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. with upstream conditions of kPa and K and a Mach number of The axis of the wedge is tilted deg with respect to the horizontal upstream air flow, determine the downstream Mach number, pressure, and temperature above MP and T the wedge and under GMP and T
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