ME-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: 0
Average GPA: N/A
Strict A Rate (No A-) : N/A%
Average Withdrawal Rate: N/A%