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Improvement of Axial Load Capacity of Elliptical Cylindrical Shells

机译:椭圆圆柱壳轴向载荷能力的提高

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By varying the thickness of the cylinder wall with circumferential position, the axial buckling capacities of homogeneous, isotropic cylindrical shells with elliptical cross sections are improved. The classic buckling stress relation for a uniform-thickness homogeneous, isotropic circular cylindrical shell is applied to cylinders with elliptical cross sections. It is assumed that this relation can be used to design the wall thicknesses of elliptical cylinders as a function of circumferential location to compensate for the negative effects of the variation of the radius of curvature with circumferential location. Three variable-thickness elliptical cylinder designs are proposed, and analytical expressions for the thickness variation, cross-sectional area, axial buckling stress, axial buckling stress resultant, and axial buckling load for each design are derived. Predictions from the analytical development are then compared with finite element analyses of the three designs. So-called small and large cylinders with three values of eccentricity are considered. The comparisons between the finite element results and the analytic predictions are quite good. It is shown that considerable improvement in axial buckling capacity can be achieved with the thickness-tailoring technique, and in some cases the axial capacity of the circular cylinder with the same circumference is achieved.
机译:通过沿圆周位置改变气缸壁的厚度,可以提高具有椭圆形横截面的均质各向同性圆柱壳的轴向屈曲能力。均匀厚度的均质各向同性圆柱壳的经典屈曲应力关系适用于具有椭圆形横截面的圆柱体。假定该关系可用于根据圆周位置来设计椭圆圆柱的壁厚,以补偿曲率半径随圆周位置变化的负面影响。提出了三种变厚度椭圆圆柱设计,并推导了每种设计的厚度变化,横截面积,轴向屈曲应力,轴向屈曲应力合力和轴向屈曲载荷的解析表达式。然后将分析开发的预测结果与三种设计的有限元分析进行比较。考虑具有三个偏心率值的所谓的小气缸和大气缸。有限元结果与解析预测之间的比较是相当不错的。结果表明,通过厚度定制技术可以实现轴向屈曲能力的显着提高,并且在某些情况下,可以实现具有相同周长的圆柱的轴向屈曲能力。

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