Question: Airflow at Ma1 = 3.2 passes through a 25° oblique-shock deflection. What isentropic expansion turn is required to bring the flow back to (a) Ma1

Airflow at Ma1 = 3.2 passes through a 25° oblique-shock deflection. What isentropic expansion turn is required to bring the flow back to
(a) Ma1 and
(b) p1?

Airflow at Ma1 = 3.2 passes through a 25

Fan . Ma 3.2 0 (3) 25

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