理想弹性压杆临界挠度的确定

本文使用严格的边界条件,对理想弹性压杆的临界力重新定义。采用挠曲线近似微分方程方法和能量法给出了临界力的极限表达形式,解决了细长压杆临界力作用下的挠度不确定问题。     

弹性屈曲大挠度杆纵横变形的计算

弹性屈曲大挠度杆纵横变形的计算刘传芬（兰州铁道学院，兰州７３００７０）两端铰支的弹性屈曲杆纵横变形的计算，根据压杆弹性稳定的大挠度理论，其中点最大挠度δ和两支座间距离Ｄ（见图１）的精确解为￣［１］上述３个公式中，ｐ为轴向载荷，ＥＩ为抗弯刚度；分别为第...     

关于细长压杆稳定问题的注记

关于细长压杆稳定问题的注记陈家骏（常州建筑职工大学常州２１３０１５）细长压杆失稳时挠度无法确定的原因，现有文献都解释为在推导挠度方程的过程中使用的是近似微分方程，即用二阶导数代替了弹性曲线的曲率，使方程线性化的缘故，但所得到的临界压力计算公式却与精确...     

圆截面杆在曲线井中的屈曲问题

本文研究了线弹性的圆截面压杆在刚性井壁的曲线井中的屈曲问题。压杆两端为铰支，杆和井壁之间的摩擦力忽略不计，失稳前假设压杆位于曲线井的较低侧。分析了压杆屈曲时的几何变形条件，导出了压杆的曲率，变形能和各项外力势的表达式，用最小势能原理导出压杆失稳的微分方程和边界条件。引入梁单元，用有限单元法求得了压杆失稳时的临界压力和杆轴线状态。结果显示，临界压力随着压杆自重和曲线井半径的增加而增加。自重为零时，杆轴线为半个正弦曲线；自重不为零时，杆轴线为振荡的曲线，且振荡主要集中在压杆顶部。     

关于细长压杆稳定性问题的讨论

本文在利用挠曲线近似微分方程分析细长压杆稳定性问题时，对传统的边界条件进行了修正，重新解释了以往认为临界挠度无法确定的原因．     

限制失稳模态方程及约束载荷计算

针对受压限制失稳结构,利用点接触、线接触屈曲模型,建立了杆在各种屈曲模态下的挠度曲线方程.通过求解曲线方程,可以得到发生限制失稳结构在各种屈曲模态下,与外部限制失稳构件之间的接触载荷大小,分析了受压结构与限制失稳构件之间的间隙对接触载荷的影响.通过对屈曲模态中各波形的形态进行调整,研究了同一屈曲模态,不同失稳波形下接触载荷的差异.     

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.     

关于屈曲杆最大挠度的近似计算式的讨论

在一般文献中,有关两端铰支等截面细长压杆屈曲后,其最大挠度δ与载荷P 之间的近似关系式 ...     

谈细长压杆稳定性问题

谈细长压杆稳定性问题薛福林（哈尔滨工业大学，哈尔滨１５０００６）为什么在材料力学中细长压杆临界挠度是“不确定值”，为什么用挠曲线近似微分方程能得到临界力的精确解答，笔者愿谈谈自己的看法．不失一般性，本文以图１的压杆为例．首先我们应该明确什么是压杆的临...     

谈细长压杆稳定性问题

谈细长压杆稳定性问题薛福林（哈尔滨工业大学，哈尔滨１５０００６）为什么在材料力学中细长压杆临界挠度是“不确定值”，为什么用挠曲线近似微分方程能得到临界力的精确解答，笔者愿谈谈自己的看法．不失一般性，本文以图１的压杆为例．首先我们应该明确什么是压杆的临...     

地基梁动-静态响应的比较分析

采用分离变量法求得了冲击荷载作用下的开尔文地基上两端自由有限长梁动态挠曲线方程的级数解;分析了地基梁结构参数和冲击荷载作用时间对梁挠曲线特征值（最大挠度和挠曲线面积）的影响规律;比较地基梁动态挠曲线与静荷载引起的地基梁静态挠曲线之间差异,发现：(1)等效地基梁动态最大挠度或挠曲线面积的当量静荷载值与冲量之间不存在良好对应关系;(2)依据地基梁动态挠曲线用静态方法反演得到的地基梁结构参数有可能含有较大的偏差．     

Long-wave in-plane buckling of elastoplastic square honeycombs

In this study, two formulae derived for very long-wave in-plane buckling of elastic square honeycombs are extended and examined in the elastoplastic case. To this end, microscopic buckling and post-buckling behavior of elastoplastic square honeycombs subject to in-plane compression are numerically analyzed using a homogenization theory of the updated Lagrangian type. It is thus demonstrated that very long-wave buckling occurs just after the onset of macroscopic instability if periodic length is sufficiently long, and that plasticity can cause the localization of microscopic buckling accompanied by a significant decrease in macroscopic compressive stress. Then, the very long-wave buckling stresses computed are predicted by incorporating the effect of plasticity in the two formulae of elastic square honeycombs. It is shown that the resulting formulae are successful in predicting the very long-wave buckling stresses in the plastic range as well as in the elastic range.     

简支梁大挠度弹性后屈曲载荷与变形的优化算法

针对简支梁结构大挠度后屈曲载荷与变形的计算问题,本文提出了一种直接求解其后屈曲载荷和变形的优化算法。在简支梁处于大挠度屈曲平衡状态下,将梁结构划分为有限子段,以待求后屈曲载荷为设计变量,根据起点的边界条件和每个子段满足的弯矩变形公式,累积计算出其他各个节点的坐标,以得到的终点坐标满足的边界条件构建目标函数模型。在此基础上,通过MATLAB编制优化程序分析了两个典型算例,并将理论结果与相关软件的计算结果进行对比,从而证明了本文算法的正确性。本文算法求解过程简单、快速,具有一定的实用性,为变截面结构大挠度弹性屈曲稳定性问题的研究提供了参考。     

ANALYSIS ON THE MAGNETO-ELASTIC-PLASTIC BUCKLING/SNAPPING OF CANTILEVER RECTANGULAR FERROMAGNETIC PLATES

An analysis of buckling/snapping and bending behaviors of magneto-elastic-plastic interaction and coupling for cantilever rectangular soft ferromagnetic plates is presented.Based on the expression of magnetic force from the variational principle of ferromagnetic plates,the buckling and bending theory of thin plates,the Mises yield criterion and the increment theory for plastic deformation,we establish a numerical code to quantitatively simulate the behaviors of the nonlinearly multi-fields coupling problems by the finite element method.Along with the phenom- ena of buckling/snapping and bending,or the characteristic curve of deflection versus magnitude of applied magnetic fields being numerically displayed,the critical loads of buckling/snapping, and the influences of plastic deformation and the width of plate on these critical loads,the plastic regions expanding with the magnitude of applied magnetic field,as well as the evolvement of deflection configuration of the plate are numerically obtained in a case study.     

Buckling and post-buckling analysis for magneto-elastic–plastic ferromagnetic beam-plates with unmovable simple supports

This paper presents an analysis of buckling/snapping, bending and post-buckling/snapping behaviors of magneto-elastic–plastic interaction and coupling for soft ferromagnetic beam-plates with geometrically nonlinear deformation and unmovable simple supports at the ends of the plates. Based on the expression of magnetic force from the variational principle of ferromagnetic plates, the theory of thin plates with the nonlinear deformation of van Karman’s type, and the Mises yield criterion and the increment theory for plastic deformation, here, we establish a numerical code to quantitatively simulate the behaviors of the nonlinearly multi-coupling problems by the finite element method. Along with that the phenomena of buckling, bending, and post-buckling/snapping, or the characteristic curve of deflection versus magnitude of applied magnetic fields are numerically displayed, the critical values of buckling/snapping and yield magnetic fields, and the expansibility of plastic region after the plates undergo plastic deformation with increasing of the applied magnetic fields, as well as the evolvement of deflection configuration of the plate are numerically obtained in a case study.     

安全壳中钢衬壳热屈曲问题理论与实验研究（Ⅱ）—实验部分

钢衬壳热屈曲问题是核工程安全壳设计中的主要问题,但实验研究方面的文章发表得不多。文中以２００兆瓦核电站安全壳中钢宙为研究对象,采用局部１：１模型,测得了钢衬壳热屈曲温度和应变载荷,给出了钢衬壳屈曲和初始后屈曲过程中挠度和温度关系。     

黏弹性结构蠕变屈曲特性的分析

分析了线黏弹性正交铺设层合板的蠕变失稳问题，由相空间的特征方程解出临界载荷，经Laplace数值反演得到屈曲载荷与时间的关系；然后，通过建立扰动模型和分析变形的有界与无界增长，讨论了黏弹性结构延迟失稳的特性，解释了临界载荷与失稳时间的具体含义．     

A procedure of the method of reverberation ray matrix for the buckling analysis of a thin multi-span plate

A procedure of the method of reverberation ray matrix(MRRM) is developed to perform the buckling analysis of thin multi-span rectangular plates having internal line supports or stiffeners. A computation algorithm for the reverberation ray matrix in the MRRM is derived to determine the buckling loading. Specifically, the analytical solutions are presented for the buckling of the structure having two opposite simply-supported or clamped-supported edges with spans, while the constraint condition of two remaining edges may be in any combination of free, simply-supported, and clamped boundary conditions. Furthermore, based on the analysis of matrices relating to the unknown coefficients in the solution form for the deflection in terms of buckling modal functions, some recursive equations(REs) for the MRRM are introduced to generate a reduced reverberation ray matrix with unchanged dimension when the number of spans increases, which promotes the computation efficiency. Several numerical examples are given, and the present results are compared with the known solutions to illustrate the validity and accurateness of the MRRM for the buckling analysis.     

Buckling and postbuckling behavior of half-loaded shallow spherical shells

Applying the Galerkin procedure to Marguerre's shallow shell equations, reasonably accurate solutions are obtained for the buckling and postbuckling behavior of clamped shallow spherical shells subjected to external pressure distributed over half the surface.For the geometrical parameter λ smaller than 4.5, the half-loaded shells do not buckle. The buckling loads for 6 ≦ λ ≦ 15 lie about 17–30% below those of uniformly loaded shells. However, the lowest loads after buckling are higher than those for uniformly loading. As λ keeps increasing, the buckling mode shows more and more waves along the circumferential direction. The amplitude of the asymmetrical deflection component Δ₁ becomes remarkably large immediately after buckling. After passing the postbuckling lowest equilibrium point, the sinusoidal deflection disappears and the deflection is changed such that only one location on the shell surface, including the non-loaded area, has been deflected almost symmetrically. The effects of initial imperfections are not so great as for the uniformly loaded case.