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首页> 外文期刊>International journal of impact engineering >The mechanical behaviors of corrugated sandwich panel under quasi-static and dynamic shear-compressive loadings
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The mechanical behaviors of corrugated sandwich panel under quasi-static and dynamic shear-compressive loadings

机译:准静态和动态剪切压缩载荷下瓦楞三明治面板的机械行为

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摘要

This paper studies the quasi-static and dynamic mechanical behaviors of a commercial corrugated sandwich panel under combined shear-compressive loading by using a modified MTS machine and the so-called Rotatable Hopkinson Bar (RHB) loading system. Particular focus is placed on identifying the differences of large deformation behaviors of corrugation panels between uniaxial compression and combined shear-compression, especially the influences of shear-compressive loading angle and loading rate on the stress-displacement curves and the deformation modes. It is found that the normal stress decreases with the loading angle, while the shear stress increases with it for both the quasi-static and dynamic loadings. Three deformation patterns are identified for five different loading angles from 0o (corresponding to uniaxial compression) to 50o. A positive loading rate effect is found for the initial collapse of corrugated panels, which is contributed to the inertia effect within corrugation buckling. The strength of the panels after initial collapse shows a negative loading rate effect, which may be due to the strain softening behavior of base material (5754-H48 Aluminum alloy) at impact loading.
机译:本文通过使用改进的MTS机器和所谓的旋转霍普金森棒(RHB)装载系统,研究了在组合剪切压缩负载下的商用瓦楞夹层板的准静态和动态机械行为。识别单轴压缩和组合剪切压缩之间的波纹板的大变形行为的差异,特别是剪切压缩加载角和装载速率对应力 - 位移曲线和变形模式的影响。结果发现,正常应力随装载角减小,而剪切应力随着准静态和动态负载而增加。从0O(对应于单轴压缩)到50o的五个不同的装载角度识别三个变形图案。发现阳性加载率效应对于瓦楞纸板的初始塌陷,这导致波纹屈曲中的惯性效应。初始塌陷后面板的强度显示出负负载率效应,这可能是由于基材(5754-H48铝合金)在冲击载荷时的应变软化行为。

著录项

  • 来源
    《International journal of impact engineering》 |2021年第10期|103956.1-103956.11|共11页
  • 作者单位

    Northwestern Polytech Univ Sch Aeronaut Xian 710072 Peoples R China|Joint Int Res Lab Impact Dynam & Engn Applicat Xian 710072 Peoples R China|Shaanxi Key Lab Impact Dynam & Engn Applicat Xian 710072 Peoples R China;

    Northwestern Polytech Univ Sch Aeronaut Xian 710072 Peoples R China;

    Northwestern Polytech Univ Sch Aeronaut Xian 710072 Peoples R China|Joint Int Res Lab Impact Dynam & Engn Applicat Xian 710072 Peoples R China|Shaanxi Key Lab Impact Dynam & Engn Applicat Xian 710072 Peoples R China;

    Univ Paris Saclay Lab Mecan & Technol ENS Paris Saclay CNRS 61 Ave President Wilson F-94235 Cachan France|Univ Pierre & Marie Cuire Sorbonnes Univ UFR Ingn Paris France;

    Aircraft Strength Res Inst China Aviat Key Lab Sci & Technol Struct Impact Dynam Xian 710065 Peoples R China;

    Northwestern Polytech Univ Sch Aeronaut Xian 710072 Peoples R China|Joint Int Res Lab Impact Dynam & Engn Applicat Xian 710072 Peoples R China|Shaanxi Key Lab Impact Dynam & Engn Applicat Xian 710072 Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Corrugated panel; Shear-compression; Impact loading; Loading rate effect;

    机译:瓦楞纸板;剪切压缩;冲击载荷;装载率效果;

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