Paper information
- Paper code
- Order
16
- Title
Numerical simulation research for the effects of trailing edge structure on the supersonic mixing layer
- abstract
- Session
7. Hypersonic Air-breathing and Combined Cycle Propulsion, and Hypersonic Vehicle
- symposium
C4. IAF SPACE PROPULSION SYMPOSIUM
- congress
IAC-20
- Type of presentation
oral
Prof. Shen Chibing, National University of Defense Technology, China