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11.3 Categories of Compressible Flow 589<br />

The wave pattern<br />

from a moving<br />

source is not<br />

symmetrical.<br />

number and Mach number is shown for air flow over a sphere. Compressibility effects can be of<br />

considerable importance.<br />

To further illustrate some curious features of compressible flow, a simplified example is considered.<br />

Imagine the emission of weak pressure pulses from a point source. These pressure waves<br />

are spherical and expand radially outward from the point source at the speed of sound, c. If a pressure<br />

wave is emitted at different times, t wave , we can determine where several waves will be at a<br />

common instant of time, t, by using the relationship<br />

r 1t t wave 2c<br />

where r is the radius of the sphere-shaped wave emitted at time t wave . For a stationary point<br />

source, the symmetrical wave pattern shown in Fig. 11.3a is involved.<br />

When the point source moves to the left with a constant velocity, V, the wave pattern is no<br />

longer symmetrical. In Figs. 11.3b, 11.3c, and 11.3d are illustrated the wave patterns at t 3 s for<br />

different values of V. Also shown with a “ ” are the positions of the moving point source at values<br />

of time, t, equal to 0 s, 1 s, 2 s, and 3 s. Knowing where the point source has been at different<br />

instances is important because it indicates to us where the different waves originated.<br />

From the pressure wave patterns of Fig. 11.3, we can draw some useful conclusions. Before<br />

doing this we should recognize that if instead of moving the point source to the left, we held the<br />

point source stationary and moved the <strong>fluid</strong> to the right with velocity V, the resulting pressure wave<br />

patterns would be identical to those indicated in Fig. 11.3.<br />

c<br />

2c<br />

3c<br />

3c<br />

2c<br />

c<br />

V<br />

2V<br />

3V<br />

(a)<br />

(b)<br />

Zone of silence<br />

Zone of action<br />

Tangent plane<br />

(Mach wave)<br />

c<br />

2c<br />

3c<br />

Zone of silence<br />

α<br />

c<br />

2c<br />

3c<br />

2V = 2c<br />

3V = 3c<br />

V = c<br />

Mach cone<br />

Zone of action<br />

(c)<br />

Wave emitted at t = 0 s Wave emitted at t = 1 s Wave emitted at t = 2 s<br />

Source at t = 0 s<br />

3V<br />

(d)<br />

Source at t = 1, 2, or 3 s<br />

F I G U R E 11.3 (a) Pressure waves at t 3 s, V 0; (b) pressure waves at t 3 s,<br />

V 6 c; (c) pressure waves at t 3 s, V c; (d) pressure waves at t 3 s, V 7 c.<br />

2V<br />

V

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