Engineering, 18.07.2019 00:40 skylastrusz7643

At a point upstream of the throat (the throat area is 35cm2) of a converging-diverging nozzle the properties are vi=200m/s, t=300k, and p1=125kpa. if the exit flow is supersonic, compute for the isentropic case (a) the mass flow rate and (b) a1.

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At a point upstream of the throat (the throat area is 35cm2) of a converging-diverging nozzle the pr...