- 1 1 5 Pts A Uniform Supersonic Stream With Mi 3 0 P 1 Atm And T1 288 K Encounters A Compression Corner Which 1 (21.59 KiB) Viewed 43 times
1. (1.5 pts) A uniform supersonic stream with Mi = 3.0, P, = 1 atm, and T1 = 288 K encounters a compression corner which
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1. (1.5 pts) A uniform supersonic stream with Mi = 3.0, P, = 1 atm, and T1 = 288 K encounters a compression corner which
1. (1.5 pts) A uniform supersonic stream with Mi = 3.0, P, = 1 atm, and T1 = 288 K encounters a compression corner which deflects the stream by an angle 8 = 30'. Calculate the shock wave angle, and P2, T2, M2, Po2, and T., behind the shock wave. 2. (1.5 pts) A uniform supersonic stream with Mi = 5.0, P= 1 atm, and T= 288 K encounters a compression corner which deflects the stream by an angle 0 = 20'. Calculate the shock wave angle, and P2, T2, M2, Poz, and T., behind the shock wave.
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