Applied Mathematics and Mechanics (English Edition) ›› 2015, Vol. 36 ›› Issue (5): 633-654.doi: https://doi.org/10.1007/s10483-015-1933-7

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Modeling vibration behavior of delaminated composite laminates using meshfree method in Hamilton system

Jie CHEN1, Hai WANG1, Guanghui QING2   

  1. 1. School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai 200240, China;
    2. College of Aeronautical Engineering, Civil Aviation University of China, Tianjin 300300, China
  • 收稿日期:2014-04-13 修回日期:2014-07-30 出版日期:2015-05-01 发布日期:2015-05-01
  • 通讯作者: Hai WANG E-mail:wanghai601@sjtu.edu.cn

Modeling vibration behavior of delaminated composite laminates using meshfree method in Hamilton system

Jie CHEN1, Hai WANG1, Guanghui QING2   

  1. 1. School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai 200240, China;
    2. College of Aeronautical Engineering, Civil Aviation University of China, Tianjin 300300, China
  • Received:2014-04-13 Revised:2014-07-30 Online:2015-05-01 Published:2015-05-01
  • Contact: Hai WANG E-mail:wanghai601@sjtu.edu.cn

摘要: Free vibration analysis of composite laminates with delaminations is performed based on a three-dimensional semi-analytical model established by introducing the local radial point interpolation method (LRPIM) into a Hamilton system. The governing equation is derived with a transfer matrix technique and a spring layer model based on a local weak-form equivalent to the modified Hellinger-Reissner variational principle. Main superiority of the present model is that the scale of the governing equation involves only the so-called state variables at the top and bottom surfaces, and is insensitive to the thickness and the layer number of the composite laminates. Several numerical examples for analyzing the vibration frequencies and mode shapes of delaminated composite beams and plates are given to validate the model. The results are in good agreement with the pre-existing results.

关键词: vibration, composite laminate, delamination, local radial point interpolation method (LRPIM)

Abstract: Free vibration analysis of composite laminates with delaminations is performed based on a three-dimensional semi-analytical model established by introducing the local radial point interpolation method (LRPIM) into a Hamilton system. The governing equation is derived with a transfer matrix technique and a spring layer model based on a local weak-form equivalent to the modified Hellinger-Reissner variational principle. Main superiority of the present model is that the scale of the governing equation involves only the so-called state variables at the top and bottom surfaces, and is insensitive to the thickness and the layer number of the composite laminates. Several numerical examples for analyzing the vibration frequencies and mode shapes of delaminated composite beams and plates are given to validate the model. The results are in good agreement with the pre-existing results.

Key words: delamination, vibration, composite laminate, local radial point interpolation method (LRPIM)

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