fluid_mechanics
120 Chapter 3 ■ Elementary Fluid Dynamics—The Bernoulli Equation E XAMPLE 3.11 Venturi Meter GIVEN Kerosene 1SG 0.852 flows through the Venturi meter shown in Fig. E3.11a with flowrates between 0.005 and 0.050 m 3 s. FIND Determine the range in pressure difference, p 1 p 2 , needed to measure these flowrates. Kerosene, SG = 0.85 D 1 = 0.1 m (2) D 2 = 0.06 m (1) 0.005 m 3 /s < Q < 0.050 m 3 /s F I G U R E E3.11a Q SOLUTION If the flow is assumed to be steady, inviscid, and incompressible, the relationship between flowrate and pressure is given by Eq. 3.20. This can be rearranged to give With the density of the flowing fluid and the area ratio the pressure difference for the smallest flowrate is Likewise, the pressure difference for the largest flowrate is Thus, p 1 p 2 Q2 r31 1A 2A 1 2 2 4 2 A 2 2 r SG r H2 O 0.8511000 kgm 3 2 850 kgm 3 A 2A 1 1D 2D 1 2 2 10.06 m0.10 m2 2 0.36 11 0.36 2 2 p 1 p 2 10.005 m 3 s2 2 1850 kgm 3 2 2 31p4210.06 m2 2 4 2 1160 Nm 2 1.16 kPa 11 0.36 2 2 p 1 p 2 10.052 2 18502 231p4210.062 2 4 2 1.16 10 5 Nm 2 116 kPa 1.16 kPa p 1 p 2 116 kPa (Ans) COMMENTS These values represent the pressure differences for inviscid, steady, incompressible conditions. The ideal results presented here are independent of the particular flow meter geometry—an orifice, nozzle, or Venturi meter 1see Fig. 3.182. It is seen from Eq. 3.20 that the flowrate varies as the square root of the pressure difference. Hence, as indicated by the numerical results and shown in Fig. E3.11b, a 10-fold increase in flowrate requires a 100-fold increase in pressure difference. This nonlinear relationship can cause difficulties when measuring flowrates over a wide range of values. Such measurements would require pressure transducers with a wide range of operation. An alternative is to use two flow meters in parallel—one for the larger and one for the smaller flowrate ranges. p 1 –p 2 , kPa 120 100 80 60 40 20 0 0 (0.005 m 3 /s, 1.16 kPa) F I G U R E E3.11b (0.05 m 3 /s, 116 kPa) 0.01 0.02 0.03 0.04 0.05 Q, m 3 /s Other flow meters based on the Bernoulli equation are used to measure flowrates in open channels such as flumes and irrigation ditches. Two of these devices, the sluice gate and the sharp-crested weir, are discussed below under the assumption of steady, inviscid, incompressible flow. These and other open-channel flow devices are discussed in more detail in Chapter 10. Sluice gates like those shown in Fig. 3.19a are often used to regulate and measure the flowrate in open channels. As indicated in Fig. 3.19b, the flowrate, Q, is a function of the water depth upstream, z 1 , the width of the gate, b, and the gate opening, a. Application of the Bernoulli equation and continuity equation between points 112 and 122 can provide a good approximation to the actual flowrate obtained. We assume the velocity profiles are uniform sufficiently far upstream and downstream of the gate.
3.6 Examples of Use of the Bernoulli Equation 121 V 1 z 1 a Sluice gates (1) Sluice gate width = b b z 2 V 2 (2) Q a (3) (4) (a) F I G U R E 3.19 (b) Sluice gate geometry. (Photograph courtesy of Plasti-Fab, Inc.) give Thus, we apply the Bernoulli equation between points on the free surfaces at 112 and 122 to p 1 1 2rV 2 1 gz 1 p 2 1 2rV 2 2 gz 2 Also, if the gate is the same width as the channel so that A 1 bz 1 and A 2 bz 2 , the continuity equation gives The flowrate under a sluice gate depends on the water depths on either side of the gate. Q A 1 V 1 bV 1 z 1 A 2 V 2 bV 2 z 2 With the fact that p 1 p 2 0, these equations can be combined and rearranged to give the flowrate as 2g1z 1 z 2 2 Q z 2 b B 1 1z 2z 1 2 2 In the limit of z 1 z 2 this result simply becomes (3.21) Q z 2 b12gz 1 This limiting result represents the fact that if the depth ratio, z 1z 2 , is large, the kinetic energy of the fluid upstream of the gate is negligible and the fluid velocity after it has fallen a distance 1z 1 z 2 2 z 1 is approximately V 2 12gz 1 . The results of Eq. 3.21 could also be obtained by using the Bernoulli equation between points 132 and 142 and the fact that p 3 gz 1 and p 4 gz 2 since the streamlines at these sections are straight. In this formulation, rather than the potential energies at 112 and 122, we have the pressure contributions at 132 and 142. The downstream depth, z 2 , not the gate opening, a, was used to obtain the result of Eq. 3.21. As was discussed relative to flow from an orifice 1Fig. 3.142, the fluid cannot turn a sharp 90° corner. A vena contracta results with a contraction coefficient, C c z 2a, less than 1. Typically C c is approximately 0.61 over the depth ratio range of 0 6 az 1 6 0.2. For larger values of az 1 the value of C c increases rapidly. E XAMPLE 3.12 Sluice Gate GIVEN Water flows under the sluice gate shown in Fig. E3.12a. FIND Determine the approximate flowrate per unit width of the channel.
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120 Chapter 3 ■ Elementary Fluid Dynamics—The Bernoulli Equation<br />
E XAMPLE 3.11<br />
Venturi Meter<br />
GIVEN Kerosene 1SG 0.852 flows through the Venturi<br />
meter shown in Fig. E3.11a with flowrates between 0.005 and<br />
0.050 m 3 s.<br />
FIND Determine the range in pressure difference, p 1 p 2 ,<br />
needed to measure these flowrates.<br />
Kerosene, SG = 0.85<br />
D 1 = 0.1 m<br />
(2) D 2 = 0.06 m<br />
(1)<br />
0.005 m 3 /s < Q < 0.050 m 3 /s<br />
F I G U R E E3.11a<br />
Q<br />
SOLUTION<br />
If the flow is assumed to be steady, inviscid, and incompressible,<br />
the relationship between flowrate and pressure is given by Eq.<br />
3.20. This can be rearranged to give<br />
With the density of the flowing <strong>fluid</strong><br />
and the area ratio<br />
the pressure difference for the smallest flowrate is<br />
Likewise, the pressure difference for the largest flowrate is<br />
Thus,<br />
p 1 p 2 Q2 r31 1A 2A 1 2 2 4<br />
2 A 2 2<br />
r SG r H2 O 0.8511000 kgm 3 2 850 kgm 3<br />
A 2A 1 1D 2D 1 2 2 10.06 m0.10 m2 2 0.36<br />
11 0.36 2 2<br />
p 1 p 2 10.005 m 3 s2 2 1850 kgm 3 2<br />
2 31p4210.06 m2 2 4 2<br />
1160 Nm 2 1.16 kPa<br />
11 0.36 2 2<br />
p 1 p 2 10.052 2 18502<br />
231p4210.062 2 4 2<br />
1.16 10 5 Nm 2 116 kPa<br />
1.16 kPa p 1 p 2 116 kPa<br />
(Ans)<br />
COMMENTS These values represent the pressure differences<br />
for inviscid, steady, incompressible conditions. The ideal<br />
results presented here are independent of the particular flow<br />
meter geometry—an orifice, nozzle, or Venturi meter 1see<br />
Fig. 3.182.<br />
It is seen from Eq. 3.20 that the flowrate varies as the<br />
square root of the pressure difference. Hence, as indicated by<br />
the numerical results and shown in Fig. E3.11b, a 10-fold increase<br />
in flowrate requires a 100-fold increase in pressure difference.<br />
This nonlinear relationship can cause difficulties when<br />
measuring flowrates over a wide range of values. Such measurements<br />
would require pressure transducers with a wide<br />
range of operation. An alternative is to use two flow meters in<br />
parallel—one for the larger and one for the smaller flowrate<br />
ranges.<br />
p 1<br />
–p 2 , kPa<br />
120<br />
100<br />
80<br />
60<br />
40<br />
20<br />
0<br />
0<br />
(0.005 m 3 /s, 1.16 kPa)<br />
F I G U R E E3.11b<br />
(0.05 m 3 /s, 116 kPa)<br />
0.01 0.02 0.03 0.04 0.05<br />
Q, m 3 /s<br />
Other flow meters based on the Bernoulli equation are used to measure flowrates in open channels<br />
such as flumes and irrigation ditches. Two of these devices, the sluice gate and the sharp-crested<br />
weir, are discussed below under the assumption of steady, inviscid, incompressible flow. These and<br />
other open-channel flow devices are discussed in more detail in Chapter 10.<br />
Sluice gates like those shown in Fig. 3.19a are often used to regulate and measure the flowrate<br />
in open channels. As indicated in Fig. 3.19b, the flowrate, Q, is a function of the water depth upstream,<br />
z 1 , the width of the gate, b, and the gate opening, a. Application of the Bernoulli equation<br />
and continuity equation between points 112 and 122 can provide a good approximation to the actual<br />
flowrate obtained. We assume the velocity profiles are uniform sufficiently far upstream and downstream<br />
of the gate.