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Prediction of Elastic Properties of Honeycomb Core Materials and Analysis of Interlaminar Stress of Honeycomb Sandwich Composite Plate

机译:蜂窝芯材料弹性性能的预测及蜂窝夹层复合板岩体应力分析

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摘要

Theoretical formulas for effective elastic modulus and Poisson's ratio of honeycomb core materials were proposed considering the bending, axial and shear deformations of cell walls, Theoretical results obtained by the formulas showed orthotropic elasticity and large Poisson's ratio, which were comparable to results by finite element analysis(FEA). Tensile test of honeycomb sandwich composite(HSC) plates was performed for analysis of their deformation behaviors and interlaminar stresses. Equivalent plate model using the theoretical results of honeycomb core layer show that interlaminar shear stress occurring due to large difference of Poisson's ratio between skin and honeycomb core layers led to the delamination in HSC plate under tensile loading. Load-displacement behavior of HSC specimen simulated by equivalent plate model coincided fairly with that of detailed FEA model similar to experimental results.
机译:提出了考虑细胞壁弯曲,轴向和剪切变形的有效弹性模量和泊松核心材料比例的理论公式,通过公式获得的理论结果显示出正交弹性和大泊松比率,与有限元分析的结果相当(FEA)。进行蜂窝夹层复合物(HSC)板的拉伸试验,用于分析它们的变形行为和层间应力。使用蜂窝核心层的理论结果的等效板模型表明,由于皮肤和蜂窝芯层之间的泊松比差异的大差异而导致了在拉伸载荷下的HSC板中的分层而导致的跨界剪切应力。相同板模型模拟的HSC样本的负荷 - 位移行为与类似于实验结果的详细FEA模型相互作用。

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