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Calculation of Stress Intensity Factors for Interfacial Cracks in Fiber Metal Laminates

机译:金属纤维层合板界面裂纹应力强度因子的计算

摘要

Stress intensity factors for interfacial cracks in Fiber Metal Laminates (FML) are computed by using the displacement ratio method recently developed by Sun and Qian (1997, Int. J. Solids. Struct. 34, 2595-2609). Various FML configurations with single and multiple delaminations subjected to different loading conditions are investigated. The displacement ratio method requires the total energy release rate, bimaterial parameters, and relative crack surface displacements as input. Details of generating the energy release rates, defining bimaterial parameters with anisotropic elasticity, and selecting proper crack surface locations for obtaining relative crack surface displacements are discussed in the paper. Even though the individual energy release rates are nonconvergent, mesh-size-independent stress intensity factors can be obtained. This study also finds that the selection of reference length can affect the magnitudes and the mode mixity angles of the stress intensity factors; thus, it is important to report the reference length used with the calculated stress intensity factors.
机译:使用Sun和Qian(1997,Int。J. Solids。Struct。34,2595-2609)最近开发的位移比方法,计算了纤维金属层压板(FML)中界面裂纹的应力强度因子。研究了在不同加载条件下具有单个和多个分层的各种FML配置。位移比方法需要总能量释放率,双材料参数和相对裂纹表面位移作为输入。本文讨论了产生能量释放速率,定义具有各向异性弹性的双材料参数以及选择适当的裂纹表面位置以获得相对裂纹表面位移的细节。即使各个能量释放速率不收敛,也可以获得与网格大小无关的应力强度因子。研究还发现,参考长度的选择会影响应力强度因子的大小和模态混合角。因此,重要的是报告与计算出的应力强度因子一起使用的参考长度。

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    Wang John T.;

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  • 年度 2009
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