Thermodynamics (Jet-Propulsion Cycle) Round up the answer up to 5 decimal places.  A turbojet aircraft moving with a velocity of 790 ft/s at a runway where the pressure & temperature is found to be 14.7psi & 546R. The axial flow compressor provides a pressure ratio of 14 to 1. Temperature at the turbine inlet is 2000R. The mass flowrate of air inside the engine is 133 lbm/s. Determine the following: a. T-S diagram b. Pressure & temperature at each state c. Thrust force (lbf)

Elements Of Electromagnetics
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Thermodynamics (Jet-Propulsion Cycle)

Round up the answer up to 5 decimal places. 

A turbojet aircraft moving with a velocity of 790 ft/s at a runway where the pressure & temperature is found to be 14.7psi & 546R. The axial flow compressor provides a pressure ratio of 14 to 1. Temperature at the turbine inlet is 2000R. The mass flowrate of air inside the engine is 133 lbm/s. Determine the following:

a. T-S diagram

b. Pressure & temperature at each state

c. Thrust force (lbf)

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