Buckling Analysis of Composite Laminate Plates Based on the n-order Shear Deformation Theory

SHI Feng; MA Hongying; SUN Yizhen; XIANG Song; WANG Yanbing; LUAN Tingting

doi:10.21656/1000-0887.410061

Volume 41 Issue 12

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Article Navigation > Applied Mathematics and Mechanics > 2020 > 41(12): 1346-1357

SHI Feng, MA Hongying, SUN Yizhen, XIANG Song, WANG Yanbing, LUAN Tingting. Buckling Analysis of Composite Laminate Plates Based on the n-order Shear Deformation Theory[J]. Applied Mathematics and Mechanics, 2020, 41(12): 1346-1357. doi: 10.21656/1000-0887.410061

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Buckling Analysis of Composite Laminate Plates Based on the n-order Shear Deformation Theory

doi: 10.21656/1000-0887.410061

¹Research and Development Center of Digital Resources, Shenyang Open University,Shenyang 110003, P.R.China;²Liaoning Key Laboratory of General Aviation, Shenyang Aerospace University,Shenyang 110136, P.R.China

Received Date: 2020-02-24
Rev Recd Date: 2020-04-16
Publish Date: 2020-12-01

Abstract

Abstract

The buckling of composite laminate plates was analyzed with the nth-order shear deformation theory. The virtual work principle was used to derive the governing equations for the critical buckling of laminate pates under in-plane loads. The comparison between the present results and the results of previous literatures shows good agreement and high calculation accuracy.
- composite laminate plate,
- buckling,
- analytical method,
- in-plane load,
- nth-order shear deformation theory

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References(15)

References

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