A uniform supersonic stream with (M_{1}=3.0, p_{1}=1 mathrm{~atm}), and (T_{1}=288 mathrm{~K}) encounters a compression corner (see Fig.

Question:

A uniform supersonic stream with $M_{1}=3.0, p_{1}=1 \mathrm{~atm}$, and $T_{1}=288 \mathrm{~K}$ encounters a compression corner (see Fig. 4.4a) which deflects the stream by an angle $\theta=20^{\circ}$. Calculate the shock wave angle, and $p_{2}, T_{2}, M_{2}, p_{o_{2}}$, and $T_{o_{2}}$ behind the shock wave.

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