Consider an oblique shock wave with a wave angle of 30 in a Mach 4 flow. The
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Consider an oblique shock wave with a wave angle of 30° in a Mach 4 flow. The upstream pressure and temperature are 2.65 x 104 N/m2 and 223.3 K, respectively (corresponding to a standard altitude of 10,000m). Calculate the pressure, temperature, Mach number, total pressure, and total temperature behind the wave and the entropy increase across the wave.
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M M sinB 40 sin 30 2 P2 From Table A2 for M 2 45 n P1 P2 T 11 25 T P P01 45 265 ...View the full answer
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