Question: A supersonic flow at M 1 = 1.58 and P 1 = 1 atm expands around a sharp corner. If the pressure downstream of the

A supersonic flow at M₁ = 1.58 and P₁= 1 atm expands around a sharp corner. If the pressure downstream of the corner is 0.1306 atm, calculate the deflection angle of the corner.

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