周光明

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教授

招生学科专业:
力学 -- 【招收博士、硕士研究生】 -- 航空学院
航空宇航科学与技术 -- 【招收硕士研究生】 -- 航空学院
机械 -- 【招收博士、硕士研究生】 -- 航空学院

学历:南京航空航天大学

学位:工学博士学位

所在单位:航空学院

办公地点:A18-812

联系方式:13601401937

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Failure analysis of plain woven glass/epoxy laminates: Comparison of off-axis and biaxial tension loadings

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所属单位:航空学院

发表刊物:POLYMER TESTING

关键字:Plain woven composite Off-axis and biaxial tests Tensile strength Failure criteria Fracture modes

摘要:An experimental study was focused on investigation of the failure properties of plain woven glass/epoxy composites under off-axis and biaxial tension loading conditions. Four fibre orientations (0 degrees, 15 degrees, 30 degrees and 45 degrees with respect to the load direction) were considered for off-axis tests and two biaxial load ratios for biaxial tests to study failure characteristics and mechanism, Four classical polynomial failure criteria Tsai-Hill, Hoffman, Tsai-Wu and Yeh-Stratton-were analysed comparatively to predict off-axis and biaxial failure strength of the composites. For failure prediction of the plain woven composites under multiaxial tension loads, the Tsai-Wu criterion was modified by introducing an interaction coefficient F12 obtained from 45 degrees off-axis or biaxial tension tests and the Yeh-Stratton criterion was modified with the interaction coefficient B-12 = 0 or obtained from the biaxial tension test. The former criterion was found to have higher accuracy. Finally, according to macroscopic and microscopic studies, the failed specimens showed mostly distinct failure with a specific fracture orientation, mainly exhibiting fibre or fabric tensile fracture mode and a combination of matrix cracking and delamination, both in off-axis and cruciform samples. (C) 2017 Elsevier Ltd. All rights reserved.

ISSN号:0142-9418

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发表时间:2017-07-01

合写作者:Cai, Deng'an,Tang, Ju,Wang, Xiaopei,Li, Chao,Silberschmidt, Vadim V.

通讯作者:周光明