Hypersonic Aeroelastic Response of Elastic Boundary Panel Based on a Modified Fourier Series Method
2019 ◽
Vol 2019
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pp. 1-13
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Keyword(s):
In this paper, an analytical method is proposed to directly obtain the aeroelastic time domain response of the elastic boundary panel. Based on a modified Fourier series method (MFSM), the vibration analysis of elastic boundary panels is carried out, after the dynamics equation of the panel is obtained. Then, the vibrational functions are combined with the supersonic piston theory to establish the aeroelastic equation. The aeroelastic time domain response of the panel is obtained to analyze the flutter speed of the panel more intuitively. Finally, the flutter speeds of panels with different length-width ratios, thicknesses, and elastic boundary conditions are discussed in detail.
2019 ◽
Vol 19
(12)
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pp. 1950150
2011 ◽
Vol 66-68
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pp. 1325-1329
2016 ◽
Vol 64
(6)
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pp. 766-778
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1988 ◽
Vol 1
(4)
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pp. 385-389
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Keyword(s):
1983 ◽
Vol 16
(12)
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pp. 2217-2223
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2005 ◽
Vol 46
(3)
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pp. 263-268
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1996 ◽
Vol 99
(4)
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pp. 299-303
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Keyword(s):
2006 ◽
Vol 54
(2)
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pp. 564-571
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