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A supersonic air flow over the wedge shown in Fig. 3 with upstream conditions of 70 kPa and 260 K and a Mach number
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 with respect to the horizontal upstream air flow, determine the downstream Mach number, pressure, and temperature above (M2, P2 and T2) the wedge and under (M3, P3 and T3). Adiabatic Fig. 2 Isentropic 11111 M 10 M 10 Fig. 3
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Thermodynamics An Engineering Approach
Authors: Yunus A. Cengel, Michael A. Boles
8th edition
73398179, 978-0073398174
