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首页> 外文期刊>Physica status solidi, B. Basic research >Mixed auxeticity of auxetic sandwich structures
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Mixed auxeticity of auxetic sandwich structures

机译:膨胀夹层结构的混合膨胀性

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Previously, a sandwich structure in which the Poisson ratios of the core and facesheets possess opposite signs has been shown to exhibit overall conventional and auxetic behavior depending on the loading mode – axial loading or bending – for an intermediate range of relative core thickness. In addition to these two loading modes, sandwich structures in aerospace applications encounter torsional loads. In this paper, the effective Poisson's ratio for torsional loading is proposed. Results show that, depending on the loading mode and the relative core thickness, there can be up to four levels of overall auxeticity, namely (i) full auxeticity (FA) if the structure behaves as an auxetic structure under all three modes of loading, (ii) high auxeticity (HA) if the structure behaves as an auxetic structure in two of the loading modes, (iii) low auxeticity (LA) if the structure behaves as an auxetic structure in only one of the loading modes, and (iv) no auxeticity (NA) if the structure behaves as a conventional structure under all of the three loading modes. These results indicate that by selecting the Poisson's ratios and the thickness of the cores and facesheets, the sandwich structure can be made to respond differently under different external loading conditions.
机译:以前,已显示出芯和面板的泊松比具有相反符号的三明治结构,在相对芯厚度的中间范围内,根据加载模式(轴向加载或弯曲),会表现出总体常规和拉力行为。除了这两种加载模式外,航空航天应用中的夹层结构还会遇到扭转载荷。本文提出了扭转载荷的有效泊松比。结果表明,根据加载方式和相对芯厚,最多可以有四个级别的整体膨胀性,即(i)如果结构在所有三种加载方式下均表现为膨胀性结构,则为全膨胀性(FA), (ii)如果结构在两种加载模式下均表现为膨胀结构,则为高膨胀性(HA);(iii)如果结构仅在一种加载模式下表现为膨胀结构,则为低膨胀性(LA);并且(iv ),如果结构在所有三种加载模式下均表现为常规结构,则没有膨胀性(NA)。这些结果表明,通过选择泊松比以及纤芯和面板的厚度,可以使夹层结构在不同的外部载荷条件下具有不同的响应。

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