Paper information
- Paper code
- Order
3
- Room
Ballroom B (Crowne Plaza Hotel, -1 floor)
- Title
effects of primary rocket nozzle expansion ratio on combustion oscillating characteristics in a rbcc engine combustor
- abstract
- Session
9. Hypersonic and Combined Cycle Propulsion
- symposium
C4. SPACE PROPULSION SYMPOSIUM
- congress
IAC-15
- Type of presentation
oral
Prof. Guoqiang He, Northwestern Polytechnical University, China
Mr. Zhiwei Huang, Northwestern Polytechnical University,NPU, China;
Dr. Fei Qin, China;
Mr. Ya Jun Wang, College of Astronautics, Northwestern Polytechnical University, China;
Mr. Xianggeng Wei, Northwestern Polytechnical University, China;