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A Method for Calculating Strain Energy Release Rates in Preliminary Design of Composite Skin/Stringer Debonding Under Multi-Axial Loading

机译:多轴载荷下蒙皮/纵梁复合剥离初步设计中应变能释放率的计算方法

摘要

Three simple procedures were developed to determine strain energy release rates, G, in composite skin/stringer specimens for various combinations of unaxial and biaxial (in-plane/out-of-plane) loading conditions. These procedures may be used for parametric design studies in such a way that only a few finite element computations will be necessary for a study of many load combinations. The results were compared with mixed mode strain energy release rates calculated directly from nonlinear two-dimensional plane-strain finite element analyses using the virtual crack closure technique. The first procedure involved solving three unknown parameters needed to determine the energy release rates. Good agreement was obtained when the external loads were used in the expression derived. This superposition technique was only applicable if the structure exhibits a linear load/deflection behavior. Consequently, a second technique was derived which was applicable in the case of nonlinear load/deformation behavior. The technique involved calculating six unknown parameters from a set of six simultaneous linear equations with data from six nonlinear analyses to determine the energy release rates. This procedure was not time efficient, and hence, less appealing. A third procedure was developed to calculate mixed mode energy release rates as a function of delamination lengths. This procedure required only one nonlinear finite element analysis of the specimen with a single delamination length to obtain a reference solution for the energy release rates and the scale factors. The delamination was extended in three separate linear models of the local area in the vicinity of the delamination subjected to unit loads to obtain the distribution of G with delamination lengths. This set of sub-problems was Although additional modeling effort is required to create the sub- models, this local technique is efficient for parametric studies.
机译:开发了三种简单的程序来确定复合材料蒙皮/桁条样品中的应变能释放速率G,用于单轴和双轴(面内/面外)加载条件的各种组合。这些过程可用于参数设计研究,以便对许多载荷组合的研究仅需进行少量有限元计算即可。将结果与使用虚拟裂纹闭合技术直接从非线性二维平面应变有限元分析计算出的混合模式应变能释放率进行了比较。第一个过程涉及解决确定能量释放速率所需的三个未知参数。当在导出的表达式中使用外部载荷时,获得了良好的一致性。仅当结构表现出线性载荷/挠曲行为时,此叠加技术才适用。因此,得出了第二种技术,该技术适用于非线性载荷/变形行为。该技术涉及从六个同时线性方程组中计算六个未知参数,以及六个非线性分析的数据来确定能量释放率。此过程时间效率不高,因此吸引力较小。开发了第三种方法来计算作为分层长度函数的混合模式能量释放速率。此过程仅需对具有单个分层长度的样本进行一次非线性有限元分析,即可获得能量释放速率和比例因子的参考解。分层在单元负荷下分层附近的局部区域的三个单独的线性模型中扩展,以获得具有分层长度的G的分布。这组子问题是尽管创建子模型需要额外的建模工作,但是这种局部技术对于参数研究非常有效。

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