- Page 2: TRANSIENT BOILING AND TWO-PHASE FLO
- Page 6: ACKNOWLEDGEMENTS I would like to ex
- Page 9 and 10: parallel to the water flow. The eff
- Page 11 and 12: entrance and developed region of th
- Page 13 and 14: vni
- Page 15 and 16: II.3 II .2 II.4 II.5 II.6 II.7 II.8
- Page 17 and 18: VI.3 VI.4 VI.2.1 VI.2.2 VI.2.3 VI.2
- Page 19 and 20: high. The boiling phenomena under v
- Page 21 and 22: • under zero liquid flow rate ( i
- Page 24: CHAPTER I FORCED CONVECTIVE BOILING
- Page 27: There have been two groups of works
- Page 31 and 32: On the other hand,the instantaneous
- Page 33 and 34: - The properties were taken at film
- Page 35 and 36: In Fig.9(a) is shown the effect of
- Page 37 and 38: in a 19 mm i.d. tube with water and
- Page 39 and 40: long heater. The transient non-boil
- Page 41 and 42: shifts towards higher wall superhea
- Page 43 and 44: Figures 27(a) and (b) show the effe
- Page 45 and 46: where E is given by Eq.(8-2) E = 0
- Page 47 and 48: decreasing period and increased wit
- Page 49 and 50: gmax ,0 gmax ,st gmax ,st00 gmax ,t
- Page 51 and 52: REFERENCES 1. Rosenthal,M.W.,"An ex
- Page 53 and 54: (1954). 21. Kutateladze,S.S., Heat
- Page 55 and 56: 0 obtained by consulting a text boo
- Page 57 and 58: o Cooling Water Storage Tank Pump S
- Page 59 and 60: Fig.3 Z 10 Comparative coefficient
- Page 61 and 62: 0 E N lo' 106 105 Fig.4(b) The effe
- Page 63 and 64: E N 107 106 105 1 Fig.4(d) P = 0.14
- Page 65 and 66: Z N. m a) EX m 10 Fig.5 O 0 Compara
- Page 67 and 68: 0 N E X as E O' 15 0 0 Fig.6(b) 0.2
- Page 69 and 70: N E 2 E 0 0 Fig.6(d) 0.396 MPa 1,2
- Page 71 and 72: X Ln '-S N E }---..... } 2 E 0 0 Fi
- Page 73 and 74: Ui rn 1 N E X m E Q' 0 Fig.7(d) 1 T
- Page 75 and 76: x Ln Co N E ro E 0 Fig.8(b) 1 The v
- Page 77 and 78: 0 (N E x b E cr 15 10 0 0 Fig.9(a)
- Page 79 and 80:
j V c G 14 12 10 Fig .10 The variat
- Page 81 and 82:
E rn N rd E Cr Fig.12 7 6 5 4 3 2 1
- Page 83 and 84:
'.9 fS ~; x~ Photo.1 Steady state b
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^ CO TA 7 z D Z 10 1 0.1 \(1) (2) (
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" E cr Fig.16(b) 107 106 1o5 1 The
- Page 89 and 90:
N V 1 o 7 106 105 Fig.17(b) 1 10100
- Page 91 and 92:
E N 1 106 105 2 Fig.18(a) P=0.396 M
- Page 93 and 94:
iv 15 E x E (710 0 0.0 01 A Fig.19(
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2 X CO 20 cy 15 ro E °10 5 0 0.001
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• CO 0 cv 15 E ' E °'10 0.001 Fi
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03 N E 2 rd E o- Fig.20(a) The and
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00 E15 x rtl E 0'10 20 5 0 0.001 Fi
- Page 103 and 104:
00 2 co E o- Fig,20(e) The variatio
- Page 105 and 106:
00 CO I' rd 20 15 cr 10 5 0.0 01 Fi
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0 20 c+ 15 E x rd oor 10 5 01------
- Page 109 and 110:
Ni C15 2 20 x ro E o10 5 0 0.001 Ty
- Page 111 and 112:
20 N 15 E 2 E °r10 5 0 0.0 01 Fig.
- Page 113 and 114:
CN 20 (C" 15 E x CT 10 5 0t- 0.001
- Page 115 and 116:
CO Fig.24(d) The variation and velo
- Page 117 and 118:
0 0 0.001 Fig.25(b) 0.01 The variat
- Page 119 and 120:
O N N E 2 X rd' E 0 20 15 10 5 0 U.
- Page 121 and 122:
0E 0 -P- N 2 x g E 0' 20 15 10 0 5
- Page 123 and 124:
• O 0' N E 2 rd E ET' 20 0.01 Fig
- Page 125 and 126:
• F-' O m 0 o0.1 QIQ rd CT 4- I c
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110
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112
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of these works, the transient heat
- Page 133 and 134:
Y pendicular to the flat plate. v i
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One assumes temperature distributio
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u for x*>t*h* = -------------------
- Page 139 and 140:
value oft and is given by solving f
- Page 141 and 142:
v v Here, S is a thickness of veloc
- Page 143 and 144:
*1.5* for -ln[1-{1-exp(-5.67Pr x )}
- Page 145 and 146:
previous cases St =)76{ 1 - exp(-t*
- Page 147 and 148:
' u = (i)l/7 u~ S 1.7(69) T -TT= 1
- Page 149 and 150:
Equation (79) was derived based on
- Page 151 and 152:
The asymptotic value of the transie
- Page 153 and 154:
the transient heat flux attains the
- Page 155 and 156:
Greek Letters dtThermal boundarylay
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10. 11. 12. 13. 14. 15. 16. 17. 18
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C a) . V F-- 4- 3 ~~U -~xL . (1.;L
- Page 161 and 162:
s 10 - s \ 6- 4- 2- 0- 0.01 Slug Fl
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ON Fig.5 3 2 1 0 0.01 Thermal bound
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00 * s Fig. 6 5 4 3 2 1 0 0.01 Lami
- Page 167 and 168:
ln 0 * Fig.9 J 6 P. 4 3 2 1 0 Turbu
- Page 169 and 170:
Ln N N O I X a) CC Ln N O X (0 CD N
- Page 171 and 172:
154
- Page 173 and 174:
icantly influenced by the amount of
- Page 175 and 176:
Substituting Eqs. (3) and (4) into
- Page 177 and 178:
]]I. 3 DROPLET GENERATION BY ENTRAI
- Page 179 and 180:
In the entrainment regime of entrai
- Page 181 and 182:
Ia. 4 MEAN DROPLET SIZE AND SIZE DI
- Page 183 and 184:
and the volume fraction oversize A
- Page 185 and 186:
p-1/3u2/3 We(D ~) = 0.0099 Reg/3pgu
- Page 187 and 188:
a a. 1 a. 1W Ad A. iw CD C g C w D
- Page 189 and 190:
1. 2. 3. 4. 5. 6. 7- 8. 9. 10. 11.
- Page 191 and 192:
34. Mugele, R. A. and Ind. Eng. Che
- Page 193 and 194:
n WAVE REG Ti 0' r ION VOLUME Vw SU
- Page 195 and 196:
I pr) M M \ N CO a) a) 100 10-2 10-
- Page 197 and 198:
N Io° - J 10-1 M N CO M iCI_ CT ;:
- Page 199 and 200:
N C\J C311 us-- N) QQ CS' I 1.4 C\J
- Page 201 and 202:
C '14- cacri N C:51 N CC I0~ 10-I 1
- Page 203 and 204:
• N ~-1 M J,~-- ~ I Q. M N a) C C
- Page 205 and 206:
M rr) ..I~ N IQ Cr) CD Fig. 14. 100
- Page 207 and 208:
B I 00 NA D vm D max *_ D 10' D 20'
- Page 209 and 210:
192
- Page 211 and 212:
IV. 2 PREVIOUS WORKS In annular two
- Page 213 and 214:
it has been thought that a sufficie
- Page 215 and 216:
C = pf j Jfevq1 gvfe+ ifevg(10) or
- Page 217 and 218:
IV. 4 ENTRAINMENT RATE CORRELATION
- Page 219 and 220:
• E= 0 .022 pfjfRef-0.26E0.74_(26
- Page 221 and 222:
• uD= 6.6 x 10-7 Re0.74 Re0.185 W
- Page 223 and 224:
where the equilibrium rate is given
- Page 225 and 226:
f uD= 1.2 x 103RefReff..Reffm-0.25W
- Page 227 and 228:
f Figures 8 through 12 show the com
- Page 229 and 230:
droplet impingements and deposition
- Page 231 and 232:
where E is given by For The E = tan
- Page 233 and 234:
a W C C D E E ., g jf 'fe Jg k Ref
- Page 235 and 236:
1 2 3 4 5. 6. 7. 8. 9. 10 11 12 13
- Page 237 and 238:
29. Brodkey, R. S., "The Phenomena
- Page 239 and 240:
N 9 W 'W C) 67 -z 10 103 -4 10 105
- Page 241 and 242:
•W 0.1 0.01 0 0 0.2 Fig. 3. Entra
- Page 243 and 244:
s •w 10 1 0.1 0.01 0 0 a 0.2 Fig.
- Page 245 and 246:
.W 10 I o .) L1I 0 0.2 0.4 E/Em Fig
- Page 247 and 248:
I. _ I J w W a W 4 '4d 0.1 0.01 Fig
- Page 249 and 250:
4 E•- 1- U.! CC w w CL X w 'W I0
- Page 251 and 252:
w w 9 1.0 0.8 0.6 0.4 0.2 0.0 I.0 0
- Page 253 and 254:
1.0 0.8 0.6 04 0.2 8 0.0 1.0 0.8 0.
- Page 255 and 256:
1.0 0.8 0.6 0.4 0.2 0.0 1.0 0.8 0.6
- Page 257 and 258:
1.0 0.8 0.6 0.4 0.2 0.0 1.0 0.8 8 0
- Page 259 and 260:
1.0 0.8 0.6 0.2 0.4 I.0 0.8 8 0 .6
- Page 261 and 262:
LO 0.8 0.6 0.4 0.2 0.0 1.0 0.8 8 0.
- Page 263 and 264:
1.0 0.8 0.6 0.4 0.2 0.0 1.0 0.8 8 0
- Page 265 and 266:
. 1.0 0.8 0.4 0.2 1.0 0.8 8 0 .6 0.
- Page 267 and 268:
w 8 2.0 L8 1.6 I.4 1.2 1 .0 0.8 0.6
- Page 269 and 270:
252
- Page 271 and 272:
254
- Page 273 and 274:
satisfactory correlations which pre
- Page 275 and 276:
a j* 99 =jagOp1/4(3) 2 pg where a,
- Page 277 and 278:
P Then where Dc r 4j p)2]1/3 g the
- Page 279 and 280:
o Droplets ejected from the interfa
- Page 281 and 282:
height from the pool surface. Howev
- Page 283 and 284:
Substituting Eqs. (32) through (35)
- Page 285 and 286:
dv pfD a€-f = Ti - opgD ,(43) whe
- Page 287 and 288:
liquid level is very low, i.e., 5-6
- Page 289 and 290:
Substituting Eq. (63) into Eq. (54)
- Page 291 and 292:
and Y jr (vr+j g )dt (72) Equation
- Page 293 and 294:
Equation where vh vh (79) 0 2h* can
- Page 295 and 296:
On is the other hand, in annular-di
- Page 297 and 298:
In Fig. 6, the general trend of the
- Page 299 and 300:
* ~ • This Efg(h,jg) = 2.213 N1.5
- Page 301 and 302:
f(DJj) =C1()fl5j*1.5 D*0.5(105) gp3
- Page 303 and 304:
-4 *3 0.5p ()_1.0 Efg(h,jg) = 7.13
- Page 305 and 306:
h* = 1.038 x 103 jgN095 0.23 DH0.42
- Page 307 and 308:
E fg (h,jg ) =2. 213 N1.5D*1 jigH .
- Page 309 and 310:
(1) Total Droplet Flux- In this wor
- Page 311 and 312:
intermediate gas flux regimes given
- Page 313 and 314:
g(v. h h* hm h+ m d *qc jfe jf 'fd
- Page 315 and 316:
REFERENCES 1. Ishii, M. and Grolmes
- Page 317 and 318:
30. 31. 32. 33. 34. 35. 36. 37. 38.
- Page 319 and 320:
61 62 63 64 65 66 67 68 69 70 71 72
- Page 321 and 322:
and Here pool and Equation gas phas
- Page 323 and 324:
0 0 uJ -3 I0 -4 10 -5 10 -6 I0 104
- Page 325 and 326:
* N vt v- M Sc CP } 10 4 103 2 I0 0
- Page 327 and 328:
ca._ a cri E cl:- cv ._ > 1 .2 1 .0
- Page 329 and 330:
w Cn Cn I0 -2 -3 10 I0 -4 -5 I0 -4
- Page 331 and 332:
U../ -2 10 -3 10 -4 10 -5 I0 -4 10
- Page 333 and 334:
W -2 10 -3 10 -4 10 I05 Fig. 11. Co
- Page 335 and 336:
CP Q1 .4w I0 -2 -3 10 -4 I0 105 Fig
- Page 337 and 338:
Q, v CT W 10 I0 -2 -3 -4 I0 -5 I0 -
- Page 339 and 340:
w CP CP -2 10 I0 I0 -3 -4 -6 10 Fig
- Page 341 and 342:
• • Fig. 19. M 0 CL. a 101 100
- Page 343 and 344:
N CD -2 I0 -3 177'10 c, -4 0 cn -5
- Page 345 and 346:
w co Table II. Summary of Various E
- Page 347 and 348:
330
- Page 349 and 350:
equations. However, the same approa
- Page 351 and 352:
The U. = ui/uo Li = t./to T = t U0i
- Page 353 and 354:
where ai' asi' ted perimeter di = 4
- Page 355 and 356:
uoRu uom opqoR(pCp =gaoR2 R doR'OR(
- Page 357 and 358:
In contrast to the design parameter
- Page 359 and 360:
• R _Hydraulic Diameter Ratio diR
- Page 361 and 362:
• For A scale model can be design
- Page 363 and 364:
The similarity criteria based on th
- Page 365 and 366:
m where the total flux j is given b
- Page 367 and 368:
By assuming an axially uniform heat
- Page 369 and 370:
t _ 0 to density change. In two-pha
- Page 371 and 372:
Negligible Effects of Viscosity Rat
- Page 373 and 374:
SR gRQR d = 1 R uR (AHsub)R 1 .(102
- Page 375 and 376:
It is noted that the above conditio
- Page 377 and 378:
In the present study, only general
- Page 379 and 380:
Pr P qs Qs q„ c R Re St t T Ts Ts
- Page 381 and 382:
1. 2. 3 4 5 6 7 8. 9. • • • 1
- Page 383 and 384:
W 01 DOWN 1COMMER PUMP ,-. P1 SINGL
- Page 385 and 386:
L FROM PUMP H DOWN - COMMER UPPER C
- Page 387 and 388:
370
- Page 389 and 390:
Concerning a LOCA and subsequent re
- Page 391:
turbulent flow regime. For a two-ph