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A supersonic airflow at Ma1 = 3.2 and p1 = 50 kPa undergoesa compression shock followed by an isentropic expansionturn. The flow deflection is 30° for each turn. ComputeMa2 and p2 if (a) the shock is followed by the expansionand (b) the expansion is followed by the shock.

A supersonic airflow at Ma1 = 3.2 and p1 = 50 kPa undergoesa compression shock followed by an isentropic expansionturn. The flow deflection is 30° for each turn. ComputeMa2 and p2 if (a) the shock is followed by the expansionand (b) the expansion is followed by the shock.

Elements Of Electromagnetics
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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A supersonic airflow at Ma1 = 3.2 and p1 = 50 kPa undergoes
a compression shock followed by an isentropic expansion
turn. The flow deflection is 30° for each turn. Compute
Ma2 and p2 if (a) the shock is followed by the expansion
and (b) the expansion is followed by the shock.

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