Question: Problem 3 : Air, with P 0 , 1 = 1 . 0 MPa and T 0 , 1 = 1 2 5 C ,
Problem : Air, with MPa and flows steadily and adiabatically from a large tank through a converging nozzle connected to an insulated constantarea duct. The nozzle may be considered frictionless. The pressure at the nozzle exit ie duct inlet is kPa
Calculate the pressure at the end of the duct, where the static temperature is and the entropy change of the air Confirm that the flow is not choked and calculate the percent reduction in pressure required for
Sketch a Fanno line on the diagram for the process and label all states.
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