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Cycle-based analysis of damage and failure in advanced composites under fatigue 2. Stochastic mesomechanics modeling

机译:疲劳条件下高级复合材料基于损伤的循环分析2.随机细观力学模型

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Overall damage and failure in advanced composites under cyclic loading are described based on the damage development within loading cycles. The development of scattered damage in a composite over the cyclic load range and during loading and unloading was studied by acoustic emission in Part 1 of this work. In this paper, a novel general model of damage evolution and failure of laminates under cyclic loading is developed based on a stochastic mesomechanics approach. The model combines a lamination theory and a theory of stochastic processes. The randomness of the elastic and strength properties of the composite plies, the laminate microslructural parameters, and the loading are taken into account. A theory of excursions of stochastic processes beyond bounds and a mesovolume concept are utilized to evaluate the ply-level damage functions. The capablities of the approach are illustrated on an example of damage and failure analysis of a laminate under low-cycle tensile loading. The new cycle-based model is found capable of predicting the experimentally observed stages in the overall fatigue damage process, i.e. the initial damage, the gradual damage development, and the final failure. The relative durations of these stages are found to be dependent on the fatigue loading parameters. The predicted damage development over the range of fatigue loading also correlates with the experimental observations. These predictions are intrinsic to the developed stochastic-process-based approach and do not require explicit experimental information on the fatigue damage behavior or stiffness degradation. These results shed light on the fundamental mechanisms of fatigue damage development in advanced composites. The new model treats fatigue of composites as a legitimate load- and time-dependent damage accumulation process within loading cycles. It is expected to be useful for fundamental studies of the effects of variable amplitude, frequency, and cycle shape on the fatigue behavior of advanced composite materials.
机译:基于循环载荷下的损伤发展,描述了循环载荷下高级复合材料的整体损伤和破坏。在这项工作的第1部分中,通过声发射研究了复合材料在循环载荷范围内以及在加载和卸载过程中的分散损伤的发展。在本文中,基于随机细观力学方法,开发了一种新型的循环载荷作用下层板损伤演化和破坏的通用模型。该模型结合了分层理论和随机过程理论。考虑复合材料层的弹性和强度特性的随机性,层压材料的微结构参数和载荷。利用随机过程的偏移理论和中体积概念来评估层级损伤函数。在层压板在低循环拉伸载荷下的损坏和失效分析的示例中说明了该方法的功能。发现新的基于周期的模型能够预测整个疲劳损伤过程中实验观察到的阶段,即初始损伤,逐渐的损伤发展和最终失效。发现这些阶段的相对持续时间取决于疲劳载荷参数。在疲劳载荷范围内预测的损伤发展也与实验观察结果相关。这些预测是已开发的基于随机过程的方法所固有的,不需要有关疲劳损伤行为或刚度退化的明确实验信息。这些结果阐明了高级复合材料中疲劳损伤发展的基本机理。新模型将复合材料的疲劳视为载荷周期内合法的,依赖于时间和时间的损伤累积过程。有望对可变振幅,频率和循环形状对高级复合材料疲劳行为的影响进行基础研究有用。

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