A symmetrical wedge having a total vertex angle of 60 degrees is traveling at a Mach...

A symmetrical wedge having a total vertex angle of 60 degrees is traveling at a Mach number of 3 at an altitude of 15 km. What are the static values of the pressure, density, and temperature downstream of the shock, and what are the stagnation values of those quantities? What is the percentage loss of the stagnation pressure across the shock wave?

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samet mamat answered 2 years ago

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