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Experimental investigation of buckling of dented cylindrical shells under axial compression

机译:轴向压缩下牙齿圆柱壳弯曲的实验研究

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The results of unique experimental studies of buckling of dented axially compressed unstiffened cylindrical shells are provided in the suggested paper. The dimple-like geometrical imperfections of different shape, size, deflection amplitude, and number of dents were created on cylindrical shells before axial loading. The initial deflection amplitude varied in the wide range, up to several shell thicknesses. In all cases the plateaus were discovered on the buckling load initial deflection diagrams. Corresponding axial loads were close to local lower buckling loads of perfect shells. These loads are defined as minimum values of axial force when the post-buckling equilibrium states of the perfect structure with one or several dimples exist. It was shown that the lower local buckling loads slightly depend on geometrical imperfections and therefore can be used for estimation of design buckling load of the structure. Over 50 specimens were tested. Pre-buckling and post-buckling behavior of imperfect shells was studied.
机译:在建议的纸张中提供了对弯曲轴向压缩的不稳定圆柱壳的独特实验研究的结果。在轴向载荷之前在圆柱形壳上产生不同形状,尺寸,偏转幅度和凹痕数的凹坑状几何缺陷。初始偏转幅度在宽范围内变化,直至几个壳体厚度。在所有情况下,在屈曲负载初始偏转图中发现了平台。相应的轴向载荷接近局部下屈曲的完美壳。当存在一个或多个凹坑的完美结构的后屈曲平衡状态时,这些载荷定义为轴向力的最小值。结果表明,较低的局部屈曲负载略微取决于几何缺陷,因此可用于估计结构的设计屈曲负荷。测试了超过50个标本。研究了不完美壳的预屈曲和后屈曲行为。

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