fluid_mechanics
562 Chapter 10 ■ Open-Channel Flow z V 1 2 ___ 2g Energy line Free surface and hydraulic grade line h B u 2 (h) H h dh B A V 1 z A P w x (a) F I G U R E 10.20 Assumed flow structure over a weir. (b) A V A p A /g where h is the distance that point B is below the free surface. We do not know the location of point A from which came the fluid that passes over the weir at point B. However, since the total head for any particle along the vertical section 112 is the same, z H P w V 2 A p Ag V 2 12g 12g, the specific location of A 1i.e., A or A shown in the figure in the margin2 is not needed, and the velocity of the fluid over the weir plate is obtained from Eq. 10.26 as p A /g A u 2 B 2g ah V 2 1 2g b Z A V A Z A The flowrate can be calculated from hH Q 122 u 2 dA u 2 / dh h0 (10.27) where / /1h2 is the cross-channel width of a strip of the weir area, as is indicated in Fig. 10.20b. For a rectangular weir / is constant. For other weirs, such as triangular or circular weirs, the value of / is known as a function of h. For a rectangular weir, / b, and the flowrate becomes or Q 12g b H 0 ah V 2 1 2g b 12 dh Q 2 3 12g b caH V 2 1 2g b 32 a V 2 1 2g b 32 d (10.28) Equation 10.28 is a rather cumbersome expression that can be simplified by using the fact that with P w H 1as often happens in practical situations2 the upstream velocity is negligibly small. That is, V 2 12g H and Eq. 10.28 simplifies to the basic rectangular weir equation A weir coefficient is used to account for nonideal conditions excluded in the simplified analysis. Q 2 3 12g b H 3 2 (10.29) Note that the weir head, H, is the height of the upstream free surface above the crest of the weir. As is indicated in Fig. 10.18, because of the drawdown effect, H is not the distance of the free surface above the weir crest as measured directly above the weir plate. Because of the numerous approximations made to obtain Eq. 10.29, it is not unexpected that an experimentally determined correction factor must be used to obtain the actual flowrate as a function of weir head. Thus, the final form is Q C wr 2 3 12g b H 3 2 (10.30)
C wr 1 10.6 Rapidly Varied Flow 563 where C wr is the rectangular weir coefficient. From dimensional analysis arguments, it is expected that C wr is a function of Reynolds number 1viscous effects2, Weber number 1surface tension effects2, and HP w 1geometry2. In most practical situations, the Reynolds and Weber number effects are negligible, and the following correlation, shown in the figure in the margin, can be used 1Refs. 4, 72: 0 0 1 C wr 0.611 0.075 a H P w b (10.31) H/P w V10.13 Triangular weir C wr More precise values of can be found in the literature, if needed 1Refs. 3, 142. The triangular sharp-crested weir is often used for flow measurements, particularly for measuring flowrates over a wide range of values. For small flowrates, the head, H, for a rectangular weir would be very small and the flowrate could not be measured accurately. However, with the triangular weir, the flow width decreases as H decreases so that even for small flowrates, reasonable heads are developed. Accurate results can be obtained over a wide range of Q. The triangular weir equation can be obtained from Eq. 10.27 by using / 21H h2 tan a u 2 b where u is the angle of the V-notch 1see Figs. 10.19 and 10.202. After carrying out the integration and again neglecting the upstream velocity 1V 2 12g H2, we obtain Q 8 15 tan au 2 b 12g H 5 2 An experimentally determined triangular weir coefficient, C wt , is used to account for the real-world effects neglected in the analysis so that Q C wt 8 15 tan au 2 b 12g H 5 2 (10.32) V10.14 Low-head dam C wt Typical values of for triangular weirs are in the range of 0.58 to 0.62, as is shown in Fig. 10.21. Note that although C wt and u are dimensionless, the value of C wt is given as a function of the weir head, H, which is a dimensional quantity. Although using dimensional parameters is not recommended 1see the dimensional analysis discussion in Chapter 72, such parameters are often used for open-channel flow. 0.66 θ = 20° 0.64 0.62 45° 60° C wt 90° 0.60 0.58 0.56 Minimum C wt for all θ 0 0.2 0.4 0.6 0.8 1.0 H, ft F I G U R E 10.21 Weir coefficient for triangular sharp-crested weirs (Ref. 10).
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C wr<br />
1<br />
10.6 Rapidly Varied Flow 563<br />
where C wr is the rectangular weir coefficient. From dimensional analysis arguments, it is expected<br />
that C wr is a function of Reynolds number 1viscous effects2, Weber number 1surface tension<br />
effects2, and HP w 1geometry2. In most practical situations, the Reynolds and Weber number<br />
effects are negligible, and the following correlation, shown in the figure in the margin, can be<br />
used 1Refs. 4, 72:<br />
0<br />
0 1<br />
C wr 0.611 0.075 a H P w<br />
b<br />
(10.31)<br />
H/P w<br />
V10.13 Triangular<br />
weir<br />
C wr<br />
More precise values of can be found in the literature, if needed 1Refs. 3, 142.<br />
The triangular sharp-crested weir is often used for flow measurements, particularly for<br />
measuring flowrates over a wide range of values. For small flowrates, the head, H, for a rectangular<br />
weir would be very small and the flowrate could not be measured accurately. However, with the<br />
triangular weir, the flow width decreases as H decreases so that even for small flowrates, reasonable<br />
heads are developed. Accurate results can be obtained over a wide range of Q.<br />
The triangular weir equation can be obtained from Eq. 10.27 by using<br />
/ 21H h2 tan a u 2 b<br />
where u is the angle of the V-notch 1see Figs. 10.19 and 10.202. After carrying out the integration<br />
and again neglecting the upstream velocity 1V 2 12g H2, we obtain<br />
Q 8<br />
15 tan au 2 b 12g H 5 2<br />
An experimentally determined triangular weir coefficient, C wt , is used to account for the real-world<br />
effects neglected in the analysis so that<br />
Q C wt 8 15 tan au 2 b 12g H 5 2<br />
(10.32)<br />
V10.14 Low-head<br />
dam<br />
C wt<br />
Typical values of for triangular weirs are in the range of 0.58 to 0.62, as is shown in Fig. 10.21.<br />
Note that although C wt and u are dimensionless, the value of C wt is given as a function of the<br />
weir head, H, which is a dimensional quantity. Although using dimensional parameters is not<br />
recommended 1see the dimensional analysis discussion in Chapter 72, such parameters are often<br />
used for open-channel flow.<br />
0.66<br />
θ = 20°<br />
0.64<br />
0.62<br />
45°<br />
60°<br />
C wt 90°<br />
0.60<br />
0.58<br />
0.56<br />
Minimum C wt for all θ<br />
0 0.2 0.4 0.6 0.8 1.0<br />
H, ft<br />
F I G U R E 10.21 Weir coefficient<br />
for triangular sharp-crested weirs (Ref. 10).