Question: 1 - Given the following parameters for a turbojet engine ( inlet pressure = 1 0 0 kPa, compressor pressure ratio = 1 0 ,

1- Given the following parameters for a turbojet engine (inlet pressure =100 kPa, compressor pressure ratio =10, turbine inlet temperature =1600 K, ambient temperature =300 K), calculate the ideal thermal efficiency of the engine. Assume air behaves as an ideal gas with a specific heat ratio of 1.4.

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