An extended analytical model for predicting the compressive failure behaviors of composite laminate with an arbitrary elliptical delamination

INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES

卷:185

Article

Wang, Kangkang^1,2  Zhao, Libin^1,2  Hong, Haiming³  Zhang, Jianyu⁴  Hu, Ning⁴ 

[1] Beihang Univ, Sch Astronaut, Beijing 100191, Peoples R China

[2] Beihang Univ, Key Lab Spacecraft Design Optimizat & Dynam Simul, Minist Educ, Beijing 100191, Peoples R China

[3] Shenyang Aircraft Design & Res Inst, Shenyang 110035, Peoples R China

[4] Chongqing Univ, Coll Aerosp Engn, Chongqing 400044, Peoples R China

关键词: Composite;    Delamination;    Laminate theory;    Buckling;    Failure behaviors;   

DOI  :  10.1016/j.ijsolstr.2019.09.002

来源: Elsevier

【 摘 要 】

Delamination is one of the most serious failure modes in carbon fiber reinforced composite laminates, because it can reduce the overall stiffness, which further leads to premature structural buckling and failure at loads below the design level. Arbitrary elliptical delamination is the most representative case in engineering practice, and the delamination propagation and failure behaviors are much complicated. To completely evaluate the compressive failure behaviors of composite laminate with arbitrary elliptical delaminations, an extended analytical model was established based on the first order shear deformation theory and brittle fracture mechanics. The analytical model innovatively incorporated the failure evaluation, and especially the delamination propagation path into buckling analysis of composite laminate containing an arbitrary elliptical delamination. The predicted results are highly consistent with the outcomes of uniaxial compression tests, thus validating the applicability and accuracy of the analytical model as a highly efficient tool in engineering practices for the most representative arbitrary elliptical delamination problems. It is found that the propagation of the elliptical deamination in composites was fast and unstable, which led to catastrophic failures. The delamination propagation tends to initiate from the delamination boundary points with the maximum transverse coordinates and propagate transversely to the loading direction. (C) 2019 Published by Elsevier Ltd.

【 授权许可】

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