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A uniform supersonic stream with Mach = 3, P = 1 bar, and T = 300 K, passes a corner (as shown in Fig.

  

A uniform supersonic stream with Mach = 3, P = 1 bar, and T = 300 K, passes a corner (as shown in Fig. 1 which deflect the stream by an angle of 0-30. Calculate the weak and strong oblique shock wave angles and P2, T2, M2, Po2 and To2 behind the most likely occurred shock wave. M-3, P=1 bar. T= 300 K Oblique Shock wave K

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