What is the stagnation pressure and mach number of flow

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Reference no: EM13620124

You are designing a converging-diverging nozzle to operate at sea level. The nozzle will be mounted on a glider that flies at 60 mph. The entrance to the nozzle is 1 m^2. What is the stagnation pressure and Mach number of flow entering nozzle? What should throat and exit area be if exit mach number is 2?

Reference no: EM13620124

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