Just upstream of a normal shock in an airflow, Ma 3.0, T
Chapter 11, Problem 11.65(choose chapter or problem)
Just upstream of a normal shock in an airflow, Ma = 3.0, \(T = 600 \mathrm{ ~^\circ R}\), and p = 30 psia. Estimate values of Ma, \(T_0, ~T, ~p_0, ~p\), and V downstream of the shock.
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