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Failure assessment on central-sharp notched carbon/epoxy laminates

机译:中央锋利缺口碳/环氧树脂层压板的失效评估

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摘要

Fracture models to predict the strength of laminated composites having sharp notches demand the un-notched strength and the critical damage size ahead of the notch. The critical damage size, in general, depends on the material, geometry of the specimen and size of the sharp notch. The extraordinary success of a fracture model lies in its ability to combine a theoretical framework with experimentally measured quantities. Modifications are made in one of the stress-fracture criteria known as the point stress criterion for accurate prediction of notched tensile strength of composite laminates containing sharp notches. To examine the adequacy of these modifications, fracture data of central-sharp notched carbon/epoxy composite laminates with various lay-ups are considered. The notched strength estimates are found to be close to the test results. The modified point stress criterion is very simple and accurate in predicting the notched tensile strength of laminated composites.
机译:用来预测具有尖锐缺口的层压复合材料强度的断裂模型要求在缺口之前具有无缺口的强度和临界破坏尺寸。通常,临界损伤的大小取决于材料,试样的几何形状和尖锐缺口的大小。裂缝模型的非凡成功在于其将理论框架与实验量相结合的能力。对一种应力-断裂标准(称为点应力标准)进行了修改,以精确预测包含尖锐缺口的复合材料层压板的缺口拉伸强度。为了检查这些修改的适当性,考虑了具有各种铺层的中央锋利缺口碳/环氧树脂复合材料层压板的断裂数据。发现缺口强度估算值接近测试结果。修正的点应力准则在预测层压复合材料的缺口抗拉强度方面非常简单且准确。

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