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.
High Speed Propulsion
Host University
Virginia Tech
Semester
Fall 2026
Course Number
AOE-5184
CRN
92118
Credits
3
Discipline
Aerospace and Ocean Engineering
Course Information
Prerequisites
None Prerequisites Enforced: Yes