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Experimental study on buckling and progressive damage of pre-delaminated composite laminates under compression

  • Commercial Aircraft Corporation of China, Ltd.

科研成果: 会议稿件 › 论文 › 同行评审

摘要

A series of pre-delaminated composite laminates are designed and tested, in order to study the buckling and progressive damage behavior of pre-delaminated composite laminates under compressive loading. Strain measurement, C-scan and moire methods are used in combination in the experiment. The sub-laminate buckling, stress re-distribution and delamination propagation are all captured, and effect of delamination location, delamination size and multiple delaminations on buckling and post-buckling behavior of the laminates is analyzed in detail.

源语言英语
出版状态已出版 - 2017
活动21st International Conference on Composite Materials, ICCM 2017 - Xi'an, 中国
期限: 20 8月 2017 → 25 8月 2017

会议

会议21st International Conference on Composite Materials, ICCM 2017
国家/地区中国
市Xi'an
时期20/08/17 → 25/08/17

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