Large amplitude free flexural vibrations of laminated composite skew plates

被引:53
|
作者
Singha, MK [1 ]
Ganapathi, M [1 ]
机构
[1] GE Co, Engn Anal Ctr Excellence, Aircraft Engines, Bangalore 560066, Karnataka, India
关键词
composite skew plate; non-linear vibration; finite element; frequency ratio; amplitude;
D O I
10.1016/j.ijnonlinmec.2004.04.003
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Here, the large amplitude free flexural vibration behaviors of thin laminated composite skew plates are investigated using finite element approach. The formalation includes the effects of shear deformation, in-plane and rotary inertia. The geometric non-linearity based on von Karman's assumptions is introduced. The non-linear governing equations obtained employing Lagrange's equations of motion are solved using the direct iteration technique. The variation of non-linear frequency ratios with amplitudes is brought out considering different parameters such as skew angle, number of layers, fiber orientation, boundary condition and aspect ratio. The influence of higher vibration modes on the non-linear dynamic behavior of laminated skew plates is also highlighted. The present study reveals the redistribution of vibrating mode shape at certain amplitude of vibration depending on geometric and lamination parameters of the plate. Also, the degree of hardening behavior increases with the skew angle and its rate of change depends on the level of amplitude of vibration. (C) 2004 Elsevier Ltd. All rights reserved.
引用
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页码:1709 / 1720
页数:12
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