fluid_mechanics
522 Chapter 9 ■ Flow over Immersed Bodies SOLUTION For horizontal flight, the lift generated by the spinning of the ball must exactly balance the weight, w, of the ball so that or where the lift coefficient, C L , can be obtained from Fig. 9.39. For standard atmospheric conditions with r 1.23 kgm 3 we obtain which, according to Fig. 9.39, can be achieved if or Thus, 0.244 v 2U10.92 D v 1568 rads2160 smin211 rev2p rad2 5420 rpm w l 1 2 rU 2 AC L C L 2w rU 2 1p42D 2 212.45 10 2 N2 C L 11.23 kgm 3 2112 ms2 2 1p4213.8 10 2 m2 2 vD 2U 0.9 2112 m s210.92 3.8 10 2 m 568 rad s (Ans) ω F I G U R E E9.16 COMMENT Is it possible to impart this angular velocity to the ball? With larger angular velocities the ball will rise and follow an upward curved path. Similar trajectories can be produced by a well-hit golf ball—rather than falling like a rock, the golf ball trajectory is actually curved up and the spinning ball travels a greater distance than one without spin. However, if topspin is imparted to the ball 1as in an improper tee shot2 the ball will curve downward more quickly than under the action of gravity alone— the ball is “topped” and a negative lift is generated. Similarly, rotation about a vertical axis will cause the ball to hook or slice to one side or the other. U Horizontal path with backspin Path without spin 9.5 Chapter Summary and Study Guide drag lift lift coefficient drag coefficient wake region boundary layer laminar boundary layer turbulent boundary layer boundary layer thickness transition free-stream velocity favorable pressure gradient adverse pressure gradient boundary layer separation friction drag pressure drag stall circulation Magnus effect In this chapter the flow past objects is discussed. It is shown how the pressure and shear stress distributions on the surface of an object produce the net lift and drag forces on the object. The character of flow past an object is a function of the Reynolds number. For large Reynolds number flows a thin boundary layer forms on the surface. Properties of this boundary layer flow are discussed. These include the boundary layer thickness, whether the flow is laminar or turbulent, and the wall shear stress exerted on the object. In addition, boundary layer separation and its relationship to the pressure gradient are considered. The drag, which contains portions due to friction (viscous) effects and pressure effects, is written in terms of the dimensionless drag coefficient. It is shown how the drag coefficient is a function of shape, with objects ranging from very blunt to very streamlined. Other parameters affecting the drag coefficient include the Reynolds number, Froude number, Mach number, and surface roughness. The lift is written in terms of the dimensionless lift coefficient, which is strongly dependent on the shape of the object. Variation of the lift coefficient with shape is illustrated by the variation of an airfoil’s lift coefficient with angle of attack. The following checklist provides a study guide for this chapter. When your study of the entire chapter and end-of-chapter exercises has been completed you should be able to write out meanings of the terms listed here in the margin and understand each of the related concepts. These terms are particularly important and are set in italic, bold, and color type in the text.
References 523 determine the lift and drag on an object from the given pressure and shear stress distributions on the object. for flow past a flat plate, calculate the boundary layer thickness, the wall shear stress, the friction drag, and determine whether the flow is laminar or turbulent. explain the concept of the pressure gradient and its relationship to boundary layer separation. for a given object, obtain the drag coefficient from appropriate tables, figures, or equations and calculate the drag on the object. explain why golf balls have dimples. for a given object, obtain the lift coefficient from appropriate figures and calculate the lift on the object. Some of the important equations in this chapter are: Lift coefficient and drag coefficient C C D d L l (9.39), (9.36) 1 1 2rU 2 A , 2rU 2 A Boundary layer displacement thickness d* a1 u (9.3) U b dy Boundary layer momentum thickness u (9.4) U a1 u U b dy Blasius boundary layer thickness, displacement thickness, and momentum thickness for flat plate d d * , , (9.15), (9.16), (9.17) x 0.664 x 1.721 x 5 1Re x 1Re x 1Re x rm Blasius wall shear stress for flat plate t w 0.332U 3 2 (9.18) B x Drag on flat plate d rbU 2 (9.23) Blasius wall friction coefficient and friction drag coefficient c , C (9.32) Df 1.328 f 0.664 for flat plate 1Re x 1Re / 0 0 References 1. Schlichting, H., Boundary Layer Theory, 8th Ed., McGraw-Hill, New York, 2000. 2. Rosenhead, L., Laminar Boundary Layers, Oxford University Press, London, 1963. 3. White, F. M., Viscous Fluid Flow, 3rd Ed., McGraw-Hill, New York, 2005. 4. Currie, I. G., Fundamental Mechanics of Fluids, McGraw-Hill, New York, 1974. 5. Blevins, R. D., Applied Fluid Dynamics Handbook, Van Nostrand Reinhold, New York, 1984. 6. Hoerner, S. F., Fluid-Dynamic Drag, published by the author, Library of Congress No. 64,19666, 1965. 7. Happel, J., Low Reynolds Number Hydrodynamics, Prentice-Hall, Englewood Cliffs, NJ, 1965. 8. Van Dyke, M., An Album of Fluid Motion, Parabolic Press, Stanford, Calif., 1982. 9. Thompson, P. A., Compressible-Fluid Dynamics, McGraw-Hill, New York, 1972. 10. Zucrow, M. J., and Hoffman, J. D., Gas Dynamics, Vol. I, Wiley, New York, 1976. 11. Clayton, B. R., and Bishop, R. E. D., Mechanics of Marine Vehicles, Gulf Publishing Co., Houston, 1982. 12. CRC Handbook of Tables for Applied Engineering Science, 2nd Ed., CRC Press, Boca Raton, Florida, 1973. 13. Shevell, R. S., Fundamentals of Flight, 2nd Ed., Prentice-Hall, Englewood Cliffs, NJ, 1989. 14. Kuethe, A. M., and Chow, C. Y., Foundations of Aerodynamics, Bases of Aerodynamics Design, 4th Ed., Wiley, New York, 1986.
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References 523<br />
determine the lift and drag on an object from the given pressure and shear stress distributions<br />
on the object.<br />
for flow past a flat plate, calculate the boundary layer thickness, the wall shear stress, the<br />
friction drag, and determine whether the flow is laminar or turbulent.<br />
explain the concept of the pressure gradient and its relationship to boundary layer separation.<br />
for a given object, obtain the drag coefficient from appropriate tables, figures, or equations<br />
and calculate the drag on the object.<br />
explain why golf balls have dimples.<br />
for a given object, obtain the lift coefficient from appropriate figures and calculate the lift<br />
on the object.<br />
Some of the important equations in this chapter are:<br />
Lift coefficient and drag coefficient C C D <br />
d<br />
L <br />
l<br />
(9.39), (9.36)<br />
1<br />
1<br />
2rU 2 A , 2rU 2 A<br />
<br />
Boundary layer displacement thickness d* a1 u (9.3)<br />
U b dy<br />
<br />
Boundary layer momentum thickness u<br />
<br />
(9.4)<br />
U a1 u U b dy<br />
Blasius boundary layer<br />
thickness, displacement<br />
thickness, and momentum<br />
thickness for flat plate<br />
d d * <br />
, , (9.15), (9.16), (9.17)<br />
x 0.664<br />
x 1.721<br />
x 5<br />
1Re x 1Re x 1Re x<br />
rm<br />
Blasius wall shear stress for flat plate t w 0.332U 3 2<br />
(9.18)<br />
B x<br />
Drag on flat plate d rbU 2 <br />
(9.23)<br />
Blasius wall friction coefficient<br />
and friction drag coefficient c , C (9.32)<br />
Df 1.328<br />
f 0.664<br />
for flat plate<br />
1Re x 1Re /<br />
0<br />
0<br />
References<br />
1. Schlichting, H., Boundary Layer Theory, 8th Ed., McGraw-Hill, New York, 2000.<br />
2. Rosenhead, L., Laminar Boundary Layers, Oxford University Press, London, 1963.<br />
3. White, F. M., Viscous Fluid Flow, 3rd Ed., McGraw-Hill, New York, 2005.<br />
4. Currie, I. G., Fundamental Mechanics of Fluids, McGraw-Hill, New York, 1974.<br />
5. Blevins, R. D., Applied Fluid Dynamics Handbook, Van Nostrand Reinhold, New York, 1984.<br />
6. Hoerner, S. F., Fluid-Dynamic Drag, published by the author, Library of Congress No. 64,19666,<br />
1965.<br />
7. Happel, J., Low Reynolds Number Hydrodynamics, Prentice-Hall, Englewood Cliffs, NJ, 1965.<br />
8. Van Dyke, M., An Album of Fluid Motion, Parabolic Press, Stanford, Calif., 1982.<br />
9. Thompson, P. A., Compressible-Fluid Dynamics, McGraw-Hill, New York, 1972.<br />
10. Zucrow, M. J., and Hoffman, J. D., Gas Dynamics, Vol. I, Wiley, New York, 1976.<br />
11. Clayton, B. R., and Bishop, R. E. D., Mechanics of Marine Vehicles, Gulf Publishing Co., Houston,<br />
1982.<br />
12. CRC Handbook of Tables for Applied Engineering Science, 2nd Ed., CRC Press, Boca Raton, Florida,<br />
1973.<br />
13. Shevell, R. S., Fundamentals of Flight, 2nd Ed., Prentice-Hall, Englewood Cliffs, NJ, 1989.<br />
14. Kuethe, A. M., and Chow, C. Y., Foundations of Aerodynamics, Bases of Aerodynamics Design, 4th<br />
Ed., Wiley, New York, 1986.