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: 4
Average GPA: 3.46 (rounds to B+)
Strict A Rate (No A-) : 38.86%
Average Withdrawal Rate: 3.13%
| Gregory Young | 2024 | 46.2% | 48.3% | 2.5% | 0.0% | 0.0% | 3.1% | 3.46 | 4 |