Engineering, 25.11.2019 22:31 dontcareanyonemo

Aconvergent-divergent nozzle is designed to expand air from a chamber in which the pressure is 700 kpa and the temperature is 35°c to give mach 1.6. the mass flow rate through the nozzle under design conditions is 0.012 kg/s. find
a. the throat and exit areas of the nozzle
b. the design back-pressure and the temperature of the air leaving the nozzle with this back-pressure nozzle
c. the lowest back-pressure for which there will be no supersonic flow in the
d. the back-pressure below which there are no shock waves in the nozzle

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Aconvergent-divergent nozzle is designed to expand air from a chamber in which the pressure is 700 k...