ideal turbojet with an afterburner flies at 22,000 ft with a Mach numher of 0.88

ideal turbojet with an afterburner flies at 22,000 ft with a Mach numher

of 0.88. It ingests 192 lbm/s of air, and the compressor pressure ratio 

The fuel has a heating value of 17,900 Btu/Ibm. The primary burner »nd

afterburner exit total temperatures are 2350 and 2980 OR, respectively. (a)

Find the developed thrust, dimensionless thrust, and TSFC. (b) Compare

these parameters with those of the nonafterburning case.

manual solution Fundamentals of Jet Propulsion with Applications by Flack. R.D

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  Have a nice day Eng.Yazan Jarrah