Code Manual for CONTAIN 2.0 - Federation of American Scientists

More documents

Recommendations

Info

TABLE OF CONTENTS (CO NTINUED) 13.0 USER GUIDANCE AND PRACTICAL AND CAUTIONARY ADVICE . . . . . . . . . . 13-1 13.1 Key Simpli&ing Assumptions in CO~~ . . . . . . . . . . . . . . . . . . . . . . . . . . . 13-1 13.2 Specific Model Limitations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ...13-2 13.2.1 Atmosphere/Pool Thermodynamics and Intercell Flow . . . . . . . . . . . . 13-2 13.2.2 Lower Cell Modeling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. 13-3 13.2.3 DCHModeling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13-3 13.2.4 Aerosol Modeling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ...13-5 13.2.5 Fission Product Modeling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13-6 13.2.6 Combustion Modeling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. 13-7 13.2.6.1 Deflagration Model . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ...13-7 13.2.6.2. Diffusion Flame Burn (DFB) Model . . . . . . . . . . . . . . . . . 13-11 13.2.6.3 Bulk Spontaneous Reaction (BSR) Model . . . . . . . . . . . . . 13-12 13.2.7 Heatand Mass Transfer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ...13-13 13.2.8 Engineered System Modeling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13-16 13.2.9 Calculational Sequence Effects . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13-17 13.3 Practical Suggestions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ...13-17 13.3.1 Atmosphere/Pool Thermodynamics and Intercell Flow . . . . . . . . . . . 13-17 13.3.1.1 Optimizing Multicell Calculations . . . . . . . . . . . . . . . . . . . 13-17 13.3.1.2 Modeling of Suspended Liquid Coolant . . . . . . . . . . . . . . . 13-17 13.3.1.3 Modeling Stratifications . . . . . . . . . . . . . . . . . . . . . . . . . . . 13-19 13.3.1.4 Choked Flowat Less Thanthe Critical Pressure Difference 13-20 # 13.3.1.5 Modeling the Outside Environment . . . . . . . . . . . . . . . . . . 13-22 13.3.1.6 Atmosphere and Lower Cell Source Tables . . . . . . . . . . . . 13-22 13.3.2 DCH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ...13-22 13.3.2.1 General Considerations . . . . . . . . . . . . . . . . . . . . . . . . . . ..l3.22 13.3.2.2 The Standard Input Prescription for DCHCalculations . . . 13-24 13.3.2.2.1 Philosophical Basis and Purpose of the Standa.rd Prescription . . . . . . . . . . . . . . . . . . . . . . . . ...13-24 13.3.2.2.2 Standard Prescription Input and Model Choices . 13-28 13.3.2 .3 RPVModels . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ...13-51 13.3.2 .3.1 Hole Ablation . . . . . . . . . . . . . . . . . . . . . . . . . ...13-51 13.3.2 .3.2 Gas Blowthrough . . . . . . . . . . . . . . . . . . . . . . ...13-51 13.3.2 .4 Cavity Models . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ...13-52 13.3.2 .4.1 Entrainment Rate . . . . . . . . . . . . . . . . . . . . . . ...13-52 13.3.2 .4.2 Entrained Fraction . . . . . . . . . . . . . . . . . . . . . . . . 13-52 13.3.2.4.3 Cavity Constant &(CCENFand CCENR) . . . . . 13-53 13.3.2.4.4 Cavity Geometry Parameters . . . . . . . . . . . . . . . . 13-55 13.3.2.4.5 Discharge Coefficient . . . . . . . . . . . . . . . . . . . . . 13-56 13.3.2 .4.6 Levy Standard Values . . . . . . . . . . . . . . . . . . . . . 13-56 13.3.2.4.7 Whalley-Hewitt Standard Value . . . . . . . . . . . . . 13-57 13.3.2 .4.8 Weber Model . . . . . . . . . . . . . . . . . . . . . . . . . ...13-57 R O ii
TABLE OF CONTENTS (CONTINUED) 13.3.2.5 Specific Input Parameters for RPV and Cavity Models . . . 13-58 13.3.2 .5.1 AHOLE1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ...13-58 13.3.2 .5.2 CPWALL . . . . . . . . . . . . . . . . . . . . . . . . . . . . ...13-58 13.3.2.5 .3 CSUBD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ...13-58 13.3.2.5 .4 RHOWAL . . . . . . . . . . . . . . . . . . . . . . . . . . . ...13-58 13.3.2.5 .5 AFILM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ...13-58 13.3.2 .5.6 HYDDIA . . . . . . . . . . . . . . . . . . . . . . . . . . . . ...13-59 13.3.2 .5.7 WETPER . . . . . . . . . . . . . . . . . . . . . . . . . . . . ...13-59 13.3.2 .5.8 TDISP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ...13-59 13.3.2 .5.9 TSTOP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ...13-59 13.3.2.5 .1OCCENF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ...13-59 13.3.2 .5.11 ENTFR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ...13-60 13.3.3 Heatand Mass Transfer. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ...13-60 13.3.3.1 ApproximatingtheUchidaHeatTransfer Data . . . . . . . . . 13-60 13.3.3.2 Approximating CondenserTubes . . . . . . . . . . . . . . . . . . . . 13-62 13.3.3.3 ApproximatingBoilingHeat Transfer . . . . . . . . . . . . . . . . 13-63 13.3.3.4 FilmFlow Overan EllipsoidalDome Shell . . . . . . . . . . . . 13-63 13.3.3.5 Hints for StructureNarningand Ordering . . . . . . . . . . . . . . 13-64 13.3.3.6 Simulating Quenching Phenomena andSteamSpikes . . . . 13-64 13.3.4 Miscellaneous . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ...13-65 13.3.4.1 Fission Product Mass Effects . . . . . . . . . . . . . . . . . . . . . . . 13-65 13.3.4.2 Simulation ofPool ScrubbingofElemental Iodine . . . . . . 13-65 13.3.4.3 Multiple Sources for a Single Species . . . . . . . . . . . . . . . . 13-66 13.3.4.4 Restarts . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ...13-66 13.3.4.5 AnnotatedInput . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ...13-66 13.3.4.6 Hints for Collapsing Multi-Cell Input Files . . . . . . . . . . . . 13-67 13.3.4.7 Role of Sensitivity Calculations in Building Input Files . . 13-68 13.3.4.8 Spray Modeling Suggestions . . . . . . . . . . . . . . . . . . . . . . . . 13-68 14.O INPUT DESCRIPTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ...14-1 14.1 General Input Format and Structure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ...14-1 14.1.1 Ordering Requirements inInputBlocks . . . . . . . . . . . . . . . . . . . . . . . 14-6 14.2 GlobalL.evelInput . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ...14-9 14.2.1 Material, Fission Product, andAerosol Names . . . . . . . . . . . . . . . . . 14-13 14.2.1.1 User-DefinedMaterial Definition . . . . . . . . . . . . . . . . . . . . 14-16 14.2.1.2 DCHUser-DefinedMaterial Input . . . . . . . . . . . . . . . . . . . 14-19 14.2.2 Mass and EnergyAccounting . . . . . . . . . . . . . . . . . . . . . . . . . . . . ..14-20 14.2.3 Fixed Atmosphere Conditions . . . . . . . . . . . . . . . . . . . . . . . . . . . ...14-21 R O ... Xlll 6/30/97
Page 1 and 2: Code Manual for CONTAIN 2.0: A Comp
Page 3: ABSTRACT The CONTAIN 2.0 computer c
Page 6 and 7: TABLE OF CONTENTS (CONTINUED) 4.0 A
Page 8 and 9: R O TABLE OF CONTENTS (CONTINUED) 6
Page 10 and 11: TABLE OF CONTENTS (CONTINUED) 9.1.3
Page 14 and 15: TABLE OF CONTENTS (CONTINUED) 14.2.
Page 16 and 17: TABLE OF CONTENTS (CONTINUED) 16.3.
Page 18 and 19: TABLE OF CONTENTS (CONCLUDED) C.2Va
Page 20 and 21: LIST OF FIGURES (CO NTINUED) Figure
Page 22 and 23: 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 79 and 80:
4.0 ATMOSPHERIVPOOL THERMODYNAMIC A
Page 81 and 82:
o 0 *0-0 o +F-ooo 0000 Atmosphere G
Page 83 and 84:
Am An HW ❑ Ht AI * HI= Hb Figure
Page 85 and 86:
connected to the respective cells.
Page 87 and 88:
A side-connected path is defined as
Page 89 and 90:
4.3 ~ tion The flow modeling option
Page 91 and 92:
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
Page 97 and 98:
4.4.5 Gravitational Head Modeling T
Page 99 and 100:
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
Page 109 and 110:
Table 4-4 Conservation of Energy Eq
Page 111 and 112:
Table 4-5 Conservation of Mass Equa
Page 113 and 114:
Table 4-6 Conservation of Energy Eq
Page 115 and 116:
architecture. A gas-pool equilibrat
Page 117 and 118:
Finally, the mass transfer rate of
Page 119 and 120:
where Ap~jis the area of the atmosp
Page 121 and 122:
The FIX-FLOW option may be useful i
Page 123 and 124:
exit losses and other fictional los
Page 125:
. Pressure: where Pi = 2 k=l Table
Page 128 and 129:
CCIS are modeled through an embedde
Page 130 and 131:
~ 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
Page 136 and 137:
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
Page 142 and 143:
The coolant pool layer is unique in
Page 144 and 145:
water and regarding heat transfer a
Page 146 and 147:
options is directed to the fwst nod
Page 148 and 149:
5.6.2 External Lower Cell Material
Page 150 and 151:
CONTAIN Code Main Modules CONTAIN I
Page 152 and 153:
5.7.5 Restrictions in Mass and Ener
Page 154 and 155:
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
Page 160 and 161:
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
Page 189 and 190:
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
Page 217 and 218:
.. 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
Page 232 and 233:
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.
Page 238 and 239:
(7-3) where d(&(t)/dt is the time r
Page 240 and 241:
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-
Page 248 and 249:
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
Page 256 and 257:
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
Page 262 and 263:
100 1 ()-1 10-2 1()-3 10-4 ‘\ Tot
Page 264 and 265:
and Potential Flow: ELP E ll,p = =
Page 266 and 267:
The efilciency E of a spray drop ch
Page 268 and 269:
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
Page 274 and 275:
user. From this information, the co
Page 276 and 277:
No. 7 No. 8 No. 9 No. 10 No. 11 No.
Page 278 and 279:
~- ~- No. 19 l~R” —> 106Rh~ 106
Page 280 and 281:
No. 28 No. 29 No. 30 No. 31 No. 32
Page 282 and 283:
with the host. In such cases, the f
Page 284 and 285:
103Rhbranch as in the second chain
Page 286 and 287:
and B2, respectively, differing onl
Page 288 and 289:
Table 8-3 Fission Product Library -
Page 290 and 291:
inventory and for time-dependent so
Page 292 and 293:
[Lee80] Note that array space for t
Page 294 and 295:
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
Page 300 and 301:
supplied by the library. Such inven
Page 302 and 303:
The governing equation for the chan
Page 304 and 305:
s DFB is assumed to occur whenever
Page 306 and 307:
The chemical reactions that occur d
Page 308 and 309:
up before ignition occurs. For exam
Page 310 and 311:
delay factor is too small, the tota
Page 312 and 313:
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
Page 320 and 321:
Specifically, for DFB to occur, the
Page 322 and 323:
where NtOti= N~ + N~o + ~ is the to
Page 324 and 325:
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 376 and 377:
Concrete Air Figure 10-8. Cylindric
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
Page 427 and 428:
Inlet Manifold Cold Side Hot Side C
Page 429 and 430:
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:
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
show all

Code Manual for CONTAIN 2.0 - Federation of American Scientists

Create successful ePaper yourself

Delete template?

Save as template?