Course Detail
Units:
3.0
Course Components:
Lecture
Enrollment Information
Enrollment Requirement:
Prerequisites: 'C' or better in (ME EN 2300 OR ME EN 3600 OR ME EN 3610) AND (ME EN 3700 OR ME EN 3710) AND Full Major status in Mechanical Engineering
Description
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.