 225 and 226:
calculated intercell mass flow rate
- Page 227 and 228:
The total radiative energy loss fro
- Page 229:
The velocity for non-airborne debri
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UK ~ DSolid Aerosol Water [ A Spray
- Page 234 and 235:
● particle scrubbing from gases v
- Page 236 and 237:
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
- Page 242 and 243:
particles can combine at a time. Th
- Page 244 and 245:
Except when they include significan
- Page 246 and 247:
Table 7-1 Comparison Between Fixed-
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Figure 7-3. Model for Water Condens
- Page 250 and 251:
The condensation Reference Pru78: r
- Page 252 and 253:
DiffusioDhoresi$. When water conden
- Page 254 and 255:
the user may specify these paramete
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The settling area ~ is the sum of a
- Page 258 and 259:
The effective cylindrical diameter
- Page 260 and 261:
where St is the Stokes number, the
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100 1 ()-1 10-2 1()-3 10-4 ‘\ Tot
- Page 264 and 265:
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
- Page 270 and 271:
As an example of difficulties that
- Page 272 and 273:
,. - 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
- Page 282 and 283:
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
- Page 296 and 297:
where t is the problem time in seco
- Page 298 and 299:
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
- Page 314 and 315:
The above correlations assume only
- Page 316 and 317:
to occur in the bum model at a reas
- Page 318 and 319:
where At~,is the remaining bum time
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Specifically, for DFB to occur, the
- Page 322 and 323:
where NtOti= N~ + N~o + ~ is the to
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wheres, is the user-specified spont
- Page 326 and 327: —’ - ● *4 / hMl Outgassing St
- Page 328 and 329: prior to CONTAIN 1.2, there is cons
- Page 330 and 331: except for the error introduced by
- Page 332 and 333: 0.1 0.08 0.06 0.04 ~ 0.02 h G o s .
- Page 334 and 335: Nk = ~BLcp,BLABL h = kB~N~u/L (10-1
- Page 336 and 337: unsubmerged surface of the structur
- Page 338 and 339: ‘=4Hpi-Hb’iF$l (10-15) e where
- Page 340 and 341: to simulate forced convection throu
- Page 342 and 343: 10.1.3 Generalized Gas-Structure Co
- Page 344 and 345: Note that the default correlations
- Page 346 and 347: Because the heat and mass transfer
- Page 348 and 349: 0.01 0.001 0.0001 0.00001 temperatu
- Page 350 and 351: 0.01 0.001 0.0001 0.00001 ~emperatu
- Page 352 and 353: default correlations with ones of t
- Page 354 and 355: The film tracking model is discusse
- Page 356 and 357: this limit would correspond to a fi
- Page 358 and 359: follows the standard recommendation
- Page 360 and 361: In Equation (10-54) the relation 6
- Page 362 and 363: where N is the number of the surfac
- Page 364 and 365: X= XO-b At, AT (lo-66) where X“is
- Page 366 and 367: The ernissivity of each of the abov
- Page 368 and 369: The term ~ in Equation (10-80) is t
- Page 370 and 371: coolant subcooling. The various cor
- Page 372 and 373: If boiling is occurring at the inte
- Page 374 and 375: ‘TL.eid,s.b = ATbid + 8 AT,ub (10
- Page 378 and 379: where k is the thermal conductivity
- Page 380 and 381: T 2,eff = T2 h I,eff = hlz whereas
- Page 382 and 383: extrapolated temperature as defined
- Page 384 and 385: Distance ~ ~ Surface Node ~ Nodei F
- Page 386 and 387: The interface temperature Oihas sti
- Page 388 and 389: to be reduced in proportion to this
- Page 390 and 391: fde, TAPE17, to the effect that the
- Page 392 and 393: The outgassing of evaporable water
- Page 394 and 395: Gas Film Boundary Layer Bulk \& I A
- Page 396 and 397: interface temperature. Note that co
- Page 398 and 399: ● heat transfer between the atmos
- Page 400 and 401: Reactor Pressure Vessel Drywell Sou
- Page 402 and 403: Figure 11-2. CONTAIN Multi-Node Ven
- Page 404 and 405: L“ ●LO n ‘n I ,a ,rn n I I I
- Page 406 and 407: Table 11-1 Example Solution for Flo
- Page 408 and 409: IDrywell Water Vapor and Gas Source
- Page 410 and 411: —= dx — dt F Pq 1 2[pd - ‘w +
- Page 412 and 413: Drywell, Pd Ii P(f> Pw Vent Vd =
- Page 414 and 415: For flow from wetwell to drywell, a
- Page 416 and 417: Aeff =4 for AP > APU where ~ is the
- Page 418 and 419: the component hosting the fission p
- Page 420 and 421: noncondensable gases multiplied by
- Page 423 and 424: 12.0 ENGINEERED SAFETY FEATURE MODE
- Page 425 and 426: ~ Spray Flow Path ~~ Reinforced Con
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Inlet Manifold Cold Side Hot Side C
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other than air or superheated condi
- Page 431 and 432:
Because the total heat transferred
- Page 433 and 434:
7 Plenum t Ice Compartment 1 Accumu
- Page 435 and 436:
spring or gravity-controlled motion
- Page 437 and 438:
conditions. If “citlex” does no
- Page 439 and 440:
where p~is the atmosphere gas mixtu
- Page 441 and 442:
In these equations, N~~is the drop
- Page 443 and 444:
Figure 12-8. Th,o ~b Cold Leg (Outl
- Page 445 and 446:
The capacity-rate ratio CR is defin
- Page 447 and 448:
Note that the user-specified pump m
- Page 449 and 450:
13.0 USER GUIDANCE AND PRACTICAL AN
- Page 451 and 452:
small flow areas. Also, in the mome
- Page 453 and 454:
13.2.4 Aerosol Modeling ~t. The aer
- Page 455 and 456:
~s. The heat given off by many radi
- Page 457 and 458:
concentration in the cell maybe hig
- Page 459 and 460:
In comparisons with experimental re
- Page 461 and 462:
It is normally considered inappropr
- Page 463 and 464:
0.00016 0.00014 0.00012 0.0001 8E-0
- Page 465 and 466:
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 520 and 521:
CELL, must follow the global input.
- Page 522 and 523:
CELL 1 && beginning of input for ce
- Page 524 and 525:
In the following input descriptions
- Page 526 and 527:
A sub-block thus can begin with a l
- Page 528 and 529:
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 580 and 581:
14.3 Cell Level Input The cell is t
- Page 582 and 583:
a pool layer will form in the cours
- Page 584 and 585:
NSOSAT the number of safety relief
- Page 586 and 587:
GASVOL = gasvol CELLHIST n hl, area
- Page 588 and 589:
Presently, DCH and other nongaseous
- 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
- Page 630 and 631:
LENGFT = xleng KU1 = xku 1 KU2 = xk
- Page 632 and 633:
and the DIATR4P, VELTRAP, and IL4.D
- Page 634 and 635:
(data) EOIl [CONCRETE (data) EOIl (
- Page 636 and 637:
EOI [Q235U=q235u] [Q238U=q238u] [Q2
- Page 638 and 639:
EOI EOIl T=(times) MASS=(masses) {T
- Page 640 and 641:
HT-COEF NAME olay oxopt nh xhtval h
- Page 642 and 643:
EOI EOI [USERSENS [{HXBOTCOR ahtb b
- Page 644 and 645:
RBRCOMP ometl fmfrac EOI cmass TEMP
- Page 646 and 647:
w the outside radius of the cylinde
- Page 648 and 649:
SLAGSIDE a keyword which enables th
- Page 650 and 651:
HBOILFLX = nhb dtsat bflx HBOILMUL
- Page 652 and 653:
RHOOMUL = rhomul TSOMLT = tsomlt XE
- Page 654 and 655:
DETAIL nvcons ovnam nfp ofpnam wfra
- Page 656 and 657:
into CONTAIN. The obsolete VANESA k
- Page 658 and 659:
SOURCE nso Q-VOL HT-COEF the keywor
- Page 660 and 661:
smo TMETAL = tmi TOXIDE = toi LAYER
- Page 662 and 663:
METALPWR the keyword to begin speci
- Page 664 and 665:
14.3.3 Engineered Safety Systems Th
- Page 666 and 667:
iclin iclout delev now automaticall
- Page 668 and 669:
FCFLAR the frontal area of the fan
- Page 670 and 671:
DIAMDIF the effective wire cylindri
- Page 672 and 673:
hxarea the effective heat transfer
- Page 674 and 675:
PIPE the keyword to specify a pipe
- Page 676 and 677:
EOI (oaer=na [IFLAG=ival] [AMEAN=(m
- Page 678 and 679:
SOURCE nsosfp Ofp nf HOST = nhost C
- Page 680 and 681:
with standard keywords. Thus the pr
- Page 682 and 683:
encountered. Aerosol suspended mass
- Page 684 and 685:
EOI the keyword used to terminate e
- Page 686 and 687:
[PRFLOW [{ON or OFF}]] [PRAER [{ON
- Page 688 and 689:
14.5.1.1 The TIMES Block in a Resta
- Page 690 and 691:
AEROSOL a keyword sequence to speci
- Page 693 and 694:
15.0 SAMPLE PLANT CALCULATIONS In t
- Page 695 and 696:
Table 15-1 Grand Gulf Input File (C
- Page 697 and 698:
— o1 DRYWELL t o2 ANNULUS Figure
- Page 699 and 700:
. 2 190 PO o - 170 aJ L 3 In (n a)
- Page 701 and 702:
3 0 r w.- 3 0- .- _d 120 100 80 60
- Page 703 and 704:
8 7 1 0 % :k I I i I I I I I I I 1
- Page 705 and 706:
15.2 Surry Plant In the second samp
- Page 707 and 708:
Table 15-2 Surry Input File (Contin
- Page 709 and 710:
Table 15-2 Surry Input File (Contin
- Page 711 and 712:
Table 15-2 Surry Input File (Contin
- Page 713 and 714:
Table 15-2 Surry Input File (Contin
- Page 715 and 716:
Table 15-2 Surry Input File (Contin
- Page 717 and 718:
Table 15-2 Surry Input File (Contin
- Page 719 and 720:
Table 15-2 Surry Input File (Contin
- Page 721 and 722:
Table 15-2 Surry Input File (Contin
- Page 723 and 724:
Table 15-2 Surry Input File (Contin
- 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:
Table 15-3 Sequoyah Input File (Con
- Page 753 and 754:
eoi Table 15-3 Sequoyah Input File
- Page 755 and 756:
Table 15-3 Sequoyah Input File (Con
- Page 757 and 758:
Table 15-3 Sequoyah Input File (Con
- Page 759 and 760:
Table 15-3 Sequoyah Input File (Con
- Page 761 and 762:
Table 15-3 Sequoyah Input File (Con
- Page 763 and 764:
eoi 4.30918e+06 4.34125e+06 4.52691
- Page 765 and 766:
Table 15-3 Sequoyah Input File (Con
- Page 767 and 768:
eoi 1.55497e+07 1.58464e+07 1.65145
- Page 769 and 770:
Table 15-3 Sequoyah Input File (Con
- Page 771 and 772:
var-y=diatrap eoi trapping to fku &
- Page 773 and 774:
Table 15-3 Sequoyah Input File (Con
- Page 775 and 776:
Table 15-3 Sequoyah Input File (Con
- 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:
Table 16-1 Item Keywords (Continued
- Page 807 and 808:
Table 16-1 Item Keywords (Continued
- Page 809 and 810:
Table 16-1 Item Keywords (Continued
- 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:
Table C-3 Validation Matrix for Atm
- Page 899 and 900:
Table C-3 Validation Matrix for Atm
- Page 901 and 902:
Table C-3 Validation Matrix for Atm
- Page 903 and 904:
Table C-3 Validation Matrix for Atm
- Page 905 and 906:
Table C-4 Validation Matrix for Hea
- Page 907 and 908:
Table C-5 Validation Matrix for Hea
- Page 909 and 910:
I Validation Type/Basis Separate ef
- Page 911 and 912:
Table C-6 Validation Matrix for DCH
- Page 913 and 914:
Table C-6 Validation Matrix for DCH
- Page 915 and 916:
Experiment (Test Facility) SNLJIET-
- Page 917 and 918:
(Footnotes for Table C-6 Continued)
- Page 919 and 920:
Table C-7 Validation Matrix for Aer
- Page 921 and 922:
Table C-8 Validation Matrix for Hyd
- Page 923 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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