Question: A simple turbojet is operating with a compressor pressure ratio of 1 6 . 0 , a turbine inlet temperature of 1 5 0 0
A simple turbojet is operating with a compressor pressure ratio of a turbine inlet
temperature of and a mass flow of when the aircraft is flying at at an
altitude of Assuming the following component efficiencies, and ISA conditions, calculate
the propelling nozzle area required, the net thrust developed and the SFC:
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