具有非轴对称缺陷双曲冷却塔的动力有限元解

本文针对双曲冷却塔非轴对称缺陷的动力问题,提出了一种解决谐波间耦合问题的近似方法.利用这种方法,本文对具有一般局部几何缺陷双曲冷却塔旋转壳的频率和动力响应进行了分析和计算.     

圆形弹性薄板非轴对称大挠度问题的一个解法

本文建议一个求解圆形弹性薄板非轴对称大挠度问题的方法.本文以周边固定受非轴对称载荷作用下圆形薄板的大挠度问题为例阐述所述方法的原理和解题步骤.文中所述方法可以用以求解其他边界及载荷作用下圆形薄板的非轴对称大挠度问题.     

中心分布压力作用下圆底扁球壳的变形和稳定性*

本文研究圆底扁薄球壳在中心分布压力作用下的轴对称大挠度变形和稳定性.提出了求解圆底扁球壳非线性方程的牛顿-样条函数方法.分别讨论了当几何参数λ固定时,载荷作用半径的变化对壳体失稳的影响,以及当载荷作用半径固定时,几何参数λ的变化对壳体稳定性的影响.分析了临界载荷曲线与屈曲模式之间的关系.并就v=0.3的情形给出了数值分析结果.     

圆形弹性薄反非轴对称大挠度问题一个解法

本建议一个求解圆形弹性薄板非轴对称大挠度的问题方法。本以周边固定受非轴对称载荷作用下圆形薄板的大挠度问题为例阐述所述方法的原理和钥匙步骤，中所述方法可以用以求解其他边界及载荷作用下圆形薄板的非轴对称大挠度问题。     

非均匀弹性地基圆薄板大挠度问题的一般解*

本文在文[1]的基础上提出了一个新的方法可用于求解任意变系数非线性常微分方程组.文中导出了任意轴对称载荷和不同边界条件下的非均匀弹性地基圆薄板大变形的一般解,并给出了收敛于精确解的证明.问题最后可归结为求解一个仅含有三个未知量的非线性代数方程组.该方法和其它方法比较,具有收敛范围大,计算简便迅速等特点.文末给出算例表明内力和位移均可得到满意的结果,验证了本文理论的正确性.     

非保守力作用下杆的塑性动态稳定性

本文用Liapunov第二方法分析非保守力作用下直杆的塑性动态稳定性.杆处于粘性阻尼介质中,并受到切向均布的随动载荷作用.分析中在应力-应变关系中引入了应变率效应.导出了一个稳定性条件,并求出了临界失稳载荷,讨论了应变率效应对杆的稳定性的影响.     

简便积分方程法分析桩

本文用两种方法来分析桩受垂直载荷作用问题.一种是:将由Mindlin集中力组成的轴对称载荷沿弹性半空间z轴的[0,L]内分布,并迭加Boussinesq的解;另一种是:除上述诸虚载荷外,还将Mindlin的垂直集中力沿z轴的[0,L]内分布.前者使边界条件为: 的桩受垂直载荷问题归结为一个Fredholm第一种积分方程;后者使边界条件(其中1,3式同)(0.1)式中的2为:0≤z≤L,U(e,z)=a-e,(e→a);W(a,z)=常数(0.2)的桩受垂直载荷问题归结为两个联立的Fredholm第一种方程式.对刚性桩而言,前者适于容许桩和其侧面附着的土有相对滑动情况;后者适于无相对滑动情形.这两种方法较现有的虚载荷分布于桩表面的诸法具有下列优点:1.所得的积分方程不是二维、奇异的;而是一维、非奇异的.2.能考虑初应力的影响.第一种方法还无须预先假定沉陷函数W;在可压缩桩中容易考虑三维应力的影响的好处.本文还给出Fredholm第一种积分方程近似解误差估计的一个定理,以及两种方法用DJS—21机计算单桩沉陷的结果.     

均布载荷作用下开顶扁球壳的非线性稳定问题

本文利用修正迭代法研究了具有硬中心的开顶扁球壳在均布载荷作用下的轴对称非线性稳定问题,得到了临界载荷的二次近似解析公式.     

径向轴对称冲击载荷下正交异性固支圆板的Liapunov稳定性

本文用Ｌｉａｐｕｎｏｖ第二方法分析了周边受轴对称径向冲击载荷作用的极正交各向异性固支圆板的稳定性．分析是在小挠度和弹性范围内进行的．冲击载荷被假定具有阶梯脉冲形式．导出了相应的稳定性条件．     

耗散双曲Yamabe流的精确解

本文介绍了一种新的几何流, 得到了这种流的一些精确解. 首先得到了初始度量为Einstein的解. 其次得到了具有轴对称的解. 最后, 作为这种流的特殊解, 定义了稳定耗散双曲Yamabe孤子, 而且给出了这种孤子解所满足的方程.     

Computation of worst geometric imperfection profiles of composite cylindrical shell panels by minimizing the non-linear buckling load

In this article the “most unfavorable” shape of initial geometric imperfection profile for laminated cylindrical shell panel is obtained analytically by minimizing the limit point load. The partial differential equations governing the shell stability problem are reduced to a set of non-linear algebraic equations using Galerkin's technique. The non-linear equilibrium path is traced by employing Newton–Raphson method in conjunction with the Riks approach. A double Fourier series is used to represent the initial geometric imperfection profile for the cylindrical shell panel. The optimum values of these Fourier coefficients are determined by minimizing the limit point load using genetic algorithm. The results are determined for simply supported composite cylindrical shell panel. Numerical results show that more number of terms is needed in Fourier series representation to obtain the “worst” geometric imperfection profile which gives lower limit load compared to single term representation of imperfection. We have incorporated constraints on the shape of imperfection to avoid unrealistic limit point loads (due to imperfection shape) as we have assumed that the imperfection is due to machining/manufactuting.     

加肋双曲冷却塔的非线性稳定分析*

本文采用有限元数值分析方法对土木工程中的大型钢筋混凝土双曲冷却塔壳的非线性稳定问题作了具体的数值计算.文中为了讨论双曲塔壳在屈曲后的特性,采用了将普通的载荷增量迭代法与改进的R.C.弧长法相结合的混合算法.为了与实际工程相符合,文中除了将钢筋混凝土当作非均匀体以外,还考虑了塔自重、底部的离散支承、及环向加肋等因素的影响.     

The non-axisymmetric postbuckling behaviour of shallow spherical domes

The non-axisymmetric postbuckling behaviour of an elastic, shallow spherical dome, which is rigidly clamped along its contour and loaded with a uniform transverse pressure, is considered. The solution of the problem is constructed using the Rayleigh-Ritz method based on the Marguerre equations in which the displacements in the circumferential direction are approximated by a Fourier series, and the radial displacements by Bessel functions. The resulting system of non-linear algebraic equations is solved by prolongation methods. It is shown for the first time that a shell has postbuckling, non-axisymmetric equilibrium states with loads which are significantly less than the upper critical load as well as the loads corresponding to bifurcation points. It is suggested that, taking into account the forms of these equilibrium states as the initial inaccuracies of a spherical dome should enable one to model the spread in its experimentally obtained critical loads.     

Imperfection Sensitivity or Insensitivity of Zero-stiffness Postbuckling … that is the Question

Zero-stiffness postbuckling of a structure is characterized by a secondary load-displacement path along which the load remains constant. In sensitivity analysis of the (initial) postbuckling path it is usually considered as a borderline case between imperfection sensitivity and imperfection insensitivity. However, it is unclear whether zero-stiffness postbuckling as such is imperfection sensitive or insensitive. In this paper, Koiter's initial postbuckling analysis is used as a tool for sensitivity analysis. Distinction between two kinds of imperfections is made on the basis of the behavior of the equilibrium path of the imperfect structure. New definitions of imperfection insensitivity of the postbuckling behavior are provided according to the classification of imperfections. A structure with two degrees of freedom with a zero-stiffness postbuckling path is studied, considering four different imperfections. The results from this example show that zero-stiffness postbuckling is a case of transition from imperfection sensitivity to imperfection insensitivity for imperfections of the first kind and that it is imperfection insensitive for imperfections of the second kind. (© 2009 Wiley-VCH Verlag GmbH & Co. KGaA, Weinheim)     

旋转壳局部几何缺陷对其频率和振型的影响

本文在文献[7]的基础上,视旋转壳局部几何缺陷为初始位移,形成了子午向局部几何缺陷的附加刚度阵,然后用结构摄动的方法分析了其几何缺陷对系统自然频率及振型的影响。通过算例可知,子午向局部几何缺陷将引起系统频率升高;缺陷幅度越大,频率升高得也越多。     

On artificial geometry errors in the adaptive analysis of eigenvalues and eigenmodes of curved shell structures using the finite element method

The standard procedure to compute design loads for shell structures as also proposed in design rules is based on the computation of the limit load taking into account the modification of the so-called stability loads due to geometrical imperfections. The imperfections are mostly chosen affine to the buckling patterns, which are solutions of the eigenvalue-problem for the geometrically perfect structure. Thus, the eigenvalue-problems for stability points have to be solved very accurately. In the present contribution an adaptive h -refinement procedure is taken for the solution using low order shell elements. (© 2005 WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim)     

Postbuckling of a shear-deformable anisotropic laminated cylindrical shell under external pressure in thermal environments

A postbuckling analysis is presented for a shear-deformable anisotropic laminated cylindrical shell of finite length subjected to external pressure in thermal environments. The material properties are expressed as linear functions of temperature. The governing equations are based on Reddy’s higher-order shear-deformation shell theory with the von Karman-Donnell-type kinematic nonlinearity. The nonlinear prebuckling deformations and initial geometric imperfections of the shell are both taken into account. The boundary-layer theory of shell buckling, which includes the effects of nonlinear prebuckling deformations, large deflections in the postbuckling region, and the initial geometric imperfections of the shell, is extended to the case of shear-deformable anisotropic laminated cylindrical shells under lateral or hydrostatic pressure in thermal environments. The singular perturbation technique is employed to determine the interactive buckling loads and postbuckling equilibrium paths. The results obtained show that the variation in temperature, layer setting, and the geometric parameters of such shells have a significant influence on their buckling load and postbuckling behavior. Russian translation published in Mekhanika Kompozitnykh Materialov, Vol. 43, No. 6, pp. 789–822, November–December, 2007.     

Korn inequalities for shells with zero Gaussian curvature

We consider shells with zero Gaussian curvature, namely shells with one principal curvature zero and the other one having a constant sign. Our particular interests are shells that are diffeomorphic to a circular cylindrical shell with zero principal longitudinal curvature and positive circumferential curvature, including, for example, cylindrical and conical shells with arbitrary convex cross sections. We prove that the best constant in the first Korn inequality scales like thickness to the power 3/2 for a wide range of boundary conditions at the thin edges of the shell. Our methodology is to prove, for each of the three mutually orthogonal two-dimensional cross-sections of the shell, a “first-and-a-half Korn inequality”—a hybrid between the classical first and second Korn inequalities. These three two-dimensional inequalities assemble into a three-dimensional one, which, in turn, implies the asymptotically sharp first Korn inequality for the shell. This work is a part of mathematically rigorous analysis of extreme sensitivity of the buckling load of axially compressed cylindrical shells to shape imperfections.     

旋转壳的一般轴对称问题及积分方程分析*

本文得到了旋转弹性薄壳在一般荷载下轴对称问题的一种简化形式的复变量方程,该方程准确度在薄壳理论误差范围,并消除了经线极值奇点;给出了问题的Voltera积分方程表述及其数值解.