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Table 11.3  Properties of saturated water (Meyer et al., 1993; Harvey et al., 2000; IAPWS, 1994).

T

p

ρf

hfg

cpf

f × 106

kf × 103

Prf

σ × 103

βf × 106

(K)

(bar)

(kg/m3)

(kJ/kg)

(kJ/kg K)

(Ns/m2)

(W/mK)

 

(N/m)

(K–1)

273.16

0.006177

999.8

2502

4.22

1790.6

561

13.47

75.65

-68

275

0.006985

999.9

2497

4.214

1681.8

564.5

12.55

75.39

-35.5

280

0.009918

999.9

2485

4.201

1433.9

574

10.63

74.68

43.6

285

0.01389

999.5

2473

4.193

1239.4

583.5

8.91

73.95

112

290

0.0192

998.8

2461

4.187

1083.7

592.7

7.66

73.21

172

295

0.02621

997.8

2449

4.183

957.9

601.7

6.66

72.46

226

300

0.03537

996.5

2438

4.181

853.8

610.3

5.85

71.69

275

305

0.04719

995

2426

4.18

766.9

618.4

5.18

70.90

319

310

0.06231

993.3

2414

4.179

693.5

626

4.63

70.11

361

320

0.1055

989.3

2390

4.181

577.0

639.6

3.77

68.47

436

340

0.2719

979.5

2342

4.189

422.0

660.5

2.68

65.04

565

360

0.6219

967.4

2291

4.202

326.1

673.7

2.03

61.41

679

373.15

1.014

958.3

2257

4.216

281.7

679.1

1.75

58.91

751

400

2.458

937.5

2183

4.256

218.6

683.6

1.36

53.58

895

420

4.373

919.9

2123

4.299

186.7

682.5

1.18

49.41

1008

440

7.337

900.5

2059

4.357

162.8

678

1.05

45.10

1132

460

11.71

879.5

1989

4.433

144.3

670.2

0.955

40.66

1273

480

17.9

856.5

1912

4.533

129.7

659

0.892

36.11

1440

500

26.39

831.3

1825

4.664

117.7

643.9

0.853

31.47

1645

520

37.69

803.6

1730

4.838

107.6

624.6

0.833

26.78

1909

540

52.37

772.8

1622

5.077

98.8

600.1

0.835

22.08

2266

560

71.06

738

1499

5.423

90.8

570.1

0.864

17.40

2783

580

94.48

697.6

1353

5.969

83.4

534.6

0.931

12.80

3607

600

123.4

649.4

1176

6.953

75.7

495.3

1.06

8.38

5141

620

159

586.9

941

9.354

67.3

454.1

1.39

4.27

9092

640

202.7

481.5

560

25.94

55.3

414.9

3.46

0.81

39710

647

220.4

357.3

47

3905

46.9

1323

138

0.00

7735000

 

 

 

 

 

 

 

 

 

 

381 drop pressure phase-Two 8.11

382 CHAPTER 11  Boiling and condensation

Table 11.4  Properties of saturated steam (Meyer et al., 1993; Harvey et al., 2000).

T

p

ρg

cpg

g × 106

kg × 103

Prg

βg × 106

(K)

(bar)

(kg/m3)

(kJ/kg K)

(Ns/m2)

(W/m K)

 

(K–1)

273.16

0.006177

0.004855

1.884

9.216

17.07

1.02

3681

275

0.006985

0.005507

1.886

9.26

17.17

1.02

3657

280

0.009918

0.007681

1.891

9.382

17.44

1.02

3596

285

0.01389

0.01057

1.897

9.509

17.73

1.02

3538

290

0.0192

0.01436

1.902

9.641

18.03

1.02

3481

295

0.02621

0.01928

1.908

9.778

18.35

1.02

3428

300

0.03537

0.02559

1.914

9.92

18.67

1.02

3376

305

0.04719

0.0336

1.92

10.06

19.01

1.02

3328

310

0.06231

0.04366

1.927

10.21

19.37

1.02

3281

320

0.1055

0.07166

1.942

10.52

20.12

1.02

3195

340

0.2719

0.1744

1.979

11.16

21.78

1.01

3052

360

0.6219

0.3786

2.033

11.82

23.69

1.01

2948

373.15

1.014

0.5982

2.08

12.27

25.1

1.02

2902

400

2.458

1.369

2.218

13.19

28.35

1.03

2874

420

4.373

2.352

2.367

13.88

31.13

1.06

2914

440

7.337

3.833

2.56

14.57

34.23

1.09

3014

460

11.71

5.983

2.801

15.26

37.66

1.13

3181

480

17.9

9.014

3.098

15.95

41.45

1.19

3428

500

26.39

13.2

3.463

16.65

45.67

1.26

3778

520

37.69

18.9

3.926

17.38

50.44

1.35

4274

540

52.37

26.63

4.54

18.15

56.1

1.47

4994

560

71.06

37.15

5.41

19.01

63.34

1.62

6091

580

94.48

51.74

6.76

20.02

73.72

1.84

7904

600

123.4

72.84

9.181

21.35

91.05

2.15

1135

620

159

106.3

14.94

23.37

126.7

2.76

2000

640

202.7

177.1

52.59

27.94

250

5.88

7995

647

220.4

286.5

53340

39.72

1573

135

9274000

 

 

 

 

 

 

 

 

model overestimating the acceleration pressure drop, as it neglects the slip between the phases and assumes equal acceleration for both liquid and vapor phases. It may be noted that the homogenous model gives accurate results for dispersed flow – bubbly flow with small bubbles dispersed in liquid and spray flow or drop flow with small droplets dispersed in vapor, as the vapor velocity is approximately equal to the liquid velocity. The homogenous model also gives accurate results for higher pressures where vapor properties approach liquid properties. For accurate estimates of pressure drop over a wide range of operating conditions and vapor qualities, the correlations based on the separated flow model are recommended (Collier and Thome, 1994; Stephan, 1992; Jayaramu et al., 2019).

11.8 Two-phase pressure drop 383

In summary, the preceding sections gave a step by step approach to quickly estimate heat transfer and pressure drop in boiling and condensation based on the empirical correlations reported by many researchers in the past. These should be good enough for commonly encountered engineering applications, though the reader is encouraged to take the cognizance of the assumptions under which these are valid. Should situations arise where these assumptions do not hold, more advanced correlations need to be used. If these too do not work for a problem, numerical modeling or in-house experimentation may be required to determine heat transfer coefficient and pressure drop.

Example 11.3: Water flows upward in a vertical uniformly heated tube of length 0.9 m. The mass flux and the inlet subcooling are 500 kg/m2s and 0 K, respectively. The inner diameter of the tube is 25 mm. The system pressure is 10 bar. Determine the critical heat flux (given F1 = 0.478, F2 = 0.662, F3 = 0.4, F4 = 0.0166 for p = 10 bar) and the corresponding local quality at the exit.

Solution:

Using Eq. (11.44),

 

 

D G ( hsub )

 

 

 

 

 

 

 

 

 

 

 

A' +

 

 

 

 

 

 

i

 

 

 

 

 

 

 

 

 

 

 

 

 

4

 

 

 

 

 

 

 

 

 

 

 

qcrit =

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

C' + z

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

=

 

A'

(since (

Tsub ) = 0)

 

 

 

 

 

C ' + z

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

i

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

A' =

2.317

D G hfg

 

 

 

 

 

F1

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

4

 

 

 

 

 

 

 

 

1/ 2

G

 

 

 

 

 

 

1 + 0.0143 F2 D

 

 

 

=

 

 

 

0.025 500 2014.9 103 0.478

 

2.317

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

(1 +

0.0143 0.662

 

 

 

 

 

 

 

4

0.0251/ 2 500)

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

= 3.988 106

 

 

 

 

 

 

 

 

 

 

 

 

 

n = 2 0.00725 p

 

 

 

 

 

 

 

 

 

 

 

 

 

= 2 0.00725 × 10 (since p = 10 bar)

 

= 1.9275

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

C' =

 

0.077 F3 D G

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

G n

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

1 + 0.347 F4

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

1356

 

 

 

 

 

 

 

=

 

0.077 0.4

0.025 500

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

500 1.9275

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

1 + 0.347 0.0166

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

1356

 

 

 

 

 

= 0.384

384 CHAPTER 11  Boiling and condensation

Therefore,

= 3.988 ×106 qcrit 0.384 + 0.9

= 3.104 ×106 W/m2

From energy balance, the exit quality can be determined as follows:

G

π D2

(hf + xe hfg hf ) = qcrit π D z

 

4

 

 

4 qcrit z

 

 

 

xe =

 

 

 

 

G Dh

 

 

 

 

fg

 

 

=

 

4 × 3.104 × 106 × 0.9

 

 

500 × 0.025 × 2014.9 × 103

 

 

xe =

0.4436

 

It is instructive to note the order of magnitude of critical heat flux for flow boiling. As a rule of thumb it goes as MW/m2, for water.

Example 11.4: For the problem in Example 11.3, with heat flux equal to the critical heat flux, determine the local heat transfer coefficients and the corresponding wall temperatures at two locations: z = 0.4 m and 0.8 m from the inlet. Use the Chen correlation.

Solution:

Saturated water properties corresponding to 10 bar are:

k f = 0.677 W/mK, Prf = 0.967, σ = 0.04226 N/m, cpf = 4.403 × 103 J/kg K,

ρg = 5.16 kg/m3 , ρf = 887 kg/m3 , hfg = 2014.9 × 103 J/kg, µf = 148.5 × 106 Ns/m2 , µg = 15.02 × 106 Ns/m2

Using Eq. (11.34),

1

 

 

 

 

 

x 0.9

 

 

 

ρ f

 

0.5

µg

 

0.1

 

 

 

 

 

 

 

 

=

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Xtt

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

1

x

 

 

 

ρg

 

 

µ f

 

 

 

 

 

 

 

 

q = q

 

= 3.104 106 W/m2

 

 

 

 

 

 

 

 

 

 

 

 

crit

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

At z = 0.4 m,

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

x =

4 q z

=

 

 

 

4 × 3.104 × 106 × 0.4

 

= 0.197

 

 

 

500 × 0.025 × 2014.9 × 103

 

 

 

 

 

G Dhfg

 

 

 

 

1

 

 

 

 

0.197

 

 

0.9

 

887 0.5

 

15.02 × 106 0.1

 

 

 

 

=

 

 

 

 

 

 

 

 

×

 

 

 

×

× 10

6

 

 

Xtt

 

 

 

 

 

 

 

 

 

 

 

1

0.197

 

 

 

 

5.16

 

148.5

 

 

 

 

 

= 2.944

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Re

 

=

G D(1 x)

=

500 × 0.025 × (1 0.197)

= 67612

 

 

 

 

 

f

 

 

 

 

 

 

f

 

 

 

 

 

 

 

148.5 × 106

 

 

 

 

 

11.8 Two-phase pressure drop 385

Using Eq. (11.35), and since

1

> 0.1,

 

 

 

 

 

Xtt

 

1

0.736

 

 

F = 2.35

 

 

+ 0.213

 

 

 

 

 

 

Xtt

 

 

 

=2.35(2.944 + 0.213)0.736

=5.477

Using Eq. (11.32),

0.8

0.4

kf

 

hc = 0.023Ref

Prf

 

 

 

F

 

 

 

 

D

 

=0.023 (67612)0.8 (0.967)0.4 0.677 5.477

0.025

=24555W/m2 K

=24.55kW/m2 K

Using Eq. (11.33),

ReTP = Ref × F1.25

= 67612 × 5.4771.25

= 5.665 ×105

Using Eq. (11.41),

S =

1

 

1+ 2.53 ×106 × ReTP1.17

=

0.0683

Using Eq. (11.40),

hNcB = 0.00122

 

 

k0.79f c0.45pf ρ0.49f

 

(Tw Tsat )

0.24

(psat (Tw )psat (Tsat ))

0.75

(S)

 

 

 

 

 

 

 

 

 

 

 

σ

0.5

0.29

0.24

0.24

 

 

 

 

 

 

µ f

hfg

ρg

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

0.734 × 43.62 × 27.83

 

 

0.24

(psat (Tw )psat (Tsat ))

 

= 0.00122

 

 

 

 

 

 

 

 

 

 

(Tw Tsat )

 

0.75

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

0.2055 × 0.0776 × 32.58 × 1.4826

 

 

 

 

 

×0.0683

=0.0963 × (Tw Tsat )0.24 (psat (Tw )psat (Tsat ))0.75

Using Eq. (11.30),

hTP = hc + hNcB

q = hTP (Tw Tsat )

3.104 × 106 = 24555 + 0.0963 × (Tw Tsat )0.24 (psat (Tw )psat (Tsat ))0.75 (Tw Tsat ) Since q = qcrit , (Tw Tsat ) must be high.

We now face a special difficulty here. The heat flux on the left-hand side of the equation is known. The right-hand side contains Tw, which we are seeking. Unfortunately we cannot solve for Tw, as the expression on the right-hand side has the saturation pressure

psat (Tw), which is as yet unknown in view of the fact that Tw is unknown. Hence we have no option but to go for an iterative solution with an assumed value of Tw and iterating it

to convergence.

Let (Tw Tsat ) = 50 C

386 CHAPTER 11  Boiling and condensation

Tw = Tsat (10 bar) + 50 C

=180 + 50 C

=230 C

psat (Tw ) = 27.98 bar = 27.98 × 105 N/m2

psat (Tw ) psat (Tsat ) = (27.98 10) × 105 = 17.98 × 105 N/m2

q = hTP (Tw Tsat )

=24555 + 0.0963 × (Tw Tsat )0.24 (psat (Tw ) psat (Tsat ))0.75 (Tw Tsat )

=24555 + 0.0963 × 500.24 × (17.98 × 105 )0.75 × 50 =1.832 × 106 < 3.104 × 106 W/m2

Let (Tw Tsat ) = 65 C

Tw = Tsat (10 bar) + 65 C =180 + 65 C

= 245 C

psat (Tw ) = psat (245 C) = 36.62 × 105 N/m2

psat (Tw ) psat (Tsat ) = (36.62 10) × 105 = 26.62 × 105 N/m2

q = hTP (Tw Tsat )

q= 24555 + 0.0963 × 650.24 × (26.62 × 105 )0.75 × 65 = 2.719 × 106 < 3.104 × 106 W/m2

Let (Tw Tsat ) = 70 C

Tw = 180 + 70 C = 250 C psat (Tw ) = 39.776 × 105 N/m2

psat (Tw ) psat (Tsat ) = 29.776 × 105 N/m2

q = hTP (Tw Tsat )

= 3.058 × 106 3.104 × 106 W/m2

Therefore, at z = 0.4 m,

 

hTP =

3.058 × 106

= 43685 W/m2K

 

 

 

 

 

 

Tw =

 

 

 

70

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

250 C

 

 

 

 

 

 

 

 

 

 

 

 

 

At z =

0.8 m,

 

 

 

 

 

 

 

 

 

 

 

 

 

 

x =

 

 

4 q z

=

 

 

 

4 × 3.104 × 106 × 0.8

= 0.394

 

 

 

500 × 0.025 × 2014.9 × 103

 

 

 

 

 

G Dhfg

 

 

 

 

 

1

 

 

 

0.394

 

 

0.9

 

887 0.5

15.02 ×

106

0.1

 

 

 

=

 

 

 

 

 

 

 

×

 

×

 

 

6

 

= 7.07

 

Xtt

 

0.394

 

10

 

 

1

 

 

 

 

 

5.16

148.5 ×

 

 

 

Re

 

=

 

G D(1 x)

=

500 × 0.025 × (1 0.394)

= 51041

 

 

 

 

 

 

f

 

 

 

 

f

 

 

 

 

 

 

148.5 × 106

 

 

 

 

 

11.8 Two-phase pressure drop 387

 

 

1

0.736

F = 2.35

 

 

+ 0.213

 

 

Xtt

 

=2.35 × (7.07 + 0.213)0.736

=10.13

hc = 0.023 Re0f .8 Prf0.4 kDf F

=36349W/m2K

ReTP = Ref × F1.25

=9.244 × 105

S =

 

 

 

1

 

= 0.0398

1

+ 2.53

×10

6 1.17

 

ReTP

Using S = 0.0398 in the expression for hNcB,

hNcB = 0.0561× (Tw Tsat )0.24 (psat (Tw )psat (Tsat ))0.75

hTP = hc + hNcB

q = hTP (Tw Tsat ) = 36349 + 0.0561× (Tw Tsat )0.24 (psat (Tw )psat (Tsat ))0.75 (Tw Tsat )

Let(Tw Tsat ) = 65 C

Tw = Tsat + 65 C = 180 + 65 C = 245 C

psat (Tw )psat (Tsat ) = 26.62 × 105 N/m2

Substituting the above values in the expression for q,

q = 3.017 ×106 3.104 ×106 W/m2

Therefore, at z = 0.8 m,

hTP = 3.017 ×106 = 46415W/m2K 65

Tw = 245 C

Note that this sample problem does not ask for the calculation of the heat transfer coefficient at z = 0.9 m (tube exit). It is intentional, as the heat flux is equal to the critical heat flux, which indicates dryout at the exit. The Bowring CHF correlation presented in the chapter (or for that matter any other CHF correlation) estimates the CHF that corresponds to the onset of dryout (or DNB) at the tube exit. The Chen correlation should not be used to calculate the two-phase heat transfer coefficient for dryout and post-dryout (spray flow or drop flow) heat transfer, though the correlation gives some values of the heat transfer coefficient. The heat transfer coefficient calculated at the tube exit using the Chen correlation can at best be taken as the value prior to the onset of dryout at the tube exit.

388CHAPTER 11  Boiling and condensation

Example 11.5: For the problem in Example 11.3, with heat flux equal to the critical heat flux, evaluate the pressure drop across the tube using the homogeneous model.

Solution:

Fluid properties corresponding to 10 bar are:

f = 148.5 × 106 Ns/m2 , g = 15.02 × 106 Ns/m2 Specific volumes v f = 1.127 × 103 m3 /kg, vg = 0.1937m3 /kg

v fg = vg v f = 0.1926 m3 /kg

The tube exit quality, xe = 0.4436

Fanning friction factor at the tube inlet:

Re

 

=

GD =

500 × 0.025

= 84175

 

f

 

f

148.5 ×106

 

Using the Blasius equation,

f

 

=

0.079 = 0.00464

 

f

 

Re1/4f

Fanning friction factor at the tube exit:

Two-phase viscosity can be calculated from the relation

1

 

=

 

 

x

+ 1x

 

 

 

 

 

 

 

 

g

f

 

 

 

 

 

 

 

 

 

=

0.4436

+ (10.4436)

 

 

 

 

 

 

15.02 × 106

148.5 × 106

 

 

 

= 30.4 × 106 Ns/m2

Re

=

 

 

GD = 500 × 0.025 = 4.16 × 105

TP

 

 

 

 

30.4 × 106

Using the Blasius equation,

= 0.079 =

fTP ReTP1/4 0.0031

The average value of fTP over the tube length is given by

fTP, avg =

ff + fTP

= 0.00387

2

 

 

The total pressure drop can be determined using Eq. (11.91). The frictional pressure drop from the homogeneous model is given by

p

 

= 2 fTP,avg G2 vf

z

 

1 + vfg xe

 

 

 

 

 

f

 

 

D

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

vf 2

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

2 0.00387 5002 1.127

103 0.9

0.1926 0.4436

 

 

=

 

 

 

0.025

 

 

 

 

1

+

1.127 10

3

 

 

 

 

 

 

 

 

 

 

 

 

2

 

 

= 3054 N/m2

11.8 Two-phase pressure drop 389

The acceleration pressure drop from the homogeneous model is given by

pa = G2 v fg xe

=5002 × 0.1926 × 0.4436

=21359 N/m2

The gravitational head pressure drop from the homogeneous model is given by

pg =

g sin

(θ ) z

 

+

vfg

 

 

 

ln 1

 

xe

v fg

xe

v f

 

 

 

 

 

 

 

 

 

 

 

 

9.81 1 0.9

 

 

0.1926

 

 

 

 

=

 

 

ln 1

+

 

 

 

0.4436

 

0.1926

0.4436

 

-3

 

 

1.127 10

 

 

 

 

= 449 N/m2

The total pressure drop

ptotal = pf + pa + pg

=3.054 + 21.359 + 0.449 kN/m2

=24.862 kN/m2

Example 11.6: Saturated water at 0.123 bar with a mass flux of 400 kg/m2s enters a vertical tube and flows upward. There is saturated steam at 1.013 bar condensing on the tube outer surface. The length and diameter of the tube are 0.6 m and 0.025 m, respectively. Assume laminar film condensation. Determine

(a)The average heat transfer coefficient on the condensation side.

(b)The average heat transfer coefficient on the boiling side, which can be assumed to be approximately equal to the mean of the local heat transfer coefficients at the inlet and outlet of the tube. You may use the Chen correlation.

(c)The average tube wall temperature.

(d)The rate of condensation (total), kg/s.

(e)The exit quality on the boiling side.

Solution:

The average heat transfer coefficient relationship for laminar film condensation on a vertical plate, given by Eq. (11.63), can also be used for condensation on a vertical tube.

 

 

 

 

ρ f (ρ f ρg )g hfg

k3f

1/ 4

 

 

 

h f

= 0.943

 

 

 

 

µ f z (Tsat Tw )

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Though all liquid properties in the above expression correspond to the film tem-

perature (Tw + Tsat)/2, and hfg corresponds to Tsat, let all the properties be evaluated at Tsat since Tw is unknown.

390 CHAPTER 11  Boiling and condensation

 

 

= 0.943

 

958 × (958 0.598) × 9.81 × 2257 × 103 × 0.6813

1/4

h f

 

283.1 × 106 × 0.6 × (100 Tw )

 

 

 

 

 

 

 

 

 

 

1

 

 

 

 

 

 

 

 

 

 

= 0.943 × 13939.67 ×

 

 

 

 

 

(100 Tw )1/4

 

The two-phase heat transfer coefficient for saturated boiling is obtained using Eq. (11.30),

hTP = hc + hNcB

Using Eq. (11.34) and the saturated fluid properties at 0.123 bar,

1

ρ f 0.5 µg

 

0.1

x 0.9

 

 

 

 

 

=

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Xtt

 

 

 

 

 

 

 

 

 

 

ρg µ f

 

 

 

1− x

 

 

 

 

 

 

 

988

0.5

 

 

10.1 106

0.1

 

x 0.9

 

=

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

547.8 10

6

 

 

 

0.083

 

 

 

 

 

 

 

1− x

 

= 73.17

 

x

0.9

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

− x

 

 

 

 

 

 

 

 

 

 

 

 

1

 

 

 

 

 

 

 

 

 

From Eq. (11.35),

 

 

 

1

 

 

 

 

F = 1 for

 

 

 

0.1

 

 

 

 

 

 

 

 

 

 

Xtt

 

 

 

 

 

1

 

 

0.736

 

1

 

= 2.35

 

 

+ 0.213

for

 

> 0.1

 

 

 

Xtt

 

 

 

 

Xtt

 

From Eq. (11.32),

h = 0.023

G (1 x) D 0.8

cp 0.4

kf

(F)

 

 

 

 

 

 

 

 

 

 

 

 

 

 

c

 

f

 

 

 

 

 

 

 

 

 

 

 

k f

D

 

 

= 0.023

400

0.025

0.8

(1 − x)

0.8

(3.56)

0.4

 

 

6

 

 

 

 

 

 

547.8 10

 

 

 

 

 

 

 

 

 

 

 

 

= 2521.53 (1 − x)0.8 F

From Eq. (11.40),

0.643 (F)0.025

hNcB = 0.00122

 

 

k0.79f

c0.45pf ρ0.49f

 

(Tw

− Tsat )

0.24

(psat (Tw ) − psat

(Tsat ))

0.75

(S)

 

 

 

 

 

 

 

 

 

 

 

σ

0.5

0.29

0.24

0.24

 

 

 

 

 

 

 

µ f

 

hfg

ρg

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

= 0.00122

 

 

 

0.7055 42.16 29.34

 

 

 

T 0.24

 

p0.75

S

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

sup

 

sup

 

 

 

 

 

0.2606 0.1133 33.92 0.55

 

 

 

 

 

 

 

 

From Eq. (11.33),

ReTP = Ref × F1.25

=G(1 x) D × F1.25

f

=18254.8 × (1 x) × F1.25

From Eq. (11.41),

S =

1

 

 

 

1 + 2.53 × 10

6 Re1.17

 

 

TP