Consider the supersonic flow of air at upstream conditions of 70 kPa and 260 K and a Mach number of 2 4 over a two dimensional wedge of half angle 10 deg If the axis of the wedge is tilted 25 deg with respect to the upstream airflow, determine the downstream Mach number, pressure, and temperature above the wedge Ma Ma, 2 4 10

Question: Consider the supersonic flow of air at upstream conditions of 70 kPa and 260 K and a Mach number of 2.4 over a two-dimensional wedge

Consider the supersonic flow of air at upstream conditions of 70 kPa and 260 K and a Mach number of 2.4 over a two-dimensional wedge of half-angle 10°. If the axis of the wedge is tilted 25° with respect to the upstream airflow, determine the downstream Mach number, pressure, and temperature above the wedge.

Consider the supersonic flow of air at upstream

Ma Ma, 2.4 10

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