2. [10 points] A supersonic wind tunnel is to be designed to test objects flying at M-2 and pressure and temperature cor

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2 10 Points A Supersonic Wind Tunnel Is To Be Designed To Test Objects Flying At M 2 And Pressure And Temperature Cor 1 (21.45 KiB) Viewed 11 times

2. [10 points] A supersonic wind tunnel is to be designed to test objects flying at M-2 and pressure and temperature corresponding to standard sea level conditions (P=latm and T-288K). The mass flow rate of air in the test section is to be 16 kg/s. Calculate: Nozzle Test section a) The necessary reservoir pressure? b) The necessary reservoir temperature? c) The wind tunnel test section area? d) The nozzle exit area? e) The nozzle throat area? Po M-2 T-288K P-latm 2