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首页> 外文期刊>Journal of aerospace engineering >Damage and Failure of Laminated Carbon-Fiber-Reinforced Composite under Low-Velocity Impact
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Damage and Failure of Laminated Carbon-Fiber-Reinforced Composite under Low-Velocity Impact

机译:低速冲击下叠层碳纤维增强复合材料的破坏和失效

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摘要

In this paper, experimental and numerical studies are conducted to study the damage and failure behavior of a laminated T700/ BA9912 composite under low-velocity impact. The three-dimensional (3D) Hashin damage criterion and the cohesive zone model are used in the finite-element analysis, and the numerical simulation reveals the delamination, matrix damage, and fiber breakage process in the material. To show the capacity and fidelity of the numerical model, a drop-weight test and a nondamage inspection (NDI) are performed, and the model predictions are compared with the test results. The numerical model is able to predict the load versus impact time responses of the specimens. The predicted size and shape of the delamination area show excellent agreement with the NDI result, and the predicted through-thickness matrix failure directly below the impactor and the fiber breakage in the bottom layers of the laminates are in good agreement with the experimental observations.
机译:本文通过实验和数值研究来研究低速冲击下T700 / BA9912层压复合材料的损伤和破坏行为。在有限元分析中使用了三维(3D)Hashin损伤准则和内聚区模型,数值模拟显示了材料的分层,基质损伤和纤维断裂过程。为了显示数值模型的能力和保真度,进行了落锤测试和无损检查(NDI),并将模型预测与测试结果进行了比较。数值模型能够预测样品的载荷对冲击时间的响应。脱层区域的预测尺寸和形状与NDI结果显示出极佳的一致性,并且在冲击器正下方的预测的全厚度基体破坏和层压板底层的纤维断裂与实验观察结果非常吻合。

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