Air at (V_{1}=800 mathrm{~m} / mathrm{s}, p_{1}=100 mathrm{kPa}), and (T_{1}=300 mathrm{~K}) passes through a normal shock. Calculate

Question:

Air at $V_{1}=800 \mathrm{~m} / \mathrm{s}, p_{1}=100 \mathrm{kPa}$, and $T_{1}=300 \mathrm{~K}$ passes through a normal shock. Calculate the velocity $V_{2}$, temperature $T_{2}$, and pressure $p_{2}$ after the shock. What would be the values of $T_{2}$ and $p_{2}$ if the same velocity change were accomplished isentropically?

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