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Mode I and Mode II interlaminar fracture toughness of glass-cloth/epoxy laminates at cryogenic temperatures

机译:模式I和模式II在低温温度下玻璃布/环氧层压板的Interlaminar裂缝韧性

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Experiments and analysis on glass-cloth/epoxy laminate double cantilever (DCB) and end-notched flexure (ENF) specimens are presented. The Mode I and Mode II interlaminar fracture tests were conducted by the DCB and ENF test methods, respectively, at room temperature, liquid nitrogen temperature (77 K) and liquid helium temperature (4 K). the effects of temperature and geometrical variations on the interlaminar fracture toughness are shown graphically. The fracture surfaces were also examined by scanning electron microscopy to verify the fracture mechanisms. A finite element model was further used to perform the delamination crack analysis. Critical load levels, and the geometric and material properties of the test specimens were input data for the analysis which evaluated the Mode I and Mode II energy release rate at onset of delamination crack propagation. The results of the finite element analysis are utilized to supplement the experimental data.
机译:呈现了玻璃布/环氧树脂层压双悬臂(DCB)和末端缺口弯曲(ENF)标本的实验和分析。模式I和模式II层间裂缝试验分别通过DCB和ENF试验方法进行,在室温,液氮温度(77k)和液氦温度(4k)中进行。图形地示出了温度和几何变化对层间断裂韧性的影响。还通过扫描电子显微镜检查骨折表面以验证断裂机制。有限元模型进一步用于进行分层裂纹分析。临界负载水平,测试样本的几何和材料特性是分析的输入数据,其评估了模式I和模式II能量释放率,以分层裂纹传播的发作。有限元分析的结果用于补充实验数据。

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