Engineering, 17.04.2020 18:17 Izayoi
An ideal turbojet ingests 192 lbm/s of air at an altitude of 22000ft it flies at a mach number of 0.88 and the compressure pressure ratio is 17 the fuel has a heating value of 17900 and the burner exit total temperature is 2350 find the developed thrust dimensionless thrust and TSFC..
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An ideal turbojet ingests 192 lbm/s of air at an altitude of 22000ft it flies at a mach number of 0....
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