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ABSTRACT

Geometrically Non-linear Analysis of Composite Laminated Plates Subjected to Low-Velocity Impact

Xiuqin Zhang1, Simon Wang2*, Yingshun Zhang3

The International Conference on Computational & Experimental Engineering and Sciences 2011, 17(4), 121-122. https://doi.org/10.3970/icces.2011.017.121

Abstract

A B-spline finite strip model is developed in the context of a layer-wise plate theory for analysing the geometrically non-linear transient response of laminated composite plates subjected to transverse low-velocity impact. To simplify the complicated contact analysis, a Hertz-type contact law has been incorporated into the finite strip (FS) model for accounting for the contact behaviour. The model includes the geometrical non-linearity through use of von Karman's non-linear strain-displacement relationship. The resulting non-linear dynamic problem is solved using the Newmark time-stepping scheme together with Newton-Raphson iteration. Several numerical applications are described and a close comparison is found between the results calculated through the present model and the existing analytical and experimental results.

Cite This Article

Zhang, X., Wang, S., Zhang, Y. (2011). Geometrically Non-linear Analysis of Composite Laminated Plates Subjected to Low-Velocity Impact. The International Conference on Computational & Experimental Engineering and Sciences, 17(4), 121–122. https://doi.org/10.3970/icces.2011.017.121



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