Aircraft Propulsion System (SKMA 3423)

An introduction to aircraft propulsion system including its historical background.  Review of thermodynamics and fluid mechanics; Fundamental of gas dynamics; Piston engines; Shaft and thrust power; Cycle analysis: air standard and cycle with friction; Turbojet engine cycle; Turbofan engine cycle; Gas turbine engine components and their functions; Compressor and Turbine velocity diagram analysis; Turbine blades cooling techniques; Gas turbine emissions; Chemical rocket engines. It is a blended course that combines traditional teaching methods to Problem-Based Learning (PBL) approach based on real problems of aircraft propulsion system.

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