Air at a stagnation pressure of 450 kpa and stagnation temp

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Reference no: EM13621741

Air at a stagnation pressure of 450 Kpa and stagnation temp of 400K flows through a converging nozzle whose throat area is 12 cm^2. Normal shock stands where area is 20cm^2. Compute mach number,pressure,temp- before and after shock.

Reference no: EM13621741

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