首页|Analysis on the turning point of dynamic in-plane compressive strength for a plain weave composite

Analysis on the turning point of dynamic in-plane compressive strength for a plain weave composite

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Experimental investigations on dynamic in-plane compressive behavior of a plain weave composite were performed using the split Hopkinson pressure bar.A quantitative criterion for calculating the constant strain rate of composites was established.Then the upper limit of strain rate,restricted by stress equi-librium and constant loading rate,was rationally estimated and confirmed by tests.Within the achiev-able range of 0.001/s-895/s,it was found that the strength increased first and subsequently decreased as the strain rate increased.This feature was also reflected by the turning point(579/s)of the bilinear model for strength prediction.The transition in failure mechanism,from local opening damage to completely splitting destruction,was mainly responsible for such strain rate effects.And three major failure modes were summarized under microscopic observations:fiber fracture,inter-fiber fracture,and interface delamination.Finally,by introducing a nonlinear damage variable,a simplified ZWT model was devel-oped to characterize the dynamic mechanical response.Excellent agreement was shown between the experimental and simulated results.

Plain weave compositeDynamic strengthQuantitative criterionTurning pointFailure mechanism

Xiaoyu Wang、Zhixing Li、Licheng Guo、Zhenxin Wang、Jiuzhou Zhao

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Department of Astronautic Science and Mechanics,Harbin Institute of Technology,Harbin,150001,China

AECC Commercial Aircraft Engine Co,LTD,Shanghai,201108,China

National Science and Technology Major ProjectNatural Science Foundation of Heilongjiang Province

2017-VII-0011-0106ZD2019AO01

2024

防务技术
中国兵工学会

防务技术

CSTPCD
影响因子:0.358
ISSN:2214-9147
年,卷(期):2024.32(2)
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