Air enters a convergingdiverging nozzle of a supersonic
Chapter 17, Problem 1765E(choose chapter or problem)
Air enters a convergingdiverging nozzle of a supersonic wind tunnel at 150 psia and 1008F with a low velocity. The flow area of the test section is equal to the exit area of the nozzle, which is 5 ft2 . Calculate the pressure, temperature, velocity, and mass flow rate in the test section for a Mach number Ma 5 2. Explain why the air must be very dry for this application.
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