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Deformation and progressive failure. behavior of woven-fabric-reinforced glass/epoxy composite laminates under tensile, loading at cryogenic temperatures

机译:变形和渐进破坏。机织织物增强的玻璃/环氧树脂复合层压板在低温下的拉伸,负荷下的性能

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This paper focuses on understanding the deformation and progressive failure behavior of glass/epoxy plain weave fabric-reinforced laminates subjected to uniaxial tension at cryogenic temperatures. Cryogenic tensile tests were conducted on the woven-fabric laminates, and the damage development during loading was characterized by AE (acoustic emission) measurements. A finite element model for progressive failure analysis of woven-fabric composite panels was also developed, and applied to simulate the "knee" behavior in the stress-strain responses and the damage behavior in the tensile test specimens. Failure of the epoxy resin matrix in the transverse fiber bundle was predicted to occur using the maximum strain failure criterion. The effect of strain concentrations due to the fabric architecture on the failure strain of the material was considered by incorporating the SVF (strain variation factor) from the meso-scale analysis of a woven-fabric composite unit into the macro-scale analysis of the specimens. A comparison was made between the finite element predictions and the experimental data, and the agreement is good.
机译:本文着重了解在低温下承受单轴张力的玻璃/环氧树脂平纹织物增强层压材料的变形和渐进破坏行为。在机织织物层压板上进行了低温拉伸试验,并通过AE(声发射)测量来表征加载过程中的损伤发展。还开发了用于织物复合材料面板渐进式破坏分析的有限元模型,并将其用于模拟应力-应变响应中的“膝盖”行为和拉伸试样中的破坏行为。使用最大应变破坏准则,预计发生横向纤维束中环氧树脂基质的破坏。通过将织造织物复合材料单元的中尺度分析中的SVF(应变变化因子)纳入样本的宏观分析中,考虑了由于织物结构而引起的应变集中对材料破坏应变的影响。 。在有限元预测和实验数据之间进行了比较,一致性很好。

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