Rbcc engine performance analysis model
- Paper number
IAC-06-C4.P.5.03
- Author
Mr. Lu Xiang, Northwestern Polytechnical University, China
- Coauthor
Prof. Pei-Jing Liu, Northwestern Polytechnical University, China
- Coauthor
Prof. Guoqiang He, Northwestern Polytechnical University, China
- Year
2006
- Abstract
For its excellent performance, Rocket Based Combined Cycle(RBCC)should be the most competitive propulsion system of Hypersonic Vehicle for martial and civil purpose. RBCC engine performance analysis model plays an important role in model design for both Hypersonic Vehicle and RBCC engine. RBCC engine performance analysis model and corresponding software REPAM, RBCC Engine Performance Analysis Module, were both developed in this paper. Taking into account the boundary layer effect on flow structure, a correction formula for forebody analysis model was given, which produces biases less than 2
- Abstract document