An ideal turbojet ingests 192 lbm/s of air at an altitude of 22,000 ft. It flies at

An ideal turbojet ingests 192 lbm/s of air at an altitude of 22,000 ft. It flies

at a Mach number of 0.88, and the compressor pressure ratio is 17. The fuel

has a heating value of 17,900 Btu/Ibm, and the burner exit total temperature

is 2350 OR. Find the developed thrust, dimensionless thrust, and TSFC

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Eng.Yazan Jarrah

An ideal turbojet ingests 192 lbm/s of air at an altitude of 22,000 ft. It flies

at a Mach number of 0.88, and the compressor pressure ratio is 17. The fuel

has a heating value of 17,900 Btu/Ibm, and the burner exit total temperature

is 2350 OR. Find the developed thrust, dimensionless thrust, and TSFC