Proceedings of the 2015 International Conference on Advances in Mechanical Engineering and Industrial Informatics 2015
DOI: 10.2991/ameii-15.2015.329
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Response Analysis of thin-walled Structure under Non-uniform temperature field and Acoustic Loads

Abstract: Abstract. With the raised performance of advanced aircraft, hypersonic vehicles are subjected to increasingly severe environment. Very severe elevated temperature and high intensity acoustic loads will cause the thin-walled structures of aircraft to respond in a strong nonlinear large deflection vibration, and leading to premature fatigue failure of the structure. According to the Von Karman large deflection theory, the large deflection governing equation of plate under thermo-acoustic loadings is obtained. Th… Show more

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