Question: A supersonic air flow over the wedge shown in Fig. 3 with upstream conditions of 7 0 kPa and 2 6 0 K and a

A supersonic air flow over the wedge shown in Fig. 3 with upstream conditions of 70 kPa and 260 K and a Mach number of 3. The axis of the wedge is tilted 15\deg with respect to the horizontal upstream air flow, determine the downstream Mach number, pressure, and temperature above (M_{2},P_{2}) and T) the wedge and under GM_{3},P_{3} and T3).

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