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On the characteristic damage state for composite laminates based on analysis of the interfacial stresses

机译:基于界面应力分析的复合材料层合板的特征损伤状态

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An exact solution for stresses and strains in composite laminates with the lay-up [0°m/90°n] is presented in this paper.First,the shear stresses between the 90° and 0° plies are assumed to be in the form of series expansion of sinusoidalfunctions.Then the stress components in laminates have corresponding series expressions based on equilibrium equations,boundary conditions and continuous conditions at the interface.Use of the principle of minimum potential energy leads to the algebraic equations for unknown coefficients in series.Further,cyclic differential function is introduced to express analytically the resulting stresses in laminates.As an application,reduction of Young's modulus and change in Poisson's ratio for various laminates are evaluated and compared with experimental and predicted results available.The results show that the present solution is accurate enough in computation,and suitable to exact analysis of characteristic damage state for composite laminates.
机译:本文给出了层合为[0°m / 90°n]的复合材料层合板中应力和应变的精确解。首先,假定层板在90°和0°之间的剪应力为层合板中的应力分量基于界面上的平衡方程,边界条件和连续条件具有相应的级数表达式。利用最小势能原理导致未知系数级数的代数方程。循环微分函数被引入以分析地表达层压板中所产生的应力。作为一种应用,评估了各种层压板的杨氏模量的降低和泊松比的变化,并将其与可用的实验和预测结果进行了比较。结果表明,本解决方案是在计算上足够准确,并且适​​合对复合材料层压板的特征损伤状态进行精确分析。

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