The Control-Oriented Aerodynamic Design and Analysis for Hypersonic Waverider
- Paper number
IAC-14,C2,P,47,x25551
- Author
Dr. Yi Li, China Academy of Launch Vehicle Technology(CALT), China
- Coauthor
Mr. Jianhui Wu, China Academy of Launch Vehicle Technology(CALT), China
- Coauthor
Mr. Yu Cai, China Academy of Launch Vehicle Technology(CALT), China
- Year
2014
- Abstract
The waverider is a kind of aerodynamic shape for hypersonic vehicle. As a result of high lift-drag-ration and maneuvering capacity, hypersonic vehicle has the haracteristics of strong coupling, nonlinear and large envelope flight. Waverider configuration can be optimized with flight states by using aerodynamic performance analysis. The numerical results show that this configuration with static stability has a satisfying value of lift-drag-ratio.
- Abstract document
- Manuscript document
IAC-14,C2,P,47,x25551.pdf (🔒 authorized access only).
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