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首页> 外文期刊>International Journal of Plasticity >Quasi-static crush behavior of aluminum honeycomb specimens under compression dominant combined loads
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Quasi-static crush behavior of aluminum honeycomb specimens under compression dominant combined loads

机译:压缩主导复合载荷作用下铝蜂窝试样的准静态挤压行为

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摘要

The influence of shear stress on the quasi-static crush behavior of alurninuin honeycomb specimens under compression dominant combined loads is investigated by experiments. A test fixture was designed such that dominant compressive and shear loads with respect to the strongest material symmetry direction can be controlled and applied independently. Honeycomb specimens were also designed such that the secondary non-uniform stresses due to the stress-free boundary can be minimized. The experimental results indicate that the normal crush strengths under combined compressive and shear loads are lower than that under pure compressive loads. A phenomenological yield criterion for specimens with different in-plane orientation angles is proposed based on the experimental normal crush and shear strengths under combined loads. The experimental results suggest non-normality plastic flow based on the yield criterion. The non-normality flow behavior becomes more pronounced as the in-plane orientation angle increases. The experimental results also indicate that the energy absorption rate depends upon the ratio of the shear stress to the compressive stress and the in-plane orientation angle. In addition, specimens crushed under combined loads show inclined stacking patterns of folds due to the asymmetric location of horizontal plastic hinge lines and the rupture of aluminum cell walls along the adhesive lines. These experimental observations are useful to develop microscopic plasticity models of aluminum honeycombs under compression dominant combined loads. (c) 2005 Elsevier Ltd. All rights reserved.
机译:通过实验研究了剪切应力对铝压蜂窝材料在压缩主导复合载荷作用下的准静态挤压行为的影响。设计了一种测试夹具,可以相对于最强的材料对称方向独立控制和施加主要的压缩和剪切载荷。还设计了蜂窝状样品,以使由于无应力边界引起的次级不均匀应力最小化。实验结果表明,在组合压缩和剪切载荷下的正常抗压强度低于在纯压缩载荷下的正常抗压强度。基于组合载荷下的正常法向抗压强度和抗剪强度,提出了不同面内取向角试样的物候屈服准则。实验结果表明基于屈服准则的非正常塑性流动。随着面内取向角的增加,非正常流动行为变得更加明显。实验结果还表明,能量吸收率取决于剪切应力与压缩应力之比和面内定向角。此外,由于水平塑料铰链线的不对称位置以及铝制细胞壁沿粘合线的破裂,在组合载荷作用下压碎的样品显示出倾斜的褶皱堆积模式。这些实验观察对于建立铝蜂窝在压缩主导组合载荷下的微观可塑性模型很有用。 (c)2005 Elsevier Ltd.保留所有权利。

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