Air flows isentropically through a converging nozzle into a receiver where the absolute pressure is 240 kPa. Air enters the nozzle with negligible velocity, 406 kPa (abs.) of pressure, at a temperature of 95 oC. Determine the mass flow rate through the throat of this nozzle wich area is 0.01 m^2.

Q: b) Air entering a converging-diverging nozzle at 1 MPa and 527 °C with negligible velocity…

A: To = 527 +273 = 800K Po = 1 MPa  Mass flow rate = 2.86 kg/s

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A: Given data,TurbineP1=2 MPa   P1=Inlet pressureT1=830K      T1=Inlet temperatureP2=50 kpa    P2=Exit…

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A: Given:To find:The Mach number at the duct exit.The drop in stagnation pressure.

Q: e end of the pipe. If the number, the mass flow

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A: Given data P0=170 KPaT0=300 KM=0.2

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A: dear student please rate me p  stagnation air pressure = 1.1 bar Inlet stagnation temperature = 310…

Q: Required information NOTE: This is a multi-part question. Once an answer is submitted, you will be…

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