fluid_mechanics
548 Chapter 10 ■ Open-Channel Flow τ = 0 y 1 = y 2 Control surface F 1 V 1 (1) V 2 = V 1 θ τ P w y 2 F 2 θ = γ A sin θ (2) x F I G U R E 10.10 Control volume for uniform flow in an open channel. p(y) y 1 y y 2 = y 1 Equal pressure distributions where F 1 and F 2 are the hydrostatic pressure forces across either end of the control volume, as shown by the figure in the margin. Because the flow is at a uniform depth 1y 1 y 2 2, it follows that F 1 F 2 so that these two forces do not contribute to the force balance. The term wsin u is the component of the fluid weight that acts down the slope, and t w P/ is the shear force on the fluid, acting up the slope as a result of the interaction of the water and the channel’s wetted perimeter. Thus, Eq. 10.15 becomes t w w sin u P/ w S 0 P/ where we have used the approximation that sin u tan u S 0 , since the bottom slope is typically very small 1i.e., S 0 12. Since w gA/ and the hydraulic radius is defined as R h AP, the force balance equation becomes f For uniform depth, channel flow is governed by a balance between friction and weight. e f = f D Re Wholly turbulent (10.16) Most open-channel flows are turbulent rather than laminar. In fact, typical Reynolds numbers are quite large, well above the transitional value and into the wholly turbulent regime. As was discussed in Chapter 8, and shown by the figure in the margin, for very large Reynolds number pipe flows 1wholly turbulent flows2, the friction factor, f, is found to be independent of Reynolds number, dependent only on the relative roughness, eD, of the pipe surface. For such cases, the wall shear stress is proportional to the dynamic pressure, rV 2 2, and independent of the viscosity. That is, where K is a constant dependent upon the roughness of the pipe. It is not unreasonable that similar shear stress dependencies occur for the large Reynolds number open-channel flows. In such situations, Eq. 10.16 becomes or t w gA/S 0 P/ t w Kr V 2 gR h S 0 Kr V 2 2 gR hS 0 V C 2R h S 0 (10.17) where the constant C is termed the Chezy coefficient and Eq. 10.17 is termed the Chezy equation. This equation, one of the oldest in the area of fluid mechanics, was developed in 1768 by A. Chezy 11718–17982, a French engineer who designed a canal for the Paris water supply. The value of the Chezy coefficient, which must be determined by experiments, is not dimensionless but has the dimensions of 1length2 1 2 per time 1i.e., the square root of the units of acceleration2. From a series of experiments it was found that the slope dependence of Eq. 10.17 1V S 12 0 2 23 is reasonable, but that the dependence on the hydraulic radius is more nearly V R h rather than V R 12 h . In 1889, R. Manning 11816–18972, an Irish engineer, developed the following somewhat modified equation for open-channel flow to more accurately describe the dependence: 2 R h V R2 3 12 h S 0 n (10.18)
10.4 Uniform Depth Channel Flow 549 TABLE 10.1 Values of the Manning Coefficient, n (Ref. 6) Wetted Perimeter n Wetted Perimeter n A. Natural channels Clean and straight 0.030 Sluggish with deep pools 0.040 Major rivers 0.035 B. Floodplains Pasture, farmland 0.035 Light brush 0.050 Heavy brush 0.075 Trees 0.15 C. Excavated earth channels Clean 0.022 Gravelly 0.025 Weedy 0.030 Stony, cobbles 0.035 D. Artificially lined channels Glass 0.010 Brass 0.011 Steel, smooth 0.012 Steel, painted 0.014 Steel, riveted 0.015 Cast iron 0.013 Concrete, finished 0.012 Concrete, unfinished 0.014 Planed wood 0.012 Clay tile 0.014 Brickwork 0.015 Asphalt 0.016 Corrugated metal 0.022 Rubble masonry 0.025 The Manning equation is used to obtain the velocity or flowrate in an open channel. Equation 10.18 is termed the Manning equation, and the parameter n is the Manning resistance coefficient. Its value is dependent on the surface material of the channel’s wetted perimeter and is obtained from experiments. It is not dimensionless, having the units of sm 1 3 or sft 13 . As is discussed in Chapter 7, any correlation should be expressed in dimensionless form, with the coefficients that appear being dimensionless coefficients, such as the friction factor for pipe flow or the drag coefficient for flow past objects. Thus, Eq. 10.18 should be expressed in dimensionless form. Unfortunately, the Manning equation is so widely used and has been used for so long that it will continue to be used in its dimensional form with a coefficient, n, that is not dimensionless. The values of n found in the literature 1such as Table 10.12 were developed for SI units. Standard practice is to use the same value of n when using the BG system of units, and to insert a conversion factor into the equation. Thus, uniform flow in an open channel is obtained from the Manning equation written as V k n R h 2 3 S 0 12 (10.19) and Q k n AR h 2 3 S 1 2 0 (10.20) Q 0 Pasture, farmland Light brush Heavy brush 0.05 n 0.1 Trees 0.15 where k 1 if SI units are used, and k 1.49 if BG units are used. The value 1.49 is the cube root of the number of feet per meter: 13.281 ftm2 13 1.49. Thus, by using R in meters, A in m 2 h , and k 1, the average velocity is ms and the flowrate m 3 s. By using R in feet, A in ft 2 h , and k 1.49, the average velocity is fts and the flowrate ft 3 s. Typical values of the Manning coefficient are indicated in Table 10.1. As expected, the rougher the wetted perimeter, the larger the value of n. For example, the roughness of floodplain surfaces increases from pasture to brush to tree conditions. So does the corresponding value of the Manning coefficient. Thus, for a given depth of flooding, the flowrate varies with floodplain roughness as indicated by the figure in the margin. Precise values of n are often difficult to obtain. Except for artificially lined channel surfaces like those found in new canals or flumes, the channel surface structure may be quite complex and variable. There are various methods used to obtain a reasonable estimate of the value of n for a given situation 1Ref. 52. For the purpose of this book, the values from Table 10.1 are sufficient. Note that the error in Q is directly proportional to the error in n. A 10%
- Page 522 and 523: 498 Chapter 9 ■ Flow over Immerse
- Page 524 and 525: 500 Chapter 9 ■ Flow over Immerse
- Page 526 and 527: 502 Chapter 9 ■ Flow over Immerse
- Page 528 and 529: 504 Chapter 9 ■ Flow over Immerse
- Page 530 and 531: 506 Chapter 9 ■ Flow over Immerse
- Page 532 and 533: 508 Chapter 9 ■ Flow over Immerse
- Page 534 and 535: 510 Chapter 9 ■ Flow over Immerse
- Page 536 and 537: 512 Chapter 9 ■ Flow over Immerse
- Page 538 and 539: 514 Chapter 9 ■ Flow over Immerse
- Page 540 and 541: 516 Chapter 9 ■ Flow over Immerse
- Page 542 and 543: 518 Chapter 9 ■ Flow over Immerse
- Page 544 and 545: 520 Chapter 9 ■ Flow over Immerse
- Page 546 and 547: 522 Chapter 9 ■ Flow over Immerse
- Page 548 and 549: 524 Chapter 9 ■ Flow over Immerse
- Page 550 and 551: 526 Chapter 9 ■ Flow over Immerse
- Page 552 and 553: 528 Chapter 9 ■ Flow over Immerse
- Page 554 and 555: ∋ 530 Chapter 9 ■ Flow over Imm
- Page 556 and 557: 532 Chapter 9 ■ Flow over Immerse
- Page 558 and 559: 10 Open-Channel Flow CHAPTER OPENIN
- Page 560 and 561: 536 Chapter 10 ■ Open-Channel Flo
- Page 562 and 563: 538 Chapter 10 ■ Open-Channel Flo
- Page 564 and 565: 540 Chapter 10 ■ Open-Channel Flo
- Page 566 and 567: 542 Chapter 10 ■ Open-Channel Flo
- Page 568 and 569: 544 Chapter 10 ■ Open-Channel Flo
- Page 570 and 571: 546 Chapter 10 ■ Open-Channel Flo
- Page 574 and 575: 550 Chapter 10 ■ Open-Channel Flo
- Page 576 and 577: 552 Chapter 10 ■ Open-Channel Flo
- Page 578 and 579: 554 Chapter 10 ■ Open-Channel Flo
- Page 580 and 581: 556 Chapter 10 ■ Open-Channel Flo
- Page 582 and 583: 558 Chapter 10 ■ Open-Channel Flo
- Page 584 and 585: 560 Chapter 10 ■ Open-Channel Flo
- Page 586 and 587: 562 Chapter 10 ■ Open-Channel Flo
- Page 588 and 589: 564 Chapter 10 ■ Open-Channel Flo
- Page 590 and 591: 566 Chapter 10 ■ Open-Channel Flo
- Page 592 and 593: 568 Chapter 10 ■ Open-Channel Flo
- Page 594 and 595: 570 Chapter 10 ■ Open-Channel Flo
- Page 596 and 597: 572 Chapter 10 ■ Open-Channel Flo
- Page 598 and 599: 574 Chapter 10 ■ Open-Channel Flo
- Page 600 and 601: 576 Chapter 10 ■ Open-Channel Flo
- Page 602 and 603: 578 Chapter 10 ■ Open-Channel Flo
- Page 604 and 605: 580 Chapter 11 ■ Compressible Flo
- Page 606 and 607: 582 Chapter 11 ■ Compressible Flo
- Page 608 and 609: 584 Chapter 11 ■ Compressible Flo
- Page 610 and 611: 586 Chapter 11 ■ Compressible Flo
- Page 612 and 613: 588 Chapter 11 ■ Compressible Flo
- Page 614 and 615: 590 Chapter 11 ■ Compressible Flo
- Page 616 and 617: 592 Chapter 11 ■ Compressible Flo
- Page 618 and 619: 594 Chapter 11 ■ Compressible Flo
- Page 620 and 621: 596 Chapter 11 ■ Compressible Flo
10.4 Uniform Depth Channel Flow 549<br />
TABLE 10.1<br />
Values of the Manning Coefficient, n (Ref. 6)<br />
Wetted Perimeter n Wetted Perimeter n<br />
A. Natural channels<br />
Clean and straight 0.030<br />
Sluggish with deep pools 0.040<br />
Major rivers 0.035<br />
B. Floodplains<br />
Pasture, farmland 0.035<br />
Light brush 0.050<br />
Heavy brush 0.075<br />
Trees 0.15<br />
C. Excavated earth channels<br />
Clean 0.022<br />
Gravelly 0.025<br />
Weedy 0.030<br />
Stony, cobbles 0.035<br />
D. Artificially lined channels<br />
Glass 0.010<br />
Brass 0.011<br />
Steel, smooth 0.012<br />
Steel, painted 0.014<br />
Steel, riveted 0.015<br />
Cast iron 0.013<br />
Concrete, finished 0.012<br />
Concrete, unfinished 0.014<br />
Planed wood 0.012<br />
Clay tile 0.014<br />
Brickwork 0.015<br />
Asphalt 0.016<br />
Corrugated metal 0.022<br />
Rubble masonry 0.025<br />
The Manning equation<br />
is used to obtain<br />
the velocity or<br />
flowrate in an open<br />
channel.<br />
Equation 10.18 is termed the Manning equation, and the parameter n is the Manning resistance<br />
coefficient. Its value is dependent on the surface material of the channel’s wetted perimeter and is<br />
obtained from experiments. It is not dimensionless, having the units of sm 1 3<br />
or sft 13 .<br />
As is discussed in Chapter 7, any correlation should be expressed in dimensionless form,<br />
with the coefficients that appear being dimensionless coefficients, such as the friction factor for<br />
pipe flow or the drag coefficient for flow past objects. Thus, Eq. 10.18 should be expressed in<br />
dimensionless form. Unfortunately, the Manning equation is so widely used and has been used for<br />
so long that it will continue to be used in its dimensional form with a coefficient, n, that is not<br />
dimensionless. The values of n found in the literature 1such as Table 10.12 were developed for SI<br />
units. Standard practice is to use the same value of n when using the BG system of units, and to<br />
insert a conversion factor into the equation.<br />
Thus, uniform flow in an open channel is obtained from the Manning equation written as<br />
V k n R h 2 3 S 0<br />
12<br />
(10.19)<br />
and<br />
Q k n AR h 2 3 S 1 2<br />
0<br />
(10.20)<br />
Q<br />
0<br />
Pasture, farmland<br />
Light brush<br />
Heavy brush<br />
0.05<br />
n<br />
0.1<br />
Trees<br />
0.15<br />
where k 1 if SI units are used, and k 1.49 if BG units are used. The value 1.49 is the cube<br />
root of the number of feet per meter: 13.281 ftm2 13 1.49. Thus, by using R in meters, A in m 2 h<br />
,<br />
and k 1, the average velocity is ms and the flowrate m 3 s. By using R in feet, A in ft 2 h<br />
, and<br />
k 1.49, the average velocity is fts and the flowrate ft 3 s.<br />
Typical values of the Manning coefficient are indicated in Table 10.1. As expected, the<br />
rougher the wetted perimeter, the larger the value of n. For example, the roughness of floodplain<br />
surfaces increases from pasture to brush to tree conditions. So does the corresponding value of<br />
the Manning coefficient. Thus, for a given depth of flooding, the flowrate varies with floodplain<br />
roughness as indicated by the figure in the margin.<br />
Precise values of n are often difficult to obtain. Except for artificially lined channel<br />
surfaces like those found in new canals or flumes, the channel surface structure may be quite<br />
complex and variable. There are various methods used to obtain a reasonable estimate of the<br />
value of n for a given situation 1Ref. 52. For the purpose of this book, the values from Table<br />
10.1 are sufficient. Note that the error in Q is directly proportional to the error in n. A 10%