Optimization of Hypersonic Airbreathing Propulsion Systems through Mixed Analysis Methods
Accurate flow path modeling of scramjet engines is a key step in the development of an airframe integrated engine for hypersonic vehicles. A scramjet system model architecture is proposed and implemented using three different engine components: the isolator, combustor, and nozzle. For each component...
| Main Author: | |
|---|---|
| Other Authors: | |
| Format: | Others |
| Published: |
Virginia Tech
2019
|
| Subjects: | |
| Online Access: | http://hdl.handle.net/10919/95512 |