Studies on aeroservoelasticity semi-physical simulation test for missiles

Author:

Wu ZhiGang,Chu LongFei,Yuan RuiZhi,Yang Chao,Tang ChangHong

Publisher

Springer Science and Business Media LLC

Subject

General Engineering,General Materials Science

Reference12 articles.

1. Chen G B, Zou C Q, Yang C. Aeroelastic Design Foundation (in Chinese). Beijing: Beijing University of Aeronautics and Astronautics Press, 2004. 194–197

2. Yang C, Wu Z G. Aeroservoelastic stability of missile (in Chinese). Flight Dynam, 2000, 18: 1–5

3. Wu Z G, Yang C. Aeroelastic problems and methodology of slender missiles (in Chinese). In: The 9th National Aeroelasticity Conference. Chengdu: Chinese Aerody-namics Research Society, 2005. 102–110

4. Kraft E, Chapman G. A critical review of the integration of computations, ground tests, and flight test for the development of hypersonic vehicles. AIAA-93-5101, 1993

5. Miller C G. Hypersonic aerodynamic/aerothermodynamic testing capabilities at Langley research center. AIAA-92-3937, 1992

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