BUCKLING AND POSTBUCKLING OF STIFFENED CYLINDRICAL SHELLS UNDER AXIAL COMPRESSION

Buckling and postbuckling behaviors of perfect and imperfect, stringer and ortho/ropically stiffened cylindrical shells have been studied under axial compression. Based on the boundary la ver theory for the buckling oj thin elastic shells suggested in ref. [1], a theoretical analysis is presented. The effects of material properties of stiffenefs and skin, which are made of different materials, on the huckling load and postbuckling behavior of stiffened cylindrical shells have also been discussed.

Postbuckling of Imperfect Stiffened Cylindrical Shells Under Combined External Liquid Pressure and Axial Compression

posthuckling analysis is presented for the stilTened cylindrical shell of finite length subjected to combined loading of external liquid pressure and axial compression. The formulations are based on a boundary layer theory of shell buckling, which includes the effects of nonlinear prebuckling deformations, nonlinear large deflections in the postbuckling range and initial geometrical imperfections of the shell. The 'smeared stifl'cner' approach is adopted for the stiffencrs. In the analysis a singular perturbation technique is used (o determine the interactive buckling loads and the postbuckling paths. Numerical examples cover the performance of perfect and imperfect, stringer and ring stiffened cylindrical shells. Typical results arc presented in the dimcnsionless graphical form.

POSTBUCKLING OF IMPERFECT STIFFENED CYLINDRICAL SHELLS UNDER COMBINED EXTERNAL PRESSURE AND HEATING

A postbuckling analysis is presented for a stiffened cylindrical shell of finite length subjected to combined loading of external pressure and a uniform temperature rise. The formulations are based on a boundary layer theory of shell buckling, which includes the effects of nonlinear prebuckling deformations, nonlinear large deflections in the postbuckling range and initial geometrical imperfections of the shell. The 'smeared stiffener' approach is adopted for the stiffeners. The analysis uses a singular perturbation technique to determine the interactive buckling loads and the postbuckling equilibrium paths. Numerical examples cover the performances of perfect and imperfect, stringer and ring stiffened cylindrical shells. Typical results are presented in dimensionless graphical form.

BUCKLING AND POSTBUCKLING OF LAMINATED THIN CYLINDRICAL SHELLS UNDER HYGROTHERMAL ENVIRONMENTS

The influence of hygrothermal effects on the buckling and postbuckling of composite laminated cylindrical shells subjected to axial compression is investigated using a micro-to-macro-mechanical analytical model. The material properties of the composite are affected hy the variation of temperature and moisture, and are hosed on a micromechanical model of a laminate. The governing equations are based on the classical laminated shell theory, and including hygrothermal effects. The nonlinear prebuckling deformations and initial geometric imperfections of the shell were both taken into account. A boundary layer theory of shell buckling was extended to the case of laminated cylindrical shells under hygrothermal environments, and a singular peturbation technique was employed to determine buckling loads and postbuckling equilibrium paths. The numerical illustrations concern the postbuckling behavior of perfect and imperfect, cross-ply laminated cylindrical shells under different sets of environmental conditions. The influences played by temperature rise, the degree of moisture concentration, fiber volume fraction, shell geometric parameter, total number of plies, stacking sequences and initial geometric imperfections are studied.

KOITER-BOUNDARY LAYER SINGULAR PERTURBATION METHOD FOR AXIAL COMPRESSED STIFFENED CYLINDRICAL SHELLS

The double singularities induced by bifurcation point and boundary layer in non-dimensionalized nonlinear boundary-layer Karman-Donnell equations for axially compressed stiffened cylindrical shells can be treated by Koiter-boundary layer singular perturbation method in this paper. It is demonstrated that the method has high computing efficiency and accuracy based on the analysis of AS-2 shell, and some new conclusions can be directly obtained from the perturbation formulas which are very well in agreement with experimental phenomenon of axially compressed stiffened cylindrical shells.

POSTBUCKLING OF PRESSURE-LOADED SHEAR DEFORMABLE LAMINATED CYLINDRICAL PANELS

A postbuckling analysis is presented for a shear deformable laminated cylindrical panel of finite length subjected to lateral pressure. The governing equations are based on Reddy's higher order shear deformation shell theory with von Krmn_Donnell_type of kinematic nonlinearity. The nonlinear prebuckling deformations and initial geometric imperfections of the panel are both taken into account. A boundary layer theory of shell buckling, which includes the effects of nonlinear prebuckling deformations, large deflections in the postbuckling range, and initial geometric imperfections of the shell, is extended to the case of shear deformable laminated cylindrical panels under lateral pressure. A singular perturbation technique is employed to determine the buckling loads and postbuckling equilibrium paths. The numerical illustrations concern the postbuckling response of perfect and imperfect, moderately thick, cross_ply laminated cylindrical panels. The effects played by transverse shear deformation, panel geometric parameters, total number of plies, fiber orientation, and initial geometric imperfections are studied.

矩形大开孔外压薄壁圆柱壳结构稳定性研究

以含矩形大开孔的薄壁圆柱壳结构为研究对象,利用ANSYS Workbench软件对其进行了屈曲分析,研究了不同的几何影响因素和材料参数与其临界失稳载荷和屈曲行为的关系。结果表明:结构的临界失稳载荷主要影响因素为壳体的径厚比;在弹性模量不变的情况下,临界失稳载荷与材料的屈服强度近似为线性关系;径厚比和材料参数的改变并不会改变结构的屈曲行为和趋势。

地下装配式大直径组合筒仓仓壁稳定性分析

【目的】为实现地下装配式大直径组合筒仓的稳定性验算,对装配式组合仓壁进行稳定性分析。【方法】先以有限元分析法验算证明地下仓壁稳定性是可靠的,再对装配式组合仓壁和现浇组合仓壁的稳定性进行分析。【结果】结果表明,装配式组合仓壁的一阶屈曲模态与现浇混凝土仓壁、现浇组合仓壁的一阶屈曲模态均呈现“椭圆形”整体屈曲。当接头抗弯刚度不小于组合仓壁截面抗弯刚度时,装配式组合仓壁的稳定承载力不小于现浇组合仓壁。通过对刚度比-荷载比曲线上的各点进行拟合,得到可用于验算地下装配式组合仓壁整体稳定性的关系式。【结论】本研究为地下粮仓装配式筒仓仓壁的结构设计提供参考。

轴压圆柱钢薄壳稳定设计综述

轴压圆柱薄壳广泛应用于土木工程中的各类钢壳结构,包括筒仓、塔桅、烟囱及容器等。轴压圆柱壳的屈曲问题一直是壳体稳定研究中最为活跃的课题之一。本文全面总结轴压圆柱壳稳定设计方面的研究成果及设计准则。首先简要回顾轴压圆柱壳的弹性经典解及初始缺陷敏感性的经典研究,接着对实际结构中的初始缺陷与制作过程的关系以及焊接残余应力对屈曲强度影响的近期研究进展进行了总结。然后,在简单介绍欧洲钢结构协会规程对轴压圆柱壳稳定设计有关规定的基础上,详细说明了新的欧洲钢壳设计规范所给出的设计准则及相应的研究背景。

加肋圆柱壳在轴压作用下的屈曲和后屈曲

本文讨论完善和非完善的,纵向加肋和正交加肋圆柱壳在轴压作用下的屈曲和后屈曲性态.依据文[1]提供的圆柱薄壳屈曲的边界层理论及其分析方法,给出了加肋圆柱壳在轴压作用下的屈曲和后屈曲理论分析.本文同时讨论肋骨与壳板材料不同时对加肋圆柱壳屈曲和后屈曲性态的影响.

环肋圆柱壳稳定特性与破坏模式的探讨

进一步分析和研究环肋圆柱壳在均匀外压力下稳定性计算公式的适用范围，并讨论了ｍα１与１同级的限制是完全不必要的分析探讨了３种破坏模式与结构参数、屈服极限的关系，从理论上详细说明了环肋圆柱壳在３种外力状态下（仅受轴向均匀外压。

环肋圆柱壳结构壳板稳定性研究

讨论了环肋圆柱壳壳板稳定性解析法与有限元法计算结果的差异,分析了造成差异的原因,给出了对解析法公式的修正方法。

湿热环境中复合材料层合圆柱薄壳的屈曲和后屈曲

在宏_细观力学模型框架下 ,讨论湿热环境对复合材料层合圆柱薄壳在轴向压缩作用下屈曲和后屈曲行为的影响· 基于细观力学模型复合材料性能与湿度和温度变化有关· 壳体控制方程基于经典层合壳理论 ,并包括湿热效应· 壳体屈曲的边界层理论被推广用于湿热环境的情况 ,相应的奇异摄动法用于确定层合圆柱薄壳的屈曲荷载和后屈曲平衡路径· 分析中同时计及壳体非线性前屈曲变形和初始几何缺陷的影响· 数值算例给出完善和非完善正交铺设层合圆柱薄壳在不同湿热环境中的后屈曲行为· 讨论了温度和湿度 ,纤维体积比率 ,壳体几何参数 ,铺层数 。

基于Abaqus的环肋圆柱壳长舱段稳定性分析与结构优化

采用大型非线性有限元软件Abaqus分析了环肋圆柱壳长舱段的稳定性规律,对于环肋圆柱壳长舱段,随着舱段长度的增加,其稳定性的数值仿真解与解析解差别逐渐增大,有限元计算结果能够更加合理准确地反映其稳定性状况。现行规范对于环肋圆柱壳长舱段稳定性的求解适用性有所下降,应该考虑对理论公式进行修正。针对某种典型的环肋圆柱壳长舱段,分别采用一根和两根框架肋骨的方案进行结构优化以提高其总体稳定性,结果表明,一根框架肋骨的优化方案重量较轻,稳定性指标更加接近规范的容许值,两根框架肋骨则比较节省舱内空间。综合考虑,一根框架肋骨的方案更加合理。

正交铺设层合圆柱薄壳在外压作用下的屈曲和后屈曲

依据文献[1,2] 提供的圆柱薄壳屈曲的边界层理论,以挠度为摄动参数,采用奇异摄动方法,给出了完善和非完善、非对称正交铺设层合圆柱薄壳在侧向外压和静水外压作用下的屈曲和后屈曲分析.本文给出了多种复合材料层合圆柱薄壳的计算结果,同时讨论了铺层数对屈曲载荷、后屈曲平衡路径的影响.

加肋斜度对加肋壳稳定性的影响

本文从正交各向异性假设出发，推导了肋骨具有斜度时环加肋圆柱壳总体失稳的临界水压公式，并且用有限元分析软件ＡＬＧＯＲ进行了验证。在公式推导的过程中，考虑了加肋的实际分布情况，并编制了计算程序，对半圆环界面加肋圆柱壳和圆管加肋圆柱壳的临界水压进行了比较。算例表明，在消耗相同材料的情况下，半圆环加肋圆柱壳具有较好的抗水压性能；肋骨斜度增加，临界水压下降。

复合材料层合剪切圆柱曲板在侧压作用下的后屈曲

基于Reddy高阶剪切变形理论的Karmam-Donnell型非线性壳体方程,给出复合材料层合剪切圆柱曲板在侧压作用下的后屈曲分析。将壳体屈曲的边界层理论推广到复合材料层合剪切圆柱曲板受侧压作用的情况。相应的奇异摄动法,用于确定圆柱曲板的屈曲荷载和后屈曲平衡路径。分析中同时考虑非线性前屈曲变形和初始几何缺陷的影响。数值算例给出完善和非完善,中等厚度正交铺设层合圆柱曲板的后屈曲荷载-挠度曲线。讨论了横向剪切变形,曲板几何参数,铺层数,铺展方式和初始几何缺陷等各种参数变化的影响。

带加强圈外压薄壁圆柱壳体稳定性有限元分析

壳体在承受外压的作用时,往往因稳定性不足导致壳体的变形或者压扁,为避免壳体变形,通常在壳体外表面或内表面设置加强圈,以增加壳体的稳定性。采用有限元分析软件ANSYS对有无加强圈的薄壁圆柱壳体进行特征值屈曲分析,探究外加强圈对圆柱壳体的影响。同时针对含有不等高度、不等加强圈厚度以及不等加强圈的间距的薄壁圆柱壳体进行稳定性分析,以便以后能够设计出更加合理的加强圈满足稳定性的要求。

非完善加筋圆柱壳在外压和热荷载共同作用下的后屈曲

基于壳体屈曲的边界层理论，本文给出有限长加筋圆柱壳在侧向外压和均布热荷载共同作用下的后屈曲分析·分析中同时考虑壳体非线性前屈曲变形，大挠度和初始几何缺陷的影响·肋条的处理采用“平均刚度”法·采用奇异摄动方法导得壳体屈曲载荷关系曲线和后屈曲平衡路径，并给出完善和非完善，纵向加筋或环向加筋圆柱壳数值算例·

多平面柱壳水下耐压结构特性研究

由多个三角形或梯形平面在空间上以平面与平面间周期性按一定夹角连接所构成的似圆柱壳结构是一种新的结构形式,简称为多平面柱壳。论文将该新型结构用于水下耐压结构,定义了其基本几何参数,并推导了重量、体积和惯性矩等常用特征表达的计算公式;比较了多平面柱壳、环肋圆柱壳以及一般圆柱壳这三种柱壳结构受均布水压时的稳定性,并着重讨论这几种柱壳结构对几何初始缺陷的屈曲敏感性。计算结果表明,在一定重量/浮力比条件下,多平面柱壳的临界失稳压力优于圆柱壳,而与环肋圆柱壳的相当;并且多平面柱壳对于几何初始缺陷的屈曲敏感性小于环肋圆柱壳和一般圆柱壳等常用结构。