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Estimation Method for Mixed Mode (I+II) Interlaminar Fracture Toughness of Composite Laminates under Low-Velocity Impact Loading

机译:低速冲击载荷下复合层压板的混合模式(I + II)层间断裂韧性的估计方法

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摘要

A simple experimental method was developed in order to evaluate the mixed mode (I+II) interlaminar fracture toughness of polymer matrix composite laminates under low-velocity impact loading. The MMF (Mixed Mode Flexure) specimen was employed for determining the critical energy release rate at the onset of macroscopic crack growth. The SHPB (Split Hopkinson Pressure Bar) system was used for measuring the dynamic load and displacement. The dynamic response of the specimen was studied on the basis of computational results using finite element method. The dynamic stress field in the vicinity of the crack tip was similar to the static stress field when a slow-gradient ramped incident stress wave applied to the specimen. However, the dynamic stress field was largely oscillated with time when a stepped incident stress wave was applied. In the previous case, a simple formula based on static beam theory and compliance method could be applied for calculating the dynamic energy release rate. The experimental results agreed well with the above computational results.
机译:开发了一种简单的实验方法,以便在低速冲击载荷下评估聚合物基质复合层压板的混合模式(I + II)层间韧性。使用MMF(混合模式挠曲弯曲)样本用于确定宏观裂纹生长发作的临界能量释放率。 SHPB(Split Hopkinson压力条)系统用于测量动态负载和位移。使用有限元方法基于计算结果研究样本的动态响应。当施加到样本的慢梯度斜坡入射应力波时,裂纹尖端附近的动态应力场类似于静态应力场。然而,当施加阶梯式入射应力波时,动态应力场大致振荡。在前一种情况下,可以应用基于静态光束理论和合规方法的简单公式来计算动态能量释放率。实验结果与上述计算结果吻合得很好。

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