Inlet stagnation air pressure of a two-dimensional compressor cascade is 1.0 bar and inlet stagnation temperature of 295k. for an inlet mach number of 0.75 and an inlet flow angle of 48°, the exit flow angle is measured as 16.5°. assuming the flow is isentropic, determine the mass flow rate per unit frontal area, the exit mach number and the static pressure ratio across the cascade.

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