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Posted: **Mon May 02, 2022 3:49 pm**

: 2 1 5 Pts A Uniform Supersonic Stream With M1 5 0 P1 1 Atm And T 288 K Encounters A Compression Corner Which 1 (13.78 KiB) Viewed 30 times

: 2 1 5 Pts A Uniform Supersonic Stream With M1 5 0 P1 1 Atm And T 288 K Encounters A Compression Corner Which 2 (13.78 KiB) Viewed 30 times

2. (1.5 pts) A uniform supersonic stream with M1 = 5.0, P1 = 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, P.2, and T.2. behind the shock wave.