01 POWER ISLAND / 01 CCPP / V. Ganapathy-Industrial Boilers and HRSG-Design (2003)
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TABLE 7.6 Tube Diameter Versus Friction Factor (Darcy) for Turbulent Flow
di (in.) |
f |
0.50.028
0.750.0245
1.00.0230
1.50.0210
2.00.0195
2.50.0180
3.00.0175
4.00.0165
5.00.0160
8.00.0140
10.00.013
7.17b
Q:
Estimate the pressure drop in a superheater of a boiler that has an equivalent length of 200 ft. The tube inner diameter is 2.0 in., the flow per pass is 8000 lb=h, the steam pressure is 800 psia, and the temperature is 700 F.
A:
Using Eq. (13) and substituting v ¼ 0.78 cu ft=lb and f ¼ 0.0195 for turbulent flow from Table 7.6 (generally flow in superheaters, economizers, and piping would be turbulent), we obtain
DP ¼ 3:36 10 6 0:0195 200 80002 02:785 ¼ 21 psi
7.18a
Q:
How does the friction factor depend on pipe roughness?
A:
For smooth tubes such as copper and other heat exchanger tubes, f [12]
f ¼ 0:133 Re 0:174
is given by
ð15Þ
Copyright © 2003 Marcel Dekker, Inc.
Substituting this into Eq. (13) gives us
DP |
¼ 0:0267 r |
0:8267 |
m |
0:174 V 1:826 |
ð16Þ |
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Le |
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di1:174 |
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(m is the viscosity, lb=ft h; V is the velocity, fps.)
7.18b
Q:
Determine the pressure drop per 100 ft in a drawn copper tube of inner diameter 1.0 in. when 250 lb=h of air at a pressure of 30 psig and at 100 F flows through it.
A:
Calculate the density (see Chap. 5):
45
r ¼ 29 492 359 560 15 ¼ 0:213 lb=cu ft
The effect of pressure can be neglected in the estimation of viscosity of gases up to 40 psig. For a detailed computation of viscosity as a function of pressure, readers may refer to Ref. 11. From Table 7.7, m ¼ 0.047 lb=ft h. The velocity is
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V ¼ 250 |
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576 |
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¼ 60 fps |
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3600 |
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3:14 |
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0:213 |
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DP |
¼ 0:0267 |
0:213 |
0:8267 |
0:047 |
0:174 |
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601:826 |
¼ 7:7 psi |
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100 |
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1 |
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TABLE 7.7 Viscosity of Air |
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Temperature ( F) |
Viscosity (lb=ft h) |
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100 |
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0.0459 |
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200 |
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0.0520 |
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400 |
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0.062 |
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600 |
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0.0772 |
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800 |
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0.0806 |
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1000 |
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0.0884 |
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1200 |
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0.0957 |
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1400 |
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0.1027 |
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1600 |
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0.1100 |
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1800 |
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0.1512 |
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Copyright © 2003 Marcel Dekker, Inc.
7.19a
Q:
Derive the expression for DP for laminar flow of fluids.
A:
For laminar flow of fluids in pipes such as that occurring with oils, the friction factor is
64 |
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f ¼ |
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ð17aÞ |
Re |
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Substituting into Eq. (13) and using Eq. (14) gives us |
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DP ¼ 3:36 10 6 64 dimW 2 |
Le v |
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¼ 14:4 10 6 W Le vm di4
Converting lb=h to gph (gallons per hour), we can rewrite this as
DP ¼ 4:5 10 6 Le cS s gph di4
ð17bÞ
ð18Þ
where
cS ¼ viscosity, centistokes s ¼ specific gravity
Equation (18) is convenient for calculations for oil flow situations.
7.19b
Q:
Estimate the pressure drop per 100 ft in an oil line when the oil has a specific gravity of 16 API and is at 180 F. The line size is 1.0 in., and the flow is 7000 lb=h.
A:
We must estimate Re. To do this we need the viscosity [13] in centistokes:
195 |
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cS ¼ 0:226 SSU |
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for SSU 32 100 |
ð19Þ |
SSU |
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135 |
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cS ¼ 0:220 SSU |
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for SSU > 100 |
ð20Þ |
SSU |
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SSU represents the Saybolt seconds, a measure of viscosity. Also, cS s ¼ cP, where cP is the viscosity in centipoise, and 0.413 cP ¼ 1 lb=ft h.
Copyright © 2003 Marcel Dekker, Inc.
The specific gravity is to be found. At 180 F, from Eq. (23) (see Q7.21) it can be shown that the specific volume at 180 F is 0.0176 cu ft=lb. Then
1
s ¼ 0:0176 62:4 ¼ 0:91
Hence cP ¼ 0.91 24.83, where
135
cS ¼ 0:22 118 118 ¼ 24:83
and
m ¼ 2:42 0:91 24:83 ¼ 54:6 lb=ft h
7000
Re ¼ 15:2 0:91 24:83 2:42 ¼ 1948
(2.42 was used to convert cP to lb=ft h.) From Eq. (17a),
64 |
¼ 0:0328 |
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f ¼ |
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1948 |
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Substituting into Eq. (17b) yields |
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DP ¼ 14 |
10 6 54:6 7000 100 |
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¼ 9:42 psi |
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0:91 |
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62:4 |
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7.20a
Q:
For viscous fluids in turbulent flow, how is the pressure drop determined?
A:
For viscous fluids, the following expression can be used for the friction factor:
f ¼ |
0:316 |
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ð21Þ |
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Re0:22 |
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Substituting into Eq. (13) gives us |
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P |
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3:36 |
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10 6 |
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0:361 |
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d |
0:22L |
W 2 |
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v |
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ð15:2W Þ0:22di5 |
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D |
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¼ |
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ð |
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22 |
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¼ 0:58 |
10 |
6 |
m |
0:22 |
W |
1:78 |
Le |
v |
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ð |
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d4:78 |
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Copyright © 2003 Marcel Dekker, Inc.
7.20b
Q:
A fuel oil system delivers 4500 lb=h of light oil at 70 F in a pipe. What is the flow
that can be delivered at 30 F, assuming that m70=m30 ¼ 0:5; v70=v30 ¼ 0:95, and flow is turbulent?
A:
Using Eq. (22), we have
v1W11:78m01:22 ¼ v2W21:78m02:22
45001:78 0:50:22 0:95 ¼ W21:78
or
W2 ¼ 4013 lb=h
7.21
Q:
What is the flow in gpm if 1000 lb=h of an oil of specific gravity (60=60 F) ¼ 0.91 flows in a pipe at 60 F and at 168 F?
A:
We need to know the density at 60 F and at 168 F.
At 60 F:
Density ¼ r ¼ 0:91 62:4 ¼ 56:78 lb=cu ft
1
v60 ¼ 56:78 ¼ 0:0176 cu ft=lb
Hence at 60 F,
1000
q ¼ 60 56:78 ¼ 0:293 cu ft=min ðcfmÞ ¼ 0:293 7:48 ¼ 2:2 gpm
At 168 F, the specific volume of fuel oils increases with temperature:
vt ¼ v60½1 þ Eðt 60Þ& |
ð23Þ |
where E is the coefficient of expansion as given in Table 7.8 [13]. For this fuel oil, E ¼ 0.0004. Hence,
v168 ¼ 0:0176 ð1 þ 0:0004 108Þ ¼ 0:01836 cu ft=lb
Copyright © 2003 Marcel Dekker, Inc.
TABLE 7.8 Expansion Factor for Fuel Oils
API |
E |
14.9 |
0.00035 |
15–34.9 |
0.00040 |
35–50.9 |
0.00050 |
51–63.9 |
0.00060 |
64–78.9 |
0.00070 |
79–88.9 |
0.00080 |
89–93.9 |
0.00085 |
94–100 |
0.00090 |
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Hence
q168 ¼ 1000 0:01836 60
¼0:306 cfm ¼ 0:306 7:48
¼2:29 gpm
7.22
Q:
How is the pressure loss in natural gas lines determined? Determine the line size to limit the gas pressure drop to 20 psi when 20,000 scfh of natural gas of specific gravity 0.7 flows with a source pressure of 80 psig. The length of the pipeline is 150 ft.
A:
The Spitzglass formula is widely used for compressible fluids [13]:
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r |
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ð |
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q |
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3410 |
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F |
P12 P22 |
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24 |
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sL |
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where |
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q ¼ gas flow, scfh |
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P1; |
s ¼ gas specific gravity |
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P2 ¼ gas inlet and exit pressures, psia |
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F ¼ a function of pipe inner diameter (see Table 7.9) |
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L ¼ length of pipeline, ft |
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Substituting, we have |
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r |
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¼ |
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20;000 |
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3410 |
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F |
952 752 |
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0:7 |
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150 |
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Copyright © 2003 Marcel Dekker, Inc.
Hence F ¼ 1.03. From Table 7.9 we see that d should be 114 in. Choosing the next higher standard F or d limits the pressure drop to desired values. Alternatively, if q; d; L, and P1 are given, P2 can be found.
7.23
Q:
Determine the pressure loss in a rectangular duct 2 ft 2.5 ft in cross section if 25,000 lb=h of flue gases at 300 F flow through it. The equivalent length is 1000 ft.
TABLE 7.9 Standard Steel Pipea Data (Black, Galvanized, Welded, and
Seamless)
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Functions |
Nominal |
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Outside |
Inside |
Wall |
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pipe size |
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diameter |
diameter |
thickness |
diameter,c |
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[in. (mm)] |
Scheduleb |
[in. (mm)] |
(in.) |
(in.) |
F (in.) |
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1=8 (6) |
40 |
0.405 |
(10.2) |
0.269 |
0.068 |
0.00989 |
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1=4 (8) |
40 |
0.540 |
(13.6) |
0.364 |
0.088 |
0.0242 |
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3=8 (10) |
40 |
0.675 |
(17.1) |
0.493 |
0.091 |
0.0592 |
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1=2 (15) |
40 |
0.840 |
(21.4) |
0.622 |
0.109 |
0.117 |
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3=4 (20) |
40 |
1.050 |
(26.9) |
0.824 |
0.113 |
0.265 |
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(25) |
40 |
1.315 |
(33.8) |
1.049 |
0.113 |
0.533 |
11=4 (32) |
40 |
1.660 |
(42.4) |
1.380 |
0.140 |
1.17 |
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11=2 (40) |
40 |
1.900 |
(48.4) |
1.610 |
0.145 |
1.82 |
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2 |
(50) |
40 |
2.375 |
(60.2) |
2.067 |
0.154 |
3.67 |
21=2 (65) |
40 |
2.875 |
(76.0) |
2.469 |
0.203 |
6.02 |
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3 |
(80) |
40 |
3.500 |
(88.8) |
3.068 |
0.216 |
11.0 |
4 |
(100) |
40 |
4.500 |
(114.0) |
4.026 |
0.237 |
22.9 |
5 |
(125) |
40 |
5.563 |
(139.6) |
5.047 |
0.258 |
41.9 |
6 |
(150) |
40 |
6.625 |
(165.2) |
6.065 |
0.280 |
68.0 |
8 |
(200) |
40 |
8.625 |
(219.1) |
7.981 |
0.322 |
138 |
8 |
(200) |
30 |
8.625 |
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8.071 |
0.277 |
142 |
10 (250) |
40 |
10.75 (273.0) |
10.020 |
0.365 |
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10 (250) |
30 |
10.75 |
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10.136 |
0.307 |
254 |
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12 (300) |
40 |
12.75 (323.9) |
11.938 |
0.406 |
382 |
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12 (300) |
30 |
12.75 |
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12.090 |
0.330 |
395 |
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a ASTM A53-68, standard pipe.
b Schedule numbers are approx. values of 1000 maximum internal service pressure, psig allowable stress in material, psi
p
c F ¼ dð1 þ 0:03d þ 3:6=dÞ for use in Spitzglass formula ¼ 5=23 for gas line pressure loss. Source: Adapted from Ref. 13.
Copyright © 2003 Marcel Dekker, Inc.
A:
The equivalent diameter of a rectangular duct is given by
di ¼ 2 a |
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¼ 2 |
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2:5 |
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a þ b |
4:5 |
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¼ 2:22 ft ¼ 26:64 in: |
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The friction factor f |
in turbulent flow region for flow in ducts and pipes is given |
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by [11] |
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f ¼ |
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ð25Þ |
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Re0:25 |
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We make use of the equivalent diameter calculated earlier [Eq. (14)] while computing Re:
W
Re ¼ 15:2 dim
From Table 7.7 at 300 F, m ¼ 0.05 lb=ft h.
25,000
Re ¼ 15:2 26:64 0:05 ¼ 285;285
Hence
0:316
f ¼ 285;2850:25 ¼ 0:014
For air or flue gases, pressure loss is generally expressed in inches of water column and not in psi. The following equation gives DPg [11]:
DPg ¼ 93 10 6 |
L |
ð26Þ |
fW 2v d5e |
where di is in inches and the specific volume is v ¼ 1=r.
40
r ¼ 460 þ 300 ¼ 0:526 lb=cu ft
Hence |
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¼ 19 cu ft=lb |
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v ¼ |
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0:0526 |
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Substituting into Eq. (26), we have |
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DPg ¼ 93 10 6 0:014 25;0002 19 |
1000 |
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¼ 1:16 in: WC |
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ð26:64Þ |
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Copyright © 2003 Marcel Dekker, Inc.
7.24a
Q:
Determine the Reynolds number when 500,000 lb=h of superheated steam at 1600 psig and 750 F flows through a pipe of inner diameter 10 in.
A:
The viscosity of superheated steam does not vary as much with pressure as it does with temperature (see Table 7.5).
m ¼ 0:062 lb=ft h
Using Eq. (14), we have |
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Re ¼ 15:2 |
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¼ 15:2 |
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500;000 |
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dim |
10 0:062 |
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¼ 1:25 |
107 |
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7.24b
Q:
Determine the Reynolds number when hot air flows over a tube bundle.
Air mass velocity ¼ 7000 lb=ft2 h
Temperature of air film ¼ 800 F
Tube size ¼ 2 in. OD
Transverse pitch ¼ 4.0 in.
A:
The Reynolds number when gas or fluids flow over tube bundles is given by the expression
Re ¼ |
Gd |
ð27Þ |
12m |
where
G ¼ fluid mass velocity, lb=ft2 h d ¼ tube outer diameter, in.
m ¼ gas viscosity, lb=ft h
At 800 F, the air viscosity from Table 7.7 is 0.08 lb=ft h; thus
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Re ¼ 7000 12 0:08 ¼ 14;580
Copyright © 2003 Marcel Dekker, Inc.
7.25
Q:
There are three tubes connected between two headers of a super heater, and it is required to determine the flow in each parallel pass. The table gives the details of each pass.
Tube no. (pass no.) |
Inner diameter (in.) |
Equivalent length (ft) |
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1 |
2.0 |
400 |
2 |
1.75 |
350 |
3 |
2.0 |
370 |
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Total steam flow is 15,000 lb=h, and average steam conditions are 800 psia and 750 F.
A:
Because the passes are connected between the same headers, the pressure drop in each will be the same. Also, the total steam flow will be equal to the sum of the flow in each. That is,
DP1 ¼ DP2 ¼ DP3
In other words, using the pressure drop correlation, we have
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2 Le2 |
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Le3 |
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W1 |
f1 |
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¼ W2 f2 |
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¼ W3 f3 |
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di51 |
di52 |
di53 |
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and |
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W1 |
þ W2 |
þ W3 ¼ total flow |
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The effect of variations in steam properties in the various tubes can be neglected, because it will not be very significant.
Substituting the data and using f from Table 7.6, we obtain
W1 þ W2 þ W3 ¼ 15;000
W12 0:0195 |
400 |
¼ W22 |
0:02 |
350 |
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25 |
ð1:75Þ5 |
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¼ W32 |
0:0195 |
370 |
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25 |
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¼ a constant
Copyright © 2003 Marcel Dekker, Inc.
