fluid_mechanics
430 Chapter 8 ■ Viscous Flow in Pipes COMMENT Note that for this pressure drop, the amount due to elevation change 1the hydrostatic effect2 is g1z 2 z 1 2 8.67 psi and the amount due to the increase in kinetic energy is r1V 2 2 V 2 122 2.07 psi. (b) If the only losses included are the major losses, the head loss is From Table 8.1 the roughness for a 0.75-in.-diameter copper pipe 1drawn tubing2 is e 0.000005 ft so that eD 8 10 5 . With this eD and the calculated Reynolds number 1Re 45,0002, the value of f is obtained from the Moody chart as f 0.0215. Note that the Colebrook equation 1Eq. 8.352 would give the same value of f. Hence, with the total length of the pipe as / 115 5 10 10 202 ft 60 ft and the elevation and kinetic energy portions the same as for part 1a2, Eq. 1 gives or (Ans) COMMENT Of this pressure drop, the amount due to pipe friction is approximately 121.3 10.72 psi 10.6 psi. (c) or If major and minor losses are included, Eq. 1 becomes where the 21.3 psi contribution is due to elevation change, kinetic energy change, and major losses [part 1b2], and the last term represents the sum of all of the minor losses. The loss coefficients of the components 1K L 1.5 for each elbow and K L 10 for the wide-open globe valve2 are given in Table 8.2 1except for the loss coefficient of the faucet, which is given in Fig. E8.8a as K L 22. Thus, or p 1 gz 2 1 2 r1V 2 2 V 2 12 rf / D 11248 2992 lbft 2 h L f / D 2g 11.94 slugsft 3 60 ft 210.02152 a 0.0625 ft b 18.70 ft s2 2 2 11248 299 15152 lbft 2 3062 lbft 2 p 1 21.3 psi p 1 gz 2 1 2 r1V 2 2 V 2 12 fg / D p 1 21.3 psi a rK L V 2 a rK V 2 L 2 11.94 slugs 18.70 ft 3 ft22 2 310 411.52 24 2 1321 lbft 2 Note that we did not include an entrance or exit loss because points 112 and 122 are located within the fluid streams, not within an ata rK V 2 L 9.17 psi 2 V 2 1 2g a rK V 2 L 2 V 1 2 V 2 1 2 2 (2) (3) taching reservoir where the kinetic energy is zero. Thus, by combining Eqs. 2 and 3 we obtain the entire pressure drop as p 1 121.3 9.172 psi 30.5 psi (Ans) This pressure drop calculated by including all losses should be the most realistic answer of the three cases considered. COMMENTS More detailed calculations will show that the pressure distribution along the pipe is as illustrated in Fig. E8.8b for cases 1a2 and 1c2—neglecting all losses or including all losses. Note that not all of the pressure drop, p 1 p 2 , is a “pressure loss.” The pressure change due to the elevation and velocity changes is completely reversible. The portion due to the major and minor losses is irreversible. This flow can be illustrated in terms of the energy line and hydraulic grade line concepts introduced in Section 3.7. As is shown in Fig. E8.8c, for case 1a2 there are no losses and the energy line 1EL2 is horizontal, one velocity head 1V 2 2g2 above the hydraulic grade line 1HGL2, which is one pressure head 1gz2 above the pipe itself. For cases 1b2 or 1c2 the energy line is not horizontal. Each bit of friction in the pipe or loss in a component reduces the available H, elevation to energy line, ft p, psi F I G U R E E8.8b 80 60 40 20 30 20 10 30.5 psi 27.1 27.8 (a) No losses (c) Including all losses Pressure loss 20.2 21.0 18.5 19.3 10.7 Elevation and kinetic energy 10.7 0 0 10 20 30 40 50 60 Slope due to pipe friction Sharp drop due to component loss Energy line including all losses, case (c) Energy line with no losses, case (a) 0 0 10 20 30 40 50 60 Distance along pipe from point (1), ft F I G U R E E8.8c 11.7 12.4 Distance along pipe from point (1), ft 9.93 6.37 3.09 6.37 4.84 2.07 2.07 p 2 = 0 Location: (1) (3) (4) (5) (6) (7)(8) (2)
8.5 Pipe Flow Examples 431 energy, thereby lowering the energy line. Thus, for case 1a2 the total head remains constant throughout the flow with a value of H p 1 g V 2 1 2g z 1 11547 lb ft 2 2 18.70 ft s2 2 162.4 lbft 3 2 26.0 ft. p 2 g V 2 2 2g z 2 p 3 g V 3 3 2g z 3 p For case 1c2 the energy line starts at H 1 p 1 g V 2 1 2g z 1 130.5 1442lb ft 2 162.4 lbft 3 2 and falls to a final value of 18.70 ft s2 2 0 71.6 ft 2132.2 fts 2 2 H 2 p 2 g V 2 2 2g z 2 0 119.6 ft s2 2 20 ft 2132.2 fts 2 2 26.0 ft The elevation of the energy line can be calculated at any point along the pipe. For example, at point 172, 50 ft from point 112, 2132.2 fts 2 2 0 H 7 p 7 g V 2 7 2g z 7 19.93 1442 lb ft 2 162.4 lbft 3 2 18.70 ft s2 2 20 ft 2132.2 fts 2 2 44.1 ft The head loss per foot of pipe is the same all along the pipe. That is, h L / f V 2 2gD 0.021518.70 ft s2 2 2132.2 fts 2 210.0625 ft2 0.404 ft ft Thus, the energy line is a set of straight line segments of the same slope separated by steps whose height equals the head loss of the minor component at that location. As is seen from Fig. E8.8c, the globe valve produces the largest of all the minor losses. Although the governing pipe flow equations are quite simple, they can provide very reasonable results for a variety of applications, as is shown in the next example. E XAMPLE 8.9 Type I, Determine Head Loss GIVEN As shown in Fig. E8.9a, crude oil at 140 °F with 53.7 lbft 3 and 8 10 5 lb sft 2 (about four times the viscosity of water) is pumped across Alaska through the Alaskan pipeline, a 799-mile-long, 4-ft-diameter steel pipe, at a maximum rate of Q 2.4 million barrelsday 117 ft 3 s. FIND Determine the horsepower needed for the pumps that drive this large system. Oil: = 53.7 lb/ft 3 4-ft-diameter, = 8 10 5 lbf . s/ft 2 799-mile-long steel pipe (1) (2) Prudhoe Bay, Alaska Pump F I G U R E E8.9a Valdez, Alaska SOLUTION From the energy equation 1Eq. 8.212 we obtain p 1 g V 2 1 2g z 1 h p p 2 g V 2 2 2g z 2 h L where points 112 and 122 represent locations within the large holding tanks at either end of the line and h p is the head provided to the oil by the pumps. We assume that z 1 z 2 1pumped from sea level to sea level2, p 1 p 2 V 1 V 2 0 1large, open tanks2 and h L 1 f/D2V 2 2g. Minor losses are negligible because of the large length-to-diameter ratio of the relatively straight, uninterrupted pipe; /D 1799 mi2 15280 ftmi214 ft2 1.05 10 6 . Thus, h p h L f / D V 2 2g where V QA (117 ft 3 s) 3p14 ft2 2 44 9.31 fts. From Fig. 8.20 or Eq. 8.35, f 0.0125 since eD 10.00015 ft214 ft2 0.0000375 1see Table 8.12 and Re rVDm 19.31 ft s214.0 ft2 18 10 5 lb # 3153.7 32.22 slugsft 3 4 sft 2 2 7.76 10 5 . Thus, h p 0.012511.05 10 6 2 19.31 ft s2 2 17,700 ft 2132.2 fts 2 2 and the actual power supplied to the fluid, p a , is p a gQh p 153.7 lbft 3 21117 ft 3 s2117,700 ft2 1.11 10 8 ft # 1 hp lbs a 550 ft # lbs b 202,000 hp (Ans) COMMENTS There are many reasons why it is not practical to drive this flow with a single pump of this size. First, there are no pumps this large! Second, the pressure at the pump outlet would
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430 Chapter 8 ■ Viscous Flow in Pipes<br />
COMMENT Note that for this pressure drop, the amount due<br />
to elevation change 1the hydrostatic effect2 is g1z 2 z 1 2 8.67 psi<br />
and the amount due to the increase in kinetic energy is<br />
r1V 2 2 V 2 122 2.07 psi.<br />
(b) If the only losses included are the major losses, the head<br />
loss is<br />
From Table 8.1 the roughness for a 0.75-in.-diameter copper<br />
pipe 1drawn tubing2 is e 0.000005 ft so that eD 8 10 5 .<br />
With this eD and the calculated Reynolds number 1Re <br />
45,0002, the value of f is obtained from the Moody chart as<br />
f 0.0215. Note that the Colebrook equation 1Eq. 8.352 would<br />
give the same value of f. Hence, with the total length of the pipe<br />
as / 115 5 10 10 202 ft 60 ft and the elevation<br />
and kinetic energy portions the same as for part 1a2, Eq. 1 gives<br />
or<br />
(Ans)<br />
COMMENT Of this pressure drop, the amount due to pipe<br />
friction is approximately 121.3 10.72 psi 10.6 psi.<br />
(c)<br />
or<br />
If major and minor losses are included, Eq. 1 becomes<br />
where the 21.3 psi contribution is due to elevation change, kinetic<br />
energy change, and major losses [part 1b2], and the last term represents<br />
the sum of all of the minor losses. The loss coefficients of<br />
the components 1K L 1.5 for each elbow and K L 10 for the<br />
wide-open globe valve2 are given in Table 8.2 1except for the loss<br />
coefficient of the faucet, which is given in Fig. E8.8a as K L 22.<br />
Thus,<br />
or<br />
p 1 gz 2 1 2 r1V 2 2 V 2 12 rf / D<br />
11248 2992 lbft 2<br />
h L f / D 2g<br />
11.94 slugsft 3 60 ft<br />
210.02152 a<br />
0.0625 ft b 18.70 ft s2 2<br />
2<br />
11248 299 15152 lbft 2 3062 lbft 2<br />
p 1 21.3 psi<br />
p 1 gz 2 1 2 r1V 2 2 V 2 12 fg / D<br />
p 1 21.3 psi a rK L V 2<br />
a rK V 2<br />
L<br />
2 11.94 slugs 18.70<br />
ft 3 ft22<br />
2 310 411.52 24<br />
2<br />
1321 lbft 2<br />
Note that we did not include an entrance or exit loss because points<br />
112 and 122 are located within the <strong>fluid</strong> streams, not within an ata<br />
rK V 2<br />
L 9.17 psi<br />
2<br />
V 2 1<br />
2g a rK V 2<br />
L<br />
2<br />
V 1<br />
2<br />
V 2 1<br />
2<br />
2<br />
(2)<br />
(3)<br />
taching reservoir where the kinetic energy is zero. Thus, by combining<br />
Eqs. 2 and 3 we obtain the entire pressure drop as<br />
p 1 121.3 9.172 psi 30.5 psi<br />
(Ans)<br />
This pressure drop calculated by including all losses should be the<br />
most realistic answer of the three cases considered.<br />
COMMENTS More detailed calculations will show that the<br />
pressure distribution along the pipe is as illustrated in Fig. E8.8b<br />
for cases 1a2 and 1c2—neglecting all losses or including all losses.<br />
Note that not all of the pressure drop, p 1 p 2 , is a “pressure<br />
loss.” The pressure change due to the elevation and velocity<br />
changes is completely reversible. The portion due to the major<br />
and minor losses is irreversible.<br />
This flow can be illustrated in terms of the energy line and hydraulic<br />
grade line concepts introduced in Section 3.7. As is shown<br />
in Fig. E8.8c, for case 1a2 there are no losses and the energy line<br />
1EL2 is horizontal, one velocity head 1V 2 2g2 above the hydraulic<br />
grade line 1HGL2, which is one pressure head 1gz2 above the pipe<br />
itself. For cases 1b2 or 1c2 the energy line is not horizontal. Each bit<br />
of friction in the pipe or loss in a component reduces the available<br />
H, elevation to energy line, ft<br />
p, psi<br />
F I G U R E E8.8b<br />
80<br />
60<br />
40<br />
20<br />
30<br />
20<br />
10<br />
30.5 psi<br />
27.1 27.8<br />
(a) No losses<br />
(c) Including all<br />
losses<br />
Pressure<br />
loss<br />
20.2 21.0<br />
18.5 19.3<br />
10.7<br />
Elevation<br />
and<br />
kinetic<br />
energy<br />
10.7<br />
0<br />
0 10 20 30 40 50 60<br />
Slope due to pipe friction<br />
Sharp drop due to component loss<br />
Energy line including all<br />
losses, case (c)<br />
Energy line with no losses, case (a)<br />
0 0 10 20 30 40 50 60<br />
Distance along pipe from point (1), ft<br />
F I G U R E E8.8c<br />
11.7<br />
12.4<br />
Distance along pipe from point (1), ft<br />
9.93<br />
6.37<br />
3.09<br />
6.37<br />
4.84<br />
2.07<br />
2.07 p 2 = 0<br />
Location: (1) (3) (4) (5) (6) (7)(8) (2)