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Basics of Fluid Mechanics, 2014a

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534 CHAPTER 12. COMPRESSIBLE FLOW 2–DIMENSIONAL<br />

Angle, μ<br />

100<br />

90<br />

80<br />

70<br />

60<br />

50<br />

Prandtl-Meyer Function<br />

40<br />

1.1<br />

30<br />

1.2<br />

= k<br />

20<br />

1.3<br />

10<br />

1.4<br />

1.67<br />

0<br />

10 0 2 5 10 1 2 5 10 2<br />

M<br />

Fig. -12.26. The angle as a function <strong>of</strong> the Mach number and spesfic heat.<br />

A ∗ A exit β<br />

β<br />

M jet1<br />

P surroundings<br />

Slip lines<br />

expenssion<br />

lines<br />

Fig. -12.31. Schematic <strong>of</strong> the nozzle and Prandtl–Meyer expansion.

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