fluid_mechanics
118 Chapter 3 ■ Elementary Fluid Dynamics—The Bernoulli Equation SOLUTION (2) If the flow is steady, inviscid, and incompressible we can apply the Bernoulli equation along the streamline from 112 to 122 to 132 as follows: p 1 1 2rV 2 1 gz 1 p 2 1 2rV 2 2 gz 2 p 3 1 2rV 2 3 gz 3 With the tank bottom as the datum, we have z 1 15 ft, z 2 H, and z 3 5 ft. Also, V 1 0 1large tank2, p 1 0 1open tank2, p 3 0 1free jet2, and from the continuity equation A 2 V 2 A 3 V 3 , or because the hose is constant diameter, V 2 V 3 . Thus, the speed of the fluid in the hose is determined from Eq. 1 to be V 3 22g1z 1 z 3 2 22132.2 fts 2 2315 1524 ft (1) (3) (1) 35.9 fts V 2 Use of Eq. 1 between points 112 and 122 then gives the pressure p 2 at the top of the hill as p 2 p 1 1 2rV 2 1 gz 1 1 2rV 2 2 gz 2 From Table B.1, the vapor pressure of water at 60 °F is 0.256 psia. Hence, for incipient cavitation the lowest pressure in the system will be p 0.256 psia. Careful consideration of Eq. 2 and Fig. E3.10b will show that this lowest pressure will occur at the top of the hill. Since we have used gage pressure at point 112 1 p 1 02, we must use gage pressure at point 122 also. Thus, p 2 0.256 14.7 14.4 psi and Eq. 2 gives 114.4 lbin. 2 21144 in. 2 ft 2 2 162.4 lbft 3 2115 H2ft 1 2 11.94 slugsft 3 2135.9 fts2 2 or g1z 1 z 2 2 1 2rV 2 2 H 28.2 ft (2) (Ans) For larger values of H, vapor bubbles will form at point 122 and the siphon action may stop. COMMENTS Note that we could have used absolute pressure throughout 1p 2 0.256 psia and p 1 14.7 psia2 and obtained the same result. The lower the elevation of point 132, the larger the flowrate and, therefore, the smaller the value of H allowed. We could also have used the Bernoulli equation between 122 and 132, with V 2 V 3 , to obtain the same value of H. In this case it would not have been necessary to determine V 2 by use of the Bernoulli equation between 112 and 132. The above results are independent of the diameter and length of the hose 1provided viscous effects are not important2. Proper design of the hose 1or pipe2 is needed to ensure that it will not collapse due to the large pressure difference 1vacuum2 between the inside and outside of the hose. 15 ft F I G U R E E3.10a (1) Water H (2) 5 ft F I G U R E E3.10b By using the fluid properties listed in Table 1.5 and repeating the calculations for various fluids, the results shown in Fig. E3.10c are obtained. The value of H is a function of both the specific weight of the fluid, g, and its vapor pressure, . H, ft 40 35 30 25 20 15 10 5 0 Alcohol Water Fluid F I G U R E E3.10c Gasoline (3) Carbon tet p v 3.6.3 Flowrate Measurement Many types of devices using principles involved in the Bernoulli equation have been developed to measure fluid velocities and flowrates. The Pitot-static tube discussed in Section 3.5 is an example. Other examples discussed below include devices to measure flowrates in pipes and
3.6 Examples of Use of the Bernoulli Equation 119 (1) (2) Orifice Nozzle Venturi (1) (2) F I G U R E 3.18 Typical devices for measuring flowrate in pipes. conduits and devices to measure flowrates in open channels. In this chapter we will consider “ideal” flow meters—those devoid of viscous, compressibility, and other “real-world” effects. Corrections for these effects are discussed in Chapters 8 and 10. Our goal here is to understand the basic operating principles of these simple flow meters. An effective way to measure the flowrate through a pipe is to place some type of restriction within the pipe as shown in Fig. 3.18 and to measure the pressure difference between the low-velocity, high-pressure upstream section 112, and the high-velocity, low-pressure downstream section 122. Three commonly used types of flow meters are illustrated: the orifice meter, the nozzle meter, and the Venturi meter. The operation of each is based on the same physical principles— an increase in velocity causes a decrease in pressure. The difference between them is a matter of cost, accuracy, and how closely their actual operation obeys the idealized flow assumptions. We assume the flow is horizontal 1z 1 z 2 2, steady, inviscid, and incompressible between points 112 and 122. The Bernoulli equation becomes p 1 1 2rV 2 1 p 2 1 2rV 2 2 1The effect of nonhorizontal flow can be incorporated easily by including the change in elevation, z 1 z 2 , in the Bernoulli equation.2 If we assume the velocity profiles are uniform at sections 112 and 122, the continuity equation 1Eq. 3.192 can be written as Q The flowrate varies as the square root of the pressure difference across the flow meter. Q ~ Δp Δp = p 1 – p 2 Q A 1 V 1 A 2 V 2 where A 2 is the small 1A 2 6 A 1 2 flow area at section 122. Combination of these two equations results in the following theoretical flowrate Q A 2 B 21p 1 p 2 2 r31 1A 2A 1 2 2 4 (3.20) Thus, as shown by the figure in the margin, for a given flow geometry 1A 1 and A 2 2 the flowrate can be determined if the pressure difference, p 1 p 2 , is measured. The actual measured flowrate, Q actual , will be smaller than this theoretical result because of various differences between the “real world” and the assumptions used in the derivation of Eq. 3.20. These differences 1which are quite consistent and may be as small as 1 to 2% or as large as 40%, depending on the geometry used2 can be accounted for by using an empirically obtained discharge coefficient as discussed in Section 8.6.1.
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118 Chapter 3 ■ Elementary Fluid Dynamics—The Bernoulli Equation<br />
SOLUTION<br />
(2)<br />
If the flow is steady, inviscid, and incompressible we can apply<br />
the Bernoulli equation along the streamline from 112 to 122 to 132 as<br />
follows:<br />
p 1 1 2rV 2 1 gz 1 p 2 1 2rV 2 2 gz 2<br />
p 3 1 2rV 2 3 gz 3<br />
With the tank bottom as the datum, we have z 1 15 ft, z 2 H,<br />
and z 3 5 ft. Also, V 1 0 1large tank2, p 1 0 1open tank2,<br />
p 3 0 1free jet2, and from the continuity equation A 2 V 2 A 3 V 3 , or<br />
because the hose is constant diameter, V 2 V 3 . Thus, the speed of<br />
the <strong>fluid</strong> in the hose is determined from Eq. 1 to be<br />
V 3 22g1z 1 z 3 2 22132.2 fts 2 2315 1524 ft<br />
(1)<br />
(3)<br />
(1)<br />
35.9 fts V 2<br />
Use of Eq. 1 between points 112 and 122 then gives the pressure p 2<br />
at the top of the hill as<br />
p 2 p 1 1 2rV 2 1 gz 1 1 2rV 2 2 gz 2<br />
From Table B.1, the vapor pressure of water at 60 °F is<br />
0.256 psia. Hence, for incipient cavitation the lowest pressure in<br />
the system will be p 0.256 psia. Careful consideration of Eq. 2<br />
and Fig. E3.10b will show that this lowest pressure will occur at<br />
the top of the hill. Since we have used gage pressure at point 112<br />
1 p 1 02, we must use gage pressure at point 122 also. Thus,<br />
p 2 0.256 14.7 14.4 psi and Eq. 2 gives<br />
114.4 lbin. 2 21144 in. 2 ft 2 2<br />
162.4 lbft 3 2115 H2ft 1 2 11.94 slugsft 3 2135.9 fts2 2<br />
or<br />
g1z 1 z 2 2 1 2rV 2 2<br />
H 28.2 ft<br />
(2)<br />
(Ans)<br />
For larger values of H, vapor bubbles will form at point 122 and the<br />
siphon action may stop.<br />
COMMENTS Note that we could have used absolute pressure<br />
throughout 1p 2 0.256 psia and p 1 14.7 psia2 and obtained<br />
the same result. The lower the elevation of point 132, the<br />
larger the flowrate and, therefore, the smaller the value of H allowed.<br />
We could also have used the Bernoulli equation between 122<br />
and 132, with V 2 V 3 , to obtain the same value of H. In this case<br />
it would not have been necessary to determine V 2 by use of the<br />
Bernoulli equation between 112 and 132.<br />
The above results are independent of the diameter and length<br />
of the hose 1provided viscous effects are not important2. Proper<br />
design of the hose 1or pipe2 is needed to ensure that it will not collapse<br />
due to the large pressure difference 1vacuum2 between the<br />
inside and outside of the hose.<br />
15 ft<br />
F I G U R E E3.10a<br />
(1)<br />
Water<br />
H<br />
(2)<br />
5 ft<br />
F I G U R E E3.10b<br />
By using the <strong>fluid</strong> properties listed in Table 1.5 and repeating<br />
the calculations for various <strong>fluid</strong>s, the results shown in<br />
Fig. E3.10c are obtained. The value of H is a function of both the<br />
specific weight of the <strong>fluid</strong>, g, and its vapor pressure, .<br />
H, ft<br />
40<br />
35<br />
30<br />
25<br />
20<br />
15<br />
10<br />
5<br />
0<br />
Alcohol<br />
Water<br />
Fluid<br />
F I G U R E E3.10c<br />
Gasoline<br />
(3)<br />
Carbon tet<br />
p v<br />
3.6.3 Flowrate Measurement<br />
Many types of devices using principles involved in the Bernoulli equation have been developed<br />
to measure <strong>fluid</strong> velocities and flowrates. The Pitot-static tube discussed in Section 3.5 is an<br />
example. Other examples discussed below include devices to measure flowrates in pipes and