薄壁加筋肋圆柱壳稳定性分析的参数化研究

针对在轴向载荷作用下的正置、正交网格形式的薄壁加筋肋圆柱壳结构，利用有限元程序，对薄壁加筋肋圆柱壳稳定性分析进行了参数化研究，得到了进行结构优化设计的准则，对于给定的设计载荷，当结构参数位于某一个局部失稳与整体失稳的临界区域时，结构的重量最轻。提出了基于有限元分析进行结构优化设计的策略，利用优化策略，获得了一薄壁加筋肋圆柱壳结构的优化设计结果，同时给出了粘合刚度简化模型与有限元计算结果的比较。     

混凝土断裂过程及尺寸效应分析

为研究混凝土裂纹断裂过程和最大承载力计算方法,通过实验机对四种不同尺寸混凝土紧凑拉伸断裂试件进行了加载过程实验,并对其中一个试件进行应变片跟踪测试.由实验结果分析得到了一系列关系曲线,如试件的载荷-加载点位移关系曲线,断裂损伤区变形随载荷变化曲线;并且计算了不同尺寸断裂试件的应力强度因子.结合计算粘聚裂纹应力强度因子的公式与断裂准则,完成了对承载力理论值的计算,并将其与实验峰值平均值进行对比,其结果是两者相比误差较小,表明此种计算裂纹结构最大承载力方法是可行的.     

钢质套筒被动围压下混凝土材料的冲击动态力学性能

为了研究混凝土材料在钢质套筒侧限约束下的动态力学性能参数和破坏规律,采用分离式大直径（75 mm）SHPB实验技术,测试了钢质套筒侧限约束下不同混凝土试件在不同载荷作用下轴向或径向的应力、应变峰值,平均应变率,计算了混凝土材料的损伤值,描述了加载破坏现象,对实验结果进行了分析。结果表明:混凝土材料在被动围压下,延性、抗破坏能力得到加强,具有明显的增强效应。被动围压下SHPB实验中混凝土材料的破坏应变为典型SHPB实验中破坏应变的1.8～2.8倍;破坏应力达到150 MPa以上,为静力学无围压条件下的2～5倍。     

冲击载荷下钨合金圆台试件绝热剪切变形局部化的数值模拟

采用有限元计算编码ABAQUS模拟了钨合金圆台试件在冲击载荷下的变形和剪切局部化行为.计算采用二维轴对称应变条件下的绝热模型.钨合金的本构方程采用热粘塑性形式的Johnson-Cook模型.为了得到不同尺度的变形信息,计算中用了两种网格;先用粗糙网格分析试件变形局部化的概貌;接着,用细密网格(在变形局部化区域,网格尺寸达到10μm)分析绝热剪切带的形成和发展.有限元模拟得到的绝热剪切带位置和方向与实验一致.计算结果表明,绝热剪切带的形成和发展与试件的应力状态密切相关.     

悬臂高梁在静动态载荷作用下侧向失稳的实验研究

本文进行了平头圆柱形弹体对铝合金悬臂高梁自由端正撞击引起侧向失稳的实验研究．通过多种不同尺寸梁的实验，研究了梁在静动态载荷下的侧向失稳临界载荷值及屈曲模态．最后给出一个在撞击载荷下，计算悬臂高梁侧向失稳临界冲击动能值的经验公式．     

集中载荷作用下薄壁开口曲杆的稳定性

本文研究了薄壁开口曲杆的稳定性问题.该曲杆的边界条件比较复杂,一端固支,另一端既有对位移的限制,又有集中力和集中力矩作用.本文从薄壁开口曲杆的平衡方程出发,应用假想分布载荷法,导出一组关于曲杆稳定性的变系数常微分方程.为了解特征值问题,应用有限差分法,将特征方程用矩阵形式表达.对某一产品结构中的实际构件进行了数值计算与稳定性试验,构件为一Ⅰ字形截面的薄壁开口曲杆,对特征方程应用矩阵迭代法求得临界载荷的理论计算值.应用Southwell法结合最小二乘法整理了重复试验所获得的数据,得到临界载荷的实验值,理论计算值与实验值接近.     

基于立体打印自然通风冷却塔模型稳定性试验研究

为研究自然通风冷却塔在风载荷下的屈曲模式及临界风速,用立体打印技术打印了三个不同壁厚的缩尺模型,在风洞中完成了稳定性试验,并将实验结果与有限元计算结果进行对比分析.研究表明,模型失稳发生在弹性阶段,其壁厚与喉部半径之比是确定临界载荷的一个关键参数.实验得到的临界风压值同现有规范的设计相接近,约为有限元计算的1/4,说明我国现有规范中基于冷却塔整体稳定性得到的最小壁厚是偏保守的.     

环壳屈曲的渐近解

本文提出分析圆环壳屈曲的一种渐近解析方法,由Sanders非线性平衡方程和壳中面变形协调方程推导出静水外压下环壳的稳定方程,求出了方程的渐近解,理论计算的临界压力值与Fishlowitz的实验结果符合良好,并研究了屈曲前非线性变形对临界载荷的影响。     

弹性支持扁拱动力稳定性分析和变压器内线圈短路动稳定分析

本文采取脉冲载荷激励下弹支扁拱弹性动力稳定性的理论模型分析电力变压器内线圈短路动稳定问题.首先导出了脉冲载荷激励下弹支扁拱非线性运动积分微分方程级数解,给出了各平衡位置(奇点)的局部稳定(不稳定)性证明,导出弹支扁拱抗跳跃失稳的稳定性充分条件、判别公式和临界载荷;其次导出了短路载荷与脉冲载荷的相当关系,考虑内线圈各线匝(铜条)短路电动力到内线匝的传递,给出了内线圈短路动稳定临界电动力计算公式和动稳定判别方法;最后作出与实验结果的比较和算例.     

考虑轴向均布载荷时压杆的稳定性计算

为了求得压杆同时承受轴向均布载荷和集中载荷时,临界载荷的计算公式,首先对仅承受轴向均布载荷的压杆,用初参数法,导出了临界载荷特征方程,由软件分析特征方程发现, "固支--定向"、"固支--自由"、"铰支--定向"支承的压杆,轴向均布载荷对其稳定性有明显影响,并求得了临界载荷的近似解;其次采用载荷换算与叠加的方法,求得了压杆同时承受轴向均布载荷和集中载荷时,临界载荷计算的经验公式;最后就"固支--自由"支承的压杆,与其他一些研究结果进行了比较,本文结果与"平均结果"较吻合.     

THE COMPUTATIONAL METHOD FOR STABILITY OF TRUSSES WITH SMALL DEFORMATION

基于桁架结构稳定性计算的经典理论,分析了利用特征值理论开展桁架结构屈曲分析的计算方法,以及利用欧拉临界载荷屈曲理论,采取杆件撤除的静力求解确定桁架结构稳定临界载荷的计算方法. 通过理论研究和相关算例分析,论证了利用特征值理论和临界载荷屈曲理论相结合的方法,判断小变形桁架结构的失稳模态,求解桁架结构稳定临界载荷的确定性.     

THE DETERMINATION OF BUCKLING POINT AND CRITICAL LOAD OF COMPRESSIVE MEMBER

为了分析压杆失稳的临界力与失稳后杆件屈服形态的关系,在理论推导和试验研究的基础上,提出了通过捕捉细长压杆失稳时的失稳点来确定压杆临界力的分析方法,通过测量细长压杆失稳时微弯状态下杆端的纵向位移,求得临界压力的大小. 文中将该方法的实验结果与直接用欧拉公式计算的临界压力进行了比较,结果表明,考虑细长压杆微弯状态时杆端的纵向位移所得到的失稳的临界压力值大于利用欧拉公式计算的临界压力值.     

STUDY ON AMPLIFICATION FACTOR OF FLEXURAL BUCKLING CRITICAL LOAD OF AXIAL COMPRESSION BARS1)

为了建立一般条件下轴压构件屈曲临界载荷的计算理论,首先对轴心受压构件发生屈曲时的总势能方程进行了推导,然后采用Rayleigh-Ritz法并基于势能驻值原理得到了4种不同端部约束条件下轴压构件的屈曲临界载荷,对比欧拉临界载荷,给出了临界载荷放大系数 的计算式,全面考虑了构件长细比、压缩变形、剪切变形以及截面形状系数对临界载荷的影响,推导的计算式可用于较小长细比轴压构件发生屈曲时临界载荷的计算.圆截面和双轴对称工字形截面轴压构件屈曲临界载荷的分析表明构件长细比是影响放大系数的主导因素。     

Shape design sensitivity analysis for stability of elastic continuum structures

This paper addresses a method for shape design sensitivity analysis of a buckling load in a continuous elastic body. The sensitivity formula for critical load is analytically derived and expressed in terms of shape variation, based on the continuum formulation of the stability problem. Though the buckling problem is more efficiently solved by structural elements such as a beam and shell, elastic solids have been chosen for the buckling analysis in this paper because solid elements can generally be used for any kind of structure whether it is thick or thin. The initial stress and buckling analysis is carried out by the commercial analysis code ANSYS. Sensitivity is then computed by using the mathematical package MATLAB with the results of ANSYS. Several problems including straight and curved beams under compressive load, ring under pressure load, thin-walled section and bottle shaped column are chosen in order to illustrate the efficiency of the presented method.     

An analytical solution for buckling of moderately thick functionally graded sector and annular sector plates

In this article, an analytical solution for buckling of moderately thick functionally graded (FG) sectorial plates is presented. It is assumed that the material properties of the FG plate vary through the thickness of the plate as a power function. The stability equations are derived according to the Mindlin plate theory. By introducing four new functions, the stability equations are decoupled. The decoupled stability equations are solved analytically for both sector and annular sector plates with two simply supported radial edges. Satisfying the edges conditions along the circular edges of the plate, an eigenvalue problem for finding the critical buckling load is obtained. Solving the eigenvalue problem, the numerical results for the critical buckling load and mode shapes are obtained for both sector and annular sector plates. Finally, the effects of boundary conditions, volume fraction, inner to outer radius ratio (annularity) and plate thickness are studied. The results for critical buckling load of functionally graded sectorial plates are reported for the first time and can be used as benchmark.     

复杂载荷作用下圆柱壳的弹塑性动力屈曲研究

对复杂载荷作用下圆柱壳的弹塑性动力屈曲问题进行了研究。基于Hamilton变分原理导出圆柱壳的运动方程 ,本构关系采用增量理论 ,借助增量数值算法求解动力方程组。结果表明 ,均匀径向外压对圆柱壳的轴向冲击的过程或冲击性态有较大的影响 ,并讨论了径向压力与轴向冲击载荷的幅值对结构临界动力屈曲载荷和临界动力失效载荷的影响。     

Experimental method of determining the uniaxial-compression characteristics of thin-walled structures

An analytical treatment of the stability of thin-walled cylinders demonstrates that this geometry is free from the normally observed buckling instabilities when the external pressure is applied as a ‘winding’ load. Overwrapping vessels with elastomeric fiber under high tension produces an equilibrium state that is identical with simple external pressure. This state differs from the case of constant external pressure in that it is stable and has no buckling instabilities. An analysis is presented that demonstrates this experimentally observed observation and shows that the system will be stable independent of its material properties (i.e., elastic, plastic, viscoelastic, etc.). Consequently, this technique can be used to subject thin-walled cylindrical structures to large enough external pressure to cause fracture or homogeneous yielding. Simple experiments on a metal and polymer sample demonstrate the technique.     

Optimization of cylindrical shells with compliant cores

Thin-walled, cylindrical structures are found extensively in both engineering components and in nature. The weight to load bearing ratio is a critical element of design of such structures in a variety of engineering applications, including space shuttle fuel tanks, aircraft fuselages, and offshore oil platforms. In nature, thin-walled cylindrical structures are often supported by a honeycomb- or foam-like cellular core, as for example, in plant stems, porcupine quills, or hedgehog spines. Previous studies have suggested that a compliant core increases the buckling resistance of a cylindrical shell over that of a hollow cylinder of the same weight. In this paper, we extend the linear-elastic buckling theory by coupling it with basic plasticity theory to provide a more comprehensive analysis of isotropic, cylindrical shells with compliant cores. We examine the optimal design of a thin-walled cylinder with a compliant core, of given radius and specified materials, for a prescribed load bearing capacity in axial compression. The analysis gives the values of the shell thickness, the core thickness, and the core density that maximize the load bearing capacity of the shell with a compliant core over an equivalent weight hollow shell. The analysis also identifies the optimum ratio of the core modulus to the shell modulus and is supported by a Lagrangian optimization technique. The analysis further discusses the selection of materials in the design of a cylinder with a compliant core, identifying the most suitable material combinations. The performance of a cylinder with a compliant core is compared with competing designs (optimized hat-stiffened shell and optimized sandwich-wall shell). Finally, the challenges associated with achieving the optimal design in practice are discussed, and the potential for practical implementation is explored.     

外压对环肋圆柱壳轴向弹塑性动力屈曲的影响

采用增量理论,借助增量数值解法研究了复合加载（轴向流－固冲击载荷＋径向均匀外压）条件下环肋圆柱壳的弹塑性动力屈曲,采用类似B－R准则和Southwell方法来确定临界载荷,讨论了径向均匀外压对结构动力性态及抗轴冲击能力的影响。     

考虑弯扭形变的薄壁箱形梁的非线性后屈曲

在大位移和扭转的前提下,通过一中等弯曲扭转的位移场描述了薄壁箱形梁在偏心载荷作用下的静稳定性问题.该非线性公式可用于分析简支薄壁箱形梁在不同载荷作用下的屈曲和后屈曲行为.采用伽辽金方法将非线性微分系统离散,并通过牛顿-拉普森增量迭代法求解得代数方程组.数值计算结果表明,当前屈曲位移不可忽略时,经典的横向屈曲预测是保守的...