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Edgewise compression behavior of honeycomb sandwich structures

  • Beihang University
  • Commercial Aircraft Corporation of China, Ltd.

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

An analytical solution and numerical models are proposed for the buckling and post-buckling behavior of honeycomb sandwich structures under edgewise compression. General buckling and core crushing due to transverse shear are observed in the experiment. Based on these phenomena, the von Kármán plate theory are employed for the analysis for the buckling behavior and the analytical solution for the core under transverse shear are obtained for predicting the failure of the sandwich structures. Comparison between these solutions and the experiments shows that the imperfection of pre-bending deformation significantly affects the ultimate load for the sandwich structures, resulting the failure before the compression reaches the critical load for general buckling. Moreover, parameters such as core geometries, asymmetry face sheets are under discussions for the load carrying capacity of the specimens.

源语言英语
主期刊名2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017
出版商Institute of Electrical and Electronics Engineers Inc.
85-91
页数7
ISBN(电子版)9781538633052
DOI
出版状态已出版 - 14 9月 2017
活动8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017 - Prague, 捷克共和国
期限: 22 7月 201725 7月 2017

出版系列

姓名2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017

会议

会议8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017
国家/地区捷克共和国
Prague
时期22/07/1725/07/17

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