End effect and near-surface buckling in a laminate composite material compres sed by a surface load.

Authors

  • V.M. Bystrov S.P. Timoshenko Institute of Mechanics of the NAS of Ukraine, Kyiv

DOI:

https://doi.org/10.15407/dopovidi2019.10.029

Keywords:

crumpling of ends, end effect, layered composite material, longitudinal compression, mode of stability loss, multilayer representative element, near-surface buckling, surface load, three-dimensional linearized theory of stability

Abstract

Using the basic relations of the three-dimensional linearized theory of stability in the framework of the piecewise- homogeneous medium model, the problem of stability of a layered composite material under compression of reinforcing layers by a surface load is solved. The case of a non-uniform subcritical state associated with an end effect in the region of application of the load is considered. A computational model is used for the boundary conditions on the lateral sides of a multilayer sample made of a composite material, which correspond to the symmetry conditions. The influence of the end effect on the attenuation of forms of a near-surface instability at diffe rent statically equivalent loads of reinforcing layers of a composite material is studied. For the numerical solution of the problem, the grid method based on the modified variation-difference approach is applied.

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References

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Published

24.04.2024

How to Cite

Bystrov, V. (2024). End effect and near-surface buckling in a laminate composite material compres sed by a surface load . Reports of the National Academy of Sciences of Ukraine, (10), 29–37. https://doi.org/10.15407/dopovidi2019.10.029