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Experimental-numerical study into the stability and failure of compressed thin-walled composite profiles using progressive failure analysis and cohesive zone model

机译:使用渐进式破坏分析和粘性区模型压缩薄壁复合材料稳定性和压缩薄壁复合材料稳定性和失效的实验数值研究

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This study investigates the stability and failure of thin-walled composite structures with a top-hat cross section under axial compressive loading. The tested profiles were made of CFRP composite material by autoclaving. The scope of the research included experimental tests of real samples and numerical analysis by the finite element method using the ABAQUS (R) program. Both experimental tests and numerical analysis were performed over the full range of loading until structural failure. In experiments, postbuckling equilibrium paths and acoustic emission signals were measured, which allowed a comprehensive analysis of failure for the composite material. Numerical calculations were performed by progressive failure analysis, considering the failure initiation criteria under Hashin's theory and failure evolution based on the energy criterion. Additionally, the cohesive zone model (CZM) was used to simulate delamination. Numerical results and experimental findings show high agreement. Moreover, the results reveal an interesting relationship between the compressive load and the buckling, postbuckling and failure of the analyzed structures.
机译:本研究调查薄壁复合结构在轴向压缩载荷下用顶帽横截面的稳定性和失效。通过高压灭菌由CFRP复合材料制成的测试型材。该研究的范围包括使用ABAQUS(R)程序的有限元方法的真实样品和数值分析的实验测试。在整个装载范围内进行实验测试和数值分析,直至结构失败。在实验中,测量出现的均衡路径和声发射信号,这允许复合材料的失效综合分析。通过逐步失败分析进行数值计算,考虑到哈希本林理论和失败进化的故障启动标准,基于能量标准进行了衰竭。另外,粘性区域模型(CZM)用于模拟分层。数值结果与实验结果显示高协议。此外,结果揭示了抗压载荷和屈曲,后突破和分析结构失效之间的有趣关系。

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