Consider a normal shock wave in air. The upstream conditions are given by (M_{1}=3, p_{1}=1 mathrm{~atm}), and

Question:

Consider a normal shock wave in air. The upstream conditions are given by $M_{1}=3, p_{1}=1 \mathrm{~atm}$, and $ho_{1}=1.23 \mathrm{~kg} / \mathrm{m}^{3}$. Calculate the downstream values of $p_{2}, T_{2}, ho_{2}, M_{2}, u_{2}, p_{o_{2}}$, and $T_{o_{2}}$.

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