MEC 465
3 credits
Fundamentals of propulsion; performance parameters, thermodynamic cycles. Introduction to combustion and combustors. Performance and cycle analysis of various flight propulsion systems: turbojets, turbofans, turboprops, ramjets, scramjets, rockets and propellors. Design of supersonic inlet nozzles, component matching and map.
| Section | Days | Time | Room | Instructor |
|---|---|---|---|---|
| LEC 01 | Th | 6:30PM–9:20PM | FREY HALL 328 WESTCAMPUS | Foluso Ladeinde★ 1.6 |