共查询到20条相似文献,搜索用时 31 毫秒
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M. Bagheri A. A. Jafari M. Sadeghifar 《Archive of Applied Mechanics (Ingenieur Archiv)》2011,81(11):1639-1649
In this research, the general axial and radial buckling optimization of ring-stiffened cylindrical shells is implemented by
the genetic algorithm (GA). The stiffened shell is subjected to four constraints including the fundamental frequency, the
structural weight, the axial buckling load, and the radial buckling load. In addition, six design variables including shell
thickness, number of stiffeners, stiffeners width and height, stiffeners eccentricity distribution order, and stiffeners spacing
distribution order are considered. In analytical solution, the Ritz method is applied and stiffeners are treated as discrete
elements. The effect of the weighting coefficients of the objective functions on the optimum solution is studied. The results
show that optimized stiffening a cylindrical shell leads to a lower structural weight, higher natural frequencies, and larger
axial and radial buckling loads, simultaneously. In addition, the upper and lower bounds of the design variables influence
the optimum results considerably. It is also found that the distributions of eccentricity and spacing of the stiffeners influence
the magnitudes of the axial and radial buckling loads considerably. 相似文献
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充满液体弹塑性圆柱壳轴向冲击屈曲的数值模拟 总被引:4,自引:0,他引:4
基于对充满液体的弹塑性圆柱壳轴向冲击屈曲的实验观察 ,建立了相应的计算模型 ,借用 LS-DYNA软件包 ,在 HP-C36 0工作站上完成了数值模拟 ,得到了动画显示 ,给出的屈曲模态及一些特征量的时程曲线与实验结果相当一致。文中对壳的几何、物理参数对屈曲性能的影响进行了较详细的讨论 相似文献
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Buckling and Postbuckling of Laminated Thin Cylindrical Shells under Hygrothermal Environments 总被引:1,自引:0,他引:1
沈惠申 《应用数学和力学(英文版)》2001,22(3):270-281
IntroductionInrecentyears,fiber_reinforcedcompositelaminatedshellstructuresarewidelyusedintheaerospace ,marineindustry ,automobileindustryandotherengineeringapplications.Duringtheoperationallife ,thevarianceoftemperatureandmoisturereducestheelasticmoduli… 相似文献
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《International Journal of Solids and Structures》1999,36(4):597-617
The effect of local geometric imperfections on the buckling and postbuckling of composite laminated cylindrical shells subjected to combined axial compression and uniform temperature loading was investigated. The two cases of compressive postbuckling of initially heated shells and of thermal postbuckling of initially compressed shells are considered. The formulations are based on a boundary layer theory of shell buckling, which includes the effects of the nonlinear prebuckling deformation, the nonlinear large deflection in the postbuckling range and the initial geometric imperfection of the shell. The analysis uses a singular perturbation technique to determine buckling loads and postbuckling equilibrium paths. Numerical examples are presented that relate to the performances of cross-ply laminated cylindrical shells with or without initial local imperfections, from which results for isotropic cylindrical shells follow as a limiting case. Typical results are presented in dimensionless graphical form for different parameters and loading conditions. 相似文献
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The efficient compound strip method is used to analyse the buckling of ring-stiffened cylindrical shells under hydrostatic pressure. The eccentricity of stiffeners is taken into account. Numerical examples are given to illustrate the efficiency and accuracy of this method. 相似文献
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通过对拱顶储罐罐壁承受轴向载荷、初始几何缺陷及轴压失稳状况研究,指
出在固定顶罐设计、建造和运行各阶段都应进行罐壁轴压稳定性校核. 根据圆柱薄壳稳定性
理论和轴压失稳临界应力数值分析计算结果,提出固定顶罐罐壁轴压稳定性校核方法和数学
模型,并运用回归分析方法建立罐壁轴压失稳临界应力计算公式. 对几种常用规格的拱顶罐
有初始挠度缺陷罐壁轴压稳定性分析表明:随储罐容积和罐壁初始挠度增大,罐壁轴压稳定
性呈减弱趋势. 相似文献
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圆柱形薄壳冲击扭转屈曲的实验研究 总被引:1,自引:0,他引:1
本文对受冲击扭矩作用下的圆柱形簿壳扭转屈曲进行了实验研究,利用Hopkinson扭杆使圆柱受阶跃扭矩作用,分析所得到的应变-时间曲线,得到了不同几何参数的圆柱壳的冲击临界扭矩Mder和屈曲波数n及几条定性结论,同时找出了圆柱壳静力扭转屈曲行为和冲击扭转屈曲行为之间的异同。 相似文献
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轴向冲击圆柱壳非弹性响应 总被引:1,自引:0,他引:1
简要论述承受轴向冲击载荷圆柱壳非弹性动屈曲响应的研究进展。采用Karman-Donnell运动方程研究轴向流固冲击载荷作用下的圆柱壳轴对称弹塑性动屈曲问题。本构关系采用增量理论,借助增量数值方法求解动力方程组。研究不同边界条件对屈曲的影响,以及径向外压力在不同边界条件下对屈曲的影响。 相似文献
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David Bushnell 《International Journal of Solids and Structures》1976,12(1):51-66
The theory is summarized for axisymmetric prebuckling and nonsymmetric bifurcation buckling of ring-stiffened shells of revolution. The analysis is based on finite difference energy minimization in which moderately large meridional rotations, elastic-plastic effects, and primary or secondary creep are included. This theory is implemented in a computer program called BOSOR5, for the analysis of segmented and branched ring-stiffened shells of revolution of multi-material construction.Comparisons between test and theory are given for axisymmetric collapse and nonsymmetric bifurcation buckling of 69 machined ring-stiffened aluminum cylinders submitted to external hydrostatic pressure. Because most of the cylinders fail at an average stress which corresponds to the knee of the stress-strain curve, the analytical predictions are not very sensitive to modeling particulars such as nodal point density or boundary conditions. Agreement between test and theory is improved if the analytical model reflects the fact that the shell and rings intersect over finite axial lenths. 相似文献
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Based on the boundary layer theory for the buckling of thin elastic shells suggested in ref. [14]. the buckling and postbuckling
behavior of clamped circular cylindrical shells under lateral or hydrostatic pressure is studied applying singular perturbation
method by taking deflection as perturbation parameter. The effects of initial geometric imperfection are also considered.
Some numerical results for perfect and imperfect cylindrical shells are given. The analytical results obtained are compared
with some experimental data in detail, which shows that both are rather coincident. 相似文献
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主要研究受轴向冲击圆柱壳非对称屈曲耗能,从轴向屈曲变形、环向屈曲变形和轴向压
缩变形3个角度进行理论推导. 结果表明: 环向屈曲变形能随屈曲折叠边数增加有减小
趋势, 且占总耗能比例很小,可知圆柱壳受轴向冲击屈曲过程中外力做功主要转变为轴向变形
能,环向屈曲变形消耗外力功很少. 相似文献
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In this paper, experimental studies are carried out on the buckling of circular cylindrical thin shells under impact torque. Experiments of impact buckling are made on a Hopkinson torsional bar. The torsional bar gives a step torque on the shells. Through an analysis of the strain-time curve obtained in experiment, the dynamic buckling critical torqueM
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and buckling waves numbern of the shell with different geometric data and some qualitative results are obtained. The buckling behavior of circular cylindrical thin shells under static and impact torque is compared. 相似文献
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本文提出了一种分析环加肋开孔柱壳屈曲问题的混合有限条──有限元法。环加肋柱壳作为一个构造上的正交各向异性壳处理,柱壳非开孔区采用有限条元离散,开孔区采用有限单元离散。在有限条元与有限单元交界面上,根据位移协调条件建立条元和单元的耦合关系,并据此构造一种特殊的过渡单元、联接条元和单元,进行整体分析。算例表明,这一方法对开孔柱壳屈曲问题的分折十分有效。 相似文献