AOE-5184: High Speed Propulsion
Description: Analysis of high-speed air breathing propulsion concepts for hypersonic flight. Aerodynamic inlet design and flow path integration. Cycle analyses, flight performance, and design limitations given a set of design requirements. Aerothermodynamic analysis of ramjets, scramjets, and detonation wave engines. Pre: Graduate standing.
Pathways: N/A
Course Hours: 3 credits
Sections Taught: 2
Average GPA: 3.52 (A-)
Strict A Rate (No A-) : 45.20%
Average Withdrawal Rate: 0.00%
| Gregory Young | 2023 | 53.6% | 44.0% | 2.4% | 0.0% | 0.0% | 0.0% | 3.52 | 2 |