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A regularized orthotropic continuum damage model for layered composites: intralaminar damage progression and delamination

机译:分层复合材料的正数正交连续损伤模型:史内非损伤进展和分层

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摘要

Predicting progressive damage in composite materials is essential for the design of most lightweight constructions. When laminated composite structures are considered, both intralaminar and interlaminar (delamination) damage evolution need to be addressed. Typically, these different damage modes are treated separately. On the contrary, in this paper, a continuum damage model is presented which is capable of modeling orthotropic damage progression within layers as well as delamination. The model is formulated in a thermodynamically consistent manner. Moreover, the results are mesh independent due to a fracture energy based regularization scheme.
机译:预测复合材料中的渐进损坏对于大多数轻质结构的设计至关重要。 当考虑层压复合结构时,需要解决胰蛋白酶和层间(分层)损坏进化。 通常,这些不同的损坏模式分别处理。 相反,在本文中,提出了一种连续损伤模型,其能够在层内和分层内建模正交损伤进展。 该模型以热力学上的方式配制。 此外,由于基于裂缝能量的正则化方案,结果是独立的。

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