Airflow at Ma1 = 3.2 passes through a 25° oblique-shock deflection. What isentropic expansion turn is required

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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
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Physics

ISBN: 978-0321976444

5th edition

Authors: James S. Walker

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