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The converging-diverging nozzle(as shown in the figure given below) expands and accelerates dry air to supersonic speeds at the exit where p2=8kPa and T2=240K. At

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The converging-diverging nozzle(as shown in the figure given below) expands and accelerates dry air to supersonic speeds at the exit where p2=8kPa and T2=240K. At the throat, p1=284kPa,T1=665K, and V1=590m/s. NOTE: This is a multi-part question. Once an answer is submitted, you will be unable to retum to this part. Determine the mass flow for a steady compressible flow of an ideal gas. Kg/s

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