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[Solved]: Just need help with C and D Consider the sup
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(Solved): Just need help with C and D Consider the supersonic flow of air at M1=2.0 and at a static p ...


Consider the supersonic flow of air at \( M_{1}=2.0 \) and at a static pressure of \( 75.0 \mathrm{KPa} \) with a static temp

Just need help with C and D

Consider the supersonic flow of air at and at a static pressure of with a static temperature of . a) Calculate the stagnation temperature of the flow. b) Calculate the stagnation pressure of the flow. c) If the flow passes through a nozzle with area what will be the mass flow rate d) If the flow undergoes a normal shock, what will be the change in entropy across the shock?


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