calculate the gas temperature at the exit

What type of organizations should CMC use as benchmarks?
July 30, 2019
Identify the data that should be incorporated into CGC’s new system to provide adequate planning capability. Explain why each data item it is important and the level of detail needed for the data to be useful.
July 30, 2019

Consider a turbojet in an airplane flying at standard sea level with a velocity of 800 . The pressure ratio across the compress 01 r is 12.5:1. The fuel-to-air ratio (by mass) is 0.05. If the nozzle exhausts the flow to ambient pressure, calculate the gas temperature at the exit (In solving this problem, assume that the air in the diffuser is slowed to a very low velocity before entering the compressor. Also assume that the heat released per pound of fuel is 1.4 x 107 · .,.)


 

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