Fundamentals of compressible fluid flow in nozzles and diffusers, friction and heat interaction. Fanno, Rayleigh line, and isothermal flow, combustion waves (deflagration, explosion, and detonation waves), normal and oblique shock waves, Extended diffusers and supersonic airfoils. Applications to flow through pipelines, Subsonic, sonic, and supersonic flights, turbo machinery and combustion.

Pre-requisites: AE221 Or AE220 Or AE222