Analysis of laminated composite and sandwich plate structures using generalized layerwise HSDT and improved meshfree radial point interpolation method

This paper presents a generalized layerwise higher-order shear deformation theory for static, free vibration and buckling analyses of symmetric laminated composite and sandwich plates using improved meshfree radial point interpolation method (iRPIM). The approach comes from a layerwise model combine...

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Veröffentlicht in:Aerospace science and technology 2016-11, Vol.58, p.641-660
Hauptverfasser: Phan-Dao, Hoang-Hiep, Thai, Chien H., Lee, Jaehong, Nguyen-Xuan, Hung
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Sprache:eng
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Zusammenfassung:This paper presents a generalized layerwise higher-order shear deformation theory for static, free vibration and buckling analyses of symmetric laminated composite and sandwich plates using improved meshfree radial point interpolation method (iRPIM). The approach comes from a layerwise model combined with a generalized higher-order shear deformation theory. In other words, we impose the continuity on the interface of each layer for the in-plane displacements and transverse shear stresses. This yields more adequate solution for sandwich structures which present the significant difference of properties between the core sheet and the face ones. As a result, transverse shear stresses are accurately achieved as compared with the analytical ones. The present iRPIM shows stability and high accuracy with respect to the uniquely proposed correlation function. A simple but effective enforcement based on the concept of the rotation-free of essential boundary conditions yields significant advantage of computations. The numerical results are provided and compared well with other published solutions.
ISSN:1270-9638
1626-3219
DOI:10.1016/j.ast.2016.09.017