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首页> 外文期刊>Progress in Aerospace Sciences >Behavior of curved laminated composite panels and shells under axial compression
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Behavior of curved laminated composite panels and shells under axial compression

机译:弯曲层压复合板和壳在轴向压缩下的行为

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摘要

The buckling and post-buckling behavior of curved cylindrical stringer-stiffened laminated composite and metal panels had been investigated both numerically and experimentally. The results were compared to those of cylindrical stringer-stiffened laminated composite shells to yield a way of determining the optimal structure to be used for axial compression loading. For the present tested structures, the composite panels showed the best load-weight ratio. (C) 2015 Elsevier Ltd. All rights reserved.
机译:数值和实验研究了弯曲的圆柱形纵梁加劲层合复合材料和金属板的屈曲和屈曲后行为。将结果与圆柱桁架加劲的层压复合材料壳的结果进行比较,以得出确定用于轴向压缩载荷的最佳结构的方法。对于目前测试的结构,复合板显示出最佳的负载重量比。 (C)2015 Elsevier Ltd.保留所有权利。

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