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Mechanics of Fluids

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360 Boundary layers, wakes and other shear layers<br />

be 2U sin θ , where U denotes the velocity far upstream and<br />

θ the angle between the radius and the initial flow direction.<br />

Neglecting changes <strong>of</strong> elevation and assuming that the pressure<br />

in the wake is sensibly uniform and that there are no discontinuities<br />

<strong>of</strong> pressure anywhere, estimate the position at which<br />

the boundary layer separates if the measured drag coefficient is<br />

1.24. Why will this estimate be somewhat in error?<br />

8.10 If, for the cylinder and air flow mentioned in Problem 8.9,<br />

the boundary layer is entirely laminar, use Thwaites’s method<br />

(with λ =−0.09 at separation) to show that the position <strong>of</strong><br />

separation is at θ ≏ 103.1 ◦ .<br />

8.11 Air <strong>of</strong> kinematic viscosity 15 mm 2 · s −1 and density<br />

1.21 kg · m −3 flows past a smooth 150 mm diameter sphere at<br />

60 m · s −1 . Determine the drag force. What would be the drag<br />

force on a 150 mm diameter circular disc held perpendicular<br />

to this air stream?<br />

8.12 Calculate the diameter <strong>of</strong> a parachute (in the form <strong>of</strong> a<br />

hemispherical shell) to be used for dropping a small object<br />

<strong>of</strong> mass 90 kg so that it touches the earth at a velocity no<br />

greater than 6 m · s −1 . The drag coefficient for a hemispherical<br />

shell with its concave side upstream is approximately 1.32 for<br />

Re > 10 3 . (Air density = 1.22 kg · m −3 .)<br />

8.13 Determine the diameter <strong>of</strong> a sphere <strong>of</strong> density 2800 kg · m −3<br />

which would just be lifted by an air-stream flowing vertically<br />

upward at 10 m · s −1 . What would be the terminal velocity<br />

<strong>of</strong> this sphere falling through an infinite expanse <strong>of</strong> water?<br />

(Densities: air 1.21 kg · m −3 ; water 1000 kg · m −3 . Dynamic<br />

viscosities: air 18.0 µPa · s; water 1.0 mPa · s.)<br />

8.14 When water (kinematic viscosity 1.2 mm 2 · s −1 ) flows steadily<br />

at the rate <strong>of</strong> 18.5 L · s −1 through 25 m <strong>of</strong> a 100 mm diameter<br />

pipe, the head loss is 1.89 m. Estimate the relative roughness,<br />

the velocity on the axis <strong>of</strong> the pipe and the shear stress at<br />

the wall.<br />

8.15 Gas is pumped through a smooth pipe, 250 mm in diameter,<br />

with a pressure drop <strong>of</strong> 50 mm H2O per kilometre <strong>of</strong> pipe.<br />

The gas density is 0.7 kg · m −3 and the kinematic viscosity is<br />

18 mm 2 · s −1 . Use eqn 8.52 to determine the rate <strong>of</strong> flow and<br />

the shear stress at the wall <strong>of</strong> the pipe.

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