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