首页> 外文会议>International Conference on Fracture and Strength of Solids(FEOFS 2005) pt.2; 20050404-06; Bali(ID) >Prediction of Elastic Properties of Honeycomb Core Materials and Analysis of Interlaminar Stress of Honeycomb Sandwich Composite Plate
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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预测及蜂窝夹芯复合板层间应力分析

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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:提出了蜂窝壁材料的有效弹性模量和泊松比的理论公式,并考虑了蜂窝壁的弯曲,轴向和剪切变形,该公式获得的理论结果显示正交各向异性弹性和大泊松比,与有限元分析的结果具有可比性。 (FEA)。进行了蜂窝夹芯复合材料板的拉伸试验,以分析其变形行为和层间应力。利用蜂窝芯层理论结果的等效板模型表明,由于表皮层和蜂窝芯层之间的泊松比之差较大而产生的层间剪切应力导致HSC板在拉伸载荷下分层。用等效板模型模拟的HSC试样的载荷-位移行为与详细的FEA模型相吻合,与实验结果相似。

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