ANALYSIS OF THE LARGE DEFLECTION DYNAMIC PLASTIC RESPONSE OF SIMPLY-SUPPORTED CIRCULAR PLATES BY THE“MEMBRANE FACTOR METHOD”

Based on energy equilibrium,a new procedure called the Membrane Factor Method is devel- oped to analyze the dynamic plastic response of plates with deflections in the range where both bending mo- ments and membrane forces are important.The final deflection of a simply -supported circular rigid-plastic plate loaded by a uniformly distributed impulse is obtained.In comparison with other approximate solutions, the present results are found to be simpler and in better agreement with the corresponding experimental values reoorded by Florence.

Buckling and large deflection behaviors of radially functionally graded ring-stiffened circular plates with various boundary conditions

The buckling and large deflection behaviors of axis-symmetric radially functionally graded （RFG） ring-stiffened circular plates are investigated by the dynamic relaxation （DR） method combined with the finite difference discretization technique. The material properties of the constituent components of the RFG plate are assumed to vary continuously according to the Mori-Tanalka distribution along the radial direction. The nonlinear governing equations are obtained in the incremental form based on the firstorder shear deformation plate theory （FSDT） and the von Karman relations for large deflection. In the buckling analysis, an external in-plane load is applied to the plate in- crementally so that, in each load-step, the incremental form of the governing equations can be solved by a numerical code prepared based on the DR method. After converging the DR code in the first increment, the latter load-step is added to the previous one, and the program is repeated again. The critical buckling load is determined from the compressive load-displacement curve obtained by solving the incremental form of the governing equations. Based on the present incremental form of formulation, a bending analysis can also be conducted if the whole load is applied simultaneously. Finally, a detailed parametric study is carried out to investigate the influences of various boundary conditions, grading indices, thickness-to-radius ratios, stiffener＇s positions and depths on the critical buckling load, and displacements and stresses resulted from the bending analysis. It is observed that the effect of the stiffener on the results is much greater in the functionally graded plate with higher material grading indices. The results also reveal that, by increasing the depth of the stiffer, the values of ascending the critical buckling load are approximately identical for both simply supported and clamped boundary conditions.

ON THE METHOD OF ORTHOGONALITY CONDITIONS FOR SOLVING THE PROBLEM OF LARGE DEFLECTION OF CIRCULAR PLATE

In this paper, we reexamine the method of successive approximation presented by Prof. Chien Wei-zangfor solving the problem of large deflection of a circular plate, and find that the method could be regarded as the method of strained parameters in the singular perturbation theory. In terms of the parameter representing the ratio of the center deflection to the thickness of the plate, we make the asymptotic expansions of the deflection, membrane stress and the parameter of load as in Ref. [1], and then give the orthogonality conditions (i.e. the solvability conditions) for the resulting equations, by which the stiffness characteristics of the plate could be determined. It is pointed out that with the solutions for the small deflection problem of the circular plate and the orthogonality conditions, we can derive the third order approximate relations between the parameter of load and the center deflection and the first-term approximation of membrane stresses at the center and edge of the plate without solving the differential equations. For some special cases (i.e. under uniform load, under compound toad, with different boundary conditiors), we deduce the specific expressions and obtain the results in agreement with the previous ones given by Chien Wei-zang, Yeh kai-yuan and Hwang Chien in Refs. [1 - 4J.

APPLICATION OF THE MODIFIED METHOD OF MULTIPLE SCALES TO THE BENDING PROBLEMS FOR CIRCULAR THIN PLATE AT VERY LARGE DEFLECTION ANDTHE ASYMPTOTICS OF SOLUTIONS (Ⅰ)

In this paper, the modified method of multiple scales is applied to study the bending problems for circular thin plate with large deflection under the hinged and simply supported edge conditions. Theseries solutions are constructed, the boundary layer effects are analysed and their asymptotics are proved.

ITERATIVE METHOD FOR LARGE DEFLECTION NONLINEAR PROBLEM OF LAMINATED COMPOSITE SHALLOW SHELLS AND PLATES

Based on the results by Wang,in this paper, the iterative method is presented for the study of large deflection nonlinear problem of laminated composite shallow shells and plates. The rectangular laminated composite shallow shells have been analyzed. The results have been compared with the small deflection linear analytical solution and finite element nonlinear solution. The results proved that the solution coincide with small deflection linear analytical solution in the condition of the low loads and finite element nonlinear solution in the condition of the high loads.

LARGE DEFLECTION PROBLEM OF A CLAMPED ELLIPTICAL PLATE SUBJECTED TO UNIFORM PRESSURE

In this paper, the perturbation solution of large deflection problem of clampedelliptical plate subjected to uniform pressure is given on the basis of the perturbationsolution of large deflection problem of similar clamped circular plate (1948)[1], (1954)[2]. The analytical solution of this problem was obtained in 1957. However, due to social difficulties, these results have never been published. Nash and Cooley (1959)[3] published a brief note of similar nature, in which only the case λ=a/b=2 is given. In this paper, the analytical solution is given in detail up to the 2nd approximation. The numerical solutions are given for various Poisson ratios v =0.25, 0.30, 0.35 and for various eccentricities λ= 1, 2, 3, 4, 5, which can be used in the calculation of engineering designs.

LARGE DEFLECTION PROBLEM OF THIN ORTHOTROPIC CIRCULAR PLATE ON ELASTIC FOUNDATION WITH VARIABLE THICKNESS UNDER UNIFORM PRESSURE

Basic equations for large deflection theory of thin orthotropic circular plate on elastic foundation with variable thickness under uniform pressure are derived in this paper. The second opproximation solutions are obtained by means of the modified iteration method. The relation curves of the nondimensional loading and foe deflection, as to the differential ε and μrθ and λ are shown in Figs. 2, 3, 4. In special circumstance, the results are in accordance with those in [1], [6].

Axisymmetrical Nonlinear Bending and Buckling of a Circular Plate Under Large Load

With the terms of the exact series solution taken as trial functions, the method of point collocation was used to calculate the large deflection of a circular plate. The axisymmetrical bending formulae were developed for the calculation of a circular plate subjected to polynomial distributed loads, a concentrated load at the center, uniform radial forces and moments along the edge or their combinations. The support may be elastic. The buckling load was calculated. Under action of uniformly distributed load, central load or their compound load, solutions were compared with those obtained by other methods. Buckling beyond critical thrust was compared with that calculated by the power series method. The method presented in this paper has advantages of wide convergent range, high precision and short computing time. Moreover, the computing time is nearly independent of the complexity of the loads.

Further Investigation for Nonlinear Free Vibration of Elastic Circular Plate with Large Amplitude

The nonlinear free vibrations of the elastic circular thin plate with large amplitude taking radial force of inertia into account are investigated by using method similar to modified iterative method.The algorithm and formulas finding its approximate analytical solution are provided,and the solution behaviors are also discussed through the calculating example.

CUBLIC SPLINE SOLUTIONS OF AXISYMMETRICALNONLINEAR BENDING AND BUCKLING OFCIRCULAR SANDWICH PLATES

Cubic B-spline taken as trial function, the nonlinear bending of a circular sandwich plate was calculated by the method of point collocation. The support could be elastic. A sandwich plate was assumed to be Reissner model. The formulae were developed for the calculation of a circular sandwich plate subjected to polynomial distributed loads, uniformly distributed moments, radial pressure or radial prestress along the edge and their combination. Buckling load was calculated for the first time by nonlinear theory. Under action of uniformly distributed loads, results were compared with that obtained by the power series method. Excellences of the program written by the spline collocation method are wide convergent range, high precision and universal.

微流体装置力源机构的优化设计

为解决微流控系统中流体介质贮存装置输出压力不稳定等问题,设计了一种柔顺机构作为装置的力源机构。该柔顺机构基于正负刚度叠加理论设计,由四根固定导向梁和两根平面弹簧组成。首先,利用链式梁约束模型和广义打靶法分别求解出固定导向梁和平面弹簧的位移-载荷特性,建立优化模型,得到了满足设计要求的最优解。然后,为验证计算模型的准确性,使用ANSYS对柔顺梁进行大变形分析,结果显示该计算模型和有限元分析相比,误差小于1%。最后,通过实验发现该柔顺机构输出力的实验值和理论设计值存在误差,经过分析发现是加工精度、材料弹性模量误差以及只考虑了中性轴的变形等原因所导致的。

关于开孔薄板大挠度问题的一般数学理论(续)

本文讨论了作用在开孔薄板的各孔边上的外力自身不平衡吋的大挠度问题的应力函数的多值性,并给出了这种问题的一般数学模型,因此本文可以看成是[1]的继续和深入。

夹层圆板轴对称非线性弯曲和屈曲的样条函数解法

以三次B样条函数为试函数,用配点法计算夹层圆板的非线性弯曲· 支座可以是弹性的· 夹层板采用Reissner模型· 荷载可为多项式型的分布荷载、均布边缘力矩、均布径向压力或均布径向预应力及它们的组合· 首次用非线性理论计算了夹层圆板的压曲临界荷载· 在均布荷载作用下的结果同幂级数解的结果作了比较,说明样条配点法具有收敛范围大、精度高。

带旋转自由度C^0类任意四边形板(壳)单元

基于 Reissner- Mindilin板弯曲理论和 Von- Karman大挠度理论 ,采用单元域内和边界位移插值一致性的概念 ,将四节点等参弯曲板单元与 Allman膜变形二次插值模式相结合 ,对层合板壳的大挠度分析提供了一种实用的带旋转自由度的四节点 C0 类板壳单元。大量算例表明 :该单元对板壳结构的线性强度、稳定性和后屈曲分析都表现出良好的收敛性和足够的工程精度。

冲击载荷作用下大挠度圆板的弹塑性动力分析

本文利用已知弹性解分析阶跃载荷作用下大挠度回板的弹塑性动力响应，提出了本征函数法。这是对文献［３，４］的进一步发展。此外在文献［３，４］中，解决大挠度问题时，采用基于卡门方程的混合法，但在本文中，采用了位移法，它在进行分析计算时更为有利。

STACER伸展变形的一种计算方法

STACER是一种航天器上广泛应用的伸展机构,其储能部件由薄壁钢带经冷加工涡卷最终成型为螺旋管状.由于伸展长度可达装载高度的几十倍,钢带在展开过程中呈现为大挠度、大应变形变,机构伸展力的计算必然涉及强非线性问题;同时,钢带的构型、边界条件在伸展过程中不断变化,这些因素又增加了问题的难度,致使常用的商业软件已无法直接处理此类问题.此研究工作应用变分方法的思想,以研究钢带变形的几何特性为基础,构造出钢带构型恰当的可能函数空间,并利用形状函数随伸展长度的变化规律求出钢带的主应变以及变形能,再利用势能极小原理,确定出钢带的真实构型以及相应的变形能,最终利用变形能和虚功原理得出伸展力.这一方法既可以简化计算又可以得到钢带形状函数、伸展力的近似解析式,为伸展力影响因素的定量分析提供了条件.

用“膜力因子法”分析简支刚塑性圆板的大挠度动力响应

在板的变形过程中,当其挠度与厚度同量级时,膜力的作用与弯矩的作用同样重要;当其挠度超过厚度甚至接近板的面内尺寸的量级时,相对于弯矩的作用,膜力的作用是更主要的。本文发展了一种基于能量平衡的简便的“膜力因子法”,有效地解决了当板的挠度达到厚度量级时弯矩和膜力联合作用问题;用这种方法并结合塑性膜阶段的分析成功地求解了简支刚塑性圆板在冲击载荷作用下的大挠度塑性响应问题。所得结果与Florence实验结果符合良好,比已有理论近似结果有所改进。

正多边形板的塑性动力响应——小挠度分析和大挠度分析

本文基于刚性板块的总体平衡,建立运动方程,首次完整地分析了正多边形板的塑性动力响应,得到了周边简支或固支的正多边形板在均布矩形脉冲作用下的塑性动力响应小挠度解析解,并用膜力因子法作了大挠度理论分析。所得的结果包含了作为特例的正方形板、圆板等情形,具有广泛应用价值,同时具有理论上和数学上的意义。

轴对称荷载作用下环形薄板大挠度样条函数解法

环形薄板的大挠度计算因为边界条件复杂,仅有少数特殊情形的数值解答.这些解均是利用摄动法以某点挠度为摄动参数得到的结果.当这点挠度较大或为零,将出现难以解决的困难.作者以三次B样条函数为试函数,用配点法计算环形薄板的大挠度.荷载可为均布荷载、边缘均布线荷载、边缘均布力矩及它们的组合.在所有的算例中均取得了收敛的数值结果.在均布荷载、边缘均布线荷载、边缘均布力矩作用下的计算结果同摄动法的计算结果作了比较,结果表明,样条函数的方法收敛范围大、精度高和计算时间少.

应变硬化薄板夹持型滚弯成形过程分析

现存文献对薄板的连续滚弯成形过程的数学模拟多限于讨论三辊轮角锥型弯板过程,且基于较多的假定和板的小变形情况。而开发有更多的功能和更高的生产效率的四辊轮连续弯板机需研究夹持型滚弯成形过程。本文将[1]的工作,理想塑性材料平面应变薄板的夹持型连续滚弯成形过程的弹塑性大变形弯曲的力学分析,推广至一般应变硬化材料的情形。得出了控制微分方程的解析解。采用固支边界条件模拟刚度很大的夹持系统对板的夹持。通过对线性硬化薄板的数值计算,获得了将板连续滚弯成形为预期曲率的生产过程所需的几何和物理数据,并研究了材料的应变硬化性能对成形过程的影响。