In the last two chapters, basic concepts and theory behind the design and operation of turbojet and turbofan engines were discussed. In this chapter, the thermodynamic operation of these engines is discussed. Expressions for the thrust developed as well as the thrust specific fuel consumption are derived. A procedure for calculating these quantities for a given set of operating conditions is also outlined.
Thrust Calculations
Fundamentals of Propulsion ; Kapitel : 7 ; 95-133
26.08.2021
39 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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