Nonlinear Vibrations of FGM Cylindrical Panel with Simply Supported Edges in Air Flow

Chaotic and periodic motions of an FGM cylindrical panel in hypersonic flow are investigated. The cylindrical panel is also subjected to in-plane external loads and a linear temperature variation in the thickness direction. The temperature dependent material properties of panel which are assumed to...

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Bibliographic Details
Main Authors: Y. X. Hao, W. Zhang, S. B. Li, J. H. Zhang
Format: Article
Language:English
Published: Wiley 2015-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2015/246352
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