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Composite honeycomb sandwich columns under in-plane compression: Optimal geometrical design and three-dimensional failure mechanism maps

  • Published:2022-01 Issue: Volume:91 Page:104415
  • ISSN:0997-7538
  • Container-title:European Journal of Mechanics - A/Solids
  • language:en
  • Short-container-title:European Journal of Mechanics - A/Solids

Author:

Wei Xingyu,Wu Qianqian,Gao Ying,Yang Qiang,Xiong Jian

Funder

National Natural Science Foundation of China

Natural Science Foundation of Heilongjiang Province

Publisher

Elsevier BV

Subject

General Physics and Astronomy,Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference44 articles.

1. The effect of loading rate on the compression properties of carbon fibre-reinforced epoxy honeycomb structures;Alia;J. Compos. Mater.,2020

2. Analysis and Design of Structural Sandwich Panels;Allen,1969

3. Failure mode maps for composite sandwich panels subjected to air blast loading;Andrews;Int. J. Impact Eng.,2009

4. Transition from buckling to progressive failure during quasi-static in-plane crushing of CF/EP composite sandwich panels;Chen;Compos. Sci. Technol.,2018

5. The through-thickness compressive strength of a composite sandwich panel with a hierarchical square honeycomb sandwich core;Côté;ASME J. Appl. Mech.,2009

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