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首页> 外文期刊>Journal of Sandwich Structures and Materials >Experimental Investigation of Compression Failure Mechanisms of Composite Faced Foam Core Sandwich Specimens
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Experimental Investigation of Compression Failure Mechanisms of Composite Faced Foam Core Sandwich Specimens

机译:复合面泡沫芯夹心试样压缩破坏机理的实验研究

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Compression failure of sandwich specimens with glass/vinylester face sheets over PVC foams has been experimentally examined using an end loading test fixture based on the ASTM C 364 standard. The main objective of the research was to examine the roles of the faces and core in the mechanism of failure and ultimate load carrying ability of the structure. A range of PVC foam densities, core thicknesses, and specimen lengths were examined. Failure modes were identified, and compression strengths were compared to analytical predictions. Short specimens failed by compression failure of the face sheets up to a gage length that increased with increased foam density, and decreasing core thickness. At intermediate gage lengths it was found that specimens with a thick low density core failed in an antisymmetric face wrinkling mode, while long specimens failed by global buckling in the fundamental buckling mode. Predictions of the failure loads were found to be in reasonable agreement with experimental results.
机译:使用基于ASTM C 364标准的末端载荷测试夹具,已通过实验检查了玻璃/乙烯基酯面板在PVC泡沫上的三明治样品的压缩破坏。研究的主要目的是研究面和核心在结构破坏和极限承载能力中的作用。检查了一系列PVC泡沫密度,芯厚度和样本长度。确定了失效模式,并将抗压强度与分析预测值进行了比较。短的试样由于面板的压缩破坏而失败,直至厚度随着泡沫密度的增加和芯厚度的减小而增加。在中等规距长度下,发现具有厚低密度芯的试样在反对称的表面起皱模式下失效,而长试样在基本屈曲模式下由于整体屈曲而失效。发现失效载荷的预测与实验结果合理吻合。

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