ME EN5830

Introductions to compressible flow and combustion. Analysis of airbreathing propulsion systems including turbojets, turbofans, afterburners, and turboprops and analysis of chemical rocket propulsion systems including solid and liquid engines. Exploration into design considerations for components including inlets, nozzles, combustion chambers, turbines, and compressors.

Prerequisites: 'C' or better in ME EN 2300 AND ME EN 3710 AND Major Status in Mechanical Engineering AND ME EN 2-5XXX Eligible (See Admission Requirements) AND NOT ME Advising Hold.

Spring