An ideal turbojet ingests 192 lbm/s of air at an altitude of 22,000 ft. It fliesat a Mach number of 0.88, and the compressor pressure ratio is 17. The fuel has a heating value of 17,900 Btu/lbm, and the burner exit total temperature is 2350 °R. Find the developed thrust, dimensionless thrust, and TSFC.
An ideal turbojet ingests 192 lbm/s of air at an altitude of 22,000 ft. It fliesat a Mach number of 0.88, and the compressor pressure ratio is 17. The fuel has a heating value of 17,900 Btu/lbm, and the burner exit total temperature is 2350 °R. Find the developed thrust, dimensionless thrust, and TSFC.
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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Transcribed Image Text:An ideal turbojet ingests 192 lbm/s of air at an altitude of 22,000 ft. It fliesat a Mach number of 0.88, and the compressor
pressure ratio is 17. The fuel has a heating value of 17,900 Btu/lbm, and the burner exit total temperature is 2350 -R. Find
the developed thrust, dimensionless thrust, and TSFC.
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