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首页> 外文期刊>Thin-Walled Structures >Dynamic crushing behavior of a multilayer thin-walled aluminum corrugated core: The effect of velocity and imperfection
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Dynamic crushing behavior of a multilayer thin-walled aluminum corrugated core: The effect of velocity and imperfection

机译:多层薄壁铝波纹芯的动态破碎行为:速度和缺陷的影响

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The crushing behavior of a multilayer 1050 H14 aluminum corrugated core was investigated both experimentally and numerically (LS-Dyna) using the perfect and imperfect models between 0.0048 and 90 m s(-1). The dynamic compression and direct impact tests were performed in a compression type and a modified Split Hopkinson Pressure Bar set-up, respectively. The investigated fully imperfect model of the corrugated core sample represented the homogenous distribution of imperfection, while the two-layer imperfect model the localized imperfection. The corrugated core experimentally deformed by a quasi-static homogenous mode between 0.0048 and 22 m s(-1), a transition mode between 22 and 60 m s(-1) and a shock mode at 90 m s(-1). Numerical results have shown that the stress-time profile and the layer crushing mode of the homogeneous and transition mode were well predicted by the two-layer imperfect model, while the stress-time profile and the layer crushing mode were well approximated by the fully imperfect model. The fully imperfect model resulted in complete sequential layer crushing at 75 and 90 m s(-1), respectively. The imperfect layers in the shock mode only affected the distal end stresses, while all models implemented resulted in similar impact end stresses. The distal end initial crushing stress increased with increasing velocity until about 22 m s(-1); thereafter, it saturated at similar to 2 MPa, which was ascribed to the micro inertial effect. Both the stress-time and velocity-time history of the rigid perfectly-plastic-locking model and the critical velocity for the shock deformation were well predicted when a dynamic plateau stress determined from the distal end stresses in the shock mode was used in the calculations.
机译:使用0.0048和90 m s(-1)之间的完美模型和不完美模型,通过实验和数值研究(LS-Dyna)研究了多层1050 H14铝波纹芯的破碎行为。动态压缩和直接冲击测试分别在压缩类型和改进的Split Hopkinson压力杆设置下进行。研究的瓦楞芯样品的完全不完美模型代表了缺陷的均匀分布,而两层不完美模型则是局部缺陷。瓦楞芯通过0.0048至22 m s(-1)之间的准静态均匀模式,22至60 m s(-1)之间的过渡模式和90 m s(-1)处的冲击模式进行实验变形。数值结果表明,通过两层缺陷模型可以很好地预测均质和过渡模式的应力时间分布和层破碎模式,而通过完全缺陷模型可以很好地近似应力-时间分布和层破碎模式。模型。完全不完美的模型分别导致75 m和90 m s(-1)的连续层破碎。冲击模式下的不完美层仅影响远端应力,而所实施的所有模型均产生相似的冲击端应力。远端初始压应力随着速度的增加而增加,直到约22 m s(-1)为止。之后,其饱和度接近2 MPa,这归因于微惯性效应。在计算中使用由远端模式下的远端应力确定的动态平台应力时,可以很好地预测刚性完美塑性锁定模型的应力时间和速度时间历史以及冲击变形的临界速度。 。

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