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Question: supersonic air encounters the wedge shape shown below a calculate...

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Supersonic air encounters the wedge shape shown below.

a) Calculate the wave angle at the onset of face A and the normal free-stream Mach numberĀ 

b) Calculate the Mach numbers, Prandtl-Meyer functions and pressures on faces A, B and C.

Assume inviscid flow and that the air behaves as a perfect gas. Let š›¾ = 1.4.

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