CFD/CSD Approach to Predict Hypersonic Aerothermoelastic Response of a Wing

Author:

Lv Jinan,Wang Fangjian,Guo Li,Liu Ziqiang

Publisher

Elsevier BV

Subject

Applied Mathematics

Reference13 articles.

1. Peebles C. The X-43A flight research program: lessons learned on the road to Mach 10[M]. Washington, D.C. :AIAA Inc., 2007.

2. YANG Bing-yuan SHI Xiao-ming LIANG Qiang. Investigation and development of the multi-physics coupling dynamics on the hypersonic winged missiles[J]. STRUCTURE & ENVIRONMENT ENGINEERING, 2008, 35(5).

3. Yang Chao, Xu Yun, Xie Changchuan. Review of studies on aeroelasticity of hypersonic vehicles. ACTA AERONAUTICA ET ASTRONAUTICA SINICA, 2010, 31(1).

4. Thuruthinattam B J, Friedmann P P, Powell K G, et al, Aeroelasticity of a generic hypersonic vehicle[J]. AIAA-2002-1209.

5. Anderson, J.D., Aerothermodynamics: A Tutorial Discussion in Thermal Structures and Materials for High-speed Flight, AIAA, 1992, Ch. 1, pp. 3-57.

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