悬臂矩形板在对称边界荷载下的屈曲

本文用变分法对悬臂矩形板在对称边界荷载下的稳定性进行研究.我们将对在悬臂矩形板的一对相对的自由边作用有不同的对称边界荷载时,求出薄板的最小临界力.文中分别讨论了有一对集中力,均布荷载,局部均布荷载,三角形分布荷载及一对集中力偶作用之下悬臂矩形板发生屈曲时的最小临界荷载.     

中厚悬臂板的固有振动和稳定

本文由设定两个位移函数，应用最小二乘法和能量法，得到中厚悬臂矩形板固有振动和稳定的Ｒｅｉｓｓｎｅｒ近似解。     

悬臂板侧屈问题的多项式解法

本文研究了悬臂矩形板受均布载荷或集中载荷作用时的侧屈问题.挠度函数选用多项式(2.1)以取代文献[1]中的余弦函数.本文得到的最小临界载荷比文献[1]相应结果更加准确,计算过程也十分简单.     

考虑横向剪切效应的悬臂矩形板的弯曲

本文以Reissner板理论为基础,利用厚板的广义简支边概念及迭加法,求得了考虑横向剪切效应的悬臂矩形板弯曲的精确解.从所得结果来看,这种方法是有效的.     

悬臂矩形板的不对称弯曲

本文用能量法讨论了悬臂矩形板在多种荷载作用下的不对称弯曲问题。文中举了若干算例,诸如在板的自由边及角点上作用有不对称的集中力或集中力偶和在自由边上作用有不对称的,均匀的或非均匀的分布荷载等。     

矩形板的侧屈

本文研究矩形板的侧向屈曲问题.文中分别讨论了有集中力,均布荷载及集中力偶作用之下矩形板发生侧向屈曲时的最小临界荷载.文中使用了能量法.     

边界条件对板壳稳定性的影响

本文论述了边界条件对板壳稳定性影响的理论和实际意义;介绍了近年来我们在理论和实验两方面的研究结果;指出了本研究对工程的指导作用,并将研究划分为两个阶段。     

矩形板大挠度问题的样条函数解

本文以中心挠度为摄动参数,将矩形板大挠度问题的非线性偏微分方程缉转化为几个线性的偏微分方程组,然后分别用样条有限点法和样条有限元法求解,得到了在多种边界条件下具有任意长宽比的,受均布荷载的矩形板的解答,给出了板中面的位移、挠度的解析表达式;并编制了相关的计算机程序.计算的结果与现有的其他理论的结果作了比较,表明本文的结果是良好的.     

关于TRUNC板元收敛性的注记

1.引言 自从Bergan,Argyris等提出并发展了一种称之为TRUNC三角形元的非常规板元以来,在工程界得到了广泛的应用,也在数值分析方面引起了很大的兴趣。实际计算表明,它克服了Zienkiewicz元的三平行方向剖分的限制,而且简化了刚度矩阵的形成,因此,工程界很重视。不久前石钟慈对这种板元进行了细致的数学分析,给出了很     

十二参三角形板元

九参三角形板元的研究工作已有不少,但十二参三角形板元还较少见报道。唐立民等利用他们创立的拟协调方法构造一个十二参三角形拟协调元,节点参数是单元三个顶点上的函数值和两个一阶偏导数值及三边中点上的外法向导数值,他们是用力学方法构     

An explicit solution of the large deformation of a cantilever beam under point load at the free tip

The large deformation of a cantilever beam under point load at the free tip is investigated by an analytic method, namely the homotopy analysis method (HAM). The explicit analytic formulas for the rotation angle at the free tip are given, which provide a convenient and straightforward approach to calculate the vertical and horizontal displacements of a cantilever beam with large deformation. These explicit formulas are valid for most practical problems, thus providing a useful reference for engineering applications. The corresponding Mathematica code is given in the Appendix.     

Analytical solution for large deflections of a cantilever beam under nonconservative load based on homotopy analysis method

In this article, large deflection and rotation of a nonlinear beam subjected to a coplanar follower static loading is studied. It is assumed that the angle of inclination of the force with respect to the deformed axis of the beam remains unchanged during deformation. The governing equation of this problem is solved analytically for the first time using a new kind of analytic technique for nonlinear problems, namely, the homotopy analysis method (HAM). The present solution can be used in wide range of load and length for beams under large deformations. The results obtained from HAM are compared with those results obtained by fourth order Range Kutta method. Finally, the load‐displacement characteristics of a uniform cantilever under a follower force normal to the deformed beam axis are presented. © 2009 Wiley Periodicals, Inc. Numer Methods Partial Differential Eq 27:541–553, 2011     

Large deflections of a cantilever beam under an inclined end load

Large deflections of a cantilever beam subjected to a tip-concentrated load whose inclination to the deformed axis of the beam is assumed as constant. The mathematical formulation yields a non-linear two-point boundary value problem amenable to numerical integration. A relation is obtained between the load and the tip-angle of the beam when the tip-concentrated load is normal to the deformed axis of the beam. Many possible loads are found for a specified tip-angle. For the specified load, the tip-angle is found to be unique. However, there is a change in the deformation pattern of the beam having a specified tip-angle with the corresponding multiple loads. This confirms the uniqueness of the solution for the governing non-linear differential equations of a cantilever beam under a tip-concentrated load whose inclination is normal to its deformed axis.     

Optimal layout of cantilever trusses

For given allowable stress, Michell (Ref. 1) has investigated the optimal design of a cantilever truss that is to transmit a given load to two given fixed points of support. Disregarding the weight of the connections between the bars, he found that the truss of minimum weight is a truss-like continuum with an infinity of joints, and with bars that are mostly of infinitesimal length. In the present paper, a finite number of joints is enforced by including in the structural weight, which is to be minimized, not only the weight of the bars but also the weight of their connections, which is assumed to be proportional to the number of joints. The concept of two adjoint trusses is introduced, each of which coincides with the Maxwell diagram of the other truss. Two adjoint trusses have the same weight, and an optimal truss is therefore self-adjoint. The optimal configurations of 6-joint and 11-joint cantilever trusses are discussed, and the range of the weight of the typical joint is determined for which the 6-joint truss is optimal.     

On the theory of the flexural vibrations of a rotating viscoelastic cantilever

A new solution is worked out for the problem of the flexural vibrations of a viscoelastic cantilever. The method is based on the use of Laplace contour integrals for integration in a complex domain. The dependence of the solutions of the problem on the parameters introduced is investigated. Asymptotic expansions of the integrals at large and small values of the argument are constructed for numerical calculations. Solutions in the form of polynomials are found for particular values of the elastic vibration frequencies and the properties of these solutions are established.Institute of Mechanics, Academy of Sciences of the Ukrainian SSR, Kiev. Translated from Mekhanika Polimerov, No. 2, pp. 305–311, March–April, 1973.     

Analysis and modeling of a flexible rectangular cantilever plate

Flexible plate structures with large deflection and rotation are commonly used structures in engineering. How to analyze and solve the cantilever plate with large deflection and rotation is still an unsolved problem. In this paper, a general nonlinear flexible rectangular cantilever plate considering large deflection and rotation angle is modeled, solved and analyzed. Hamilton's principle is applied to obtain the nonlinear differential dynamic equations and boundary conditions by introducing a coordinate transformation between the Cartesian coordinate system and the deformed local coordinate system. Stress function relating to in-plane force resultants and shear forces is given for the first time for complex coupling equations caused by coordinate transformation. The nonlinear equations and the solving method are validated by experiments. Then, harmonic balance method is adopted to get the nonlinear frequency-response curves, which shows strong hardening spring characteristic of this system. Runge–Kutta methods are used to reveal complex nonlinear behaviors such as 5 super-harmonic resonance, bifurcations and chaos for general nonlinear flexible rectangular cantilever plate.     

Predicting nonlinear dynamic response of internal cantilever beam system on a steadily rotating ring

This paper is focused on nonlinear dynamic response of internal cantilever beam system on a steadily rotating ring via a nonlinear dynamic model. The analytical approximate solutions to the oscillation motion are obtained by combining Newton linearization with Galerkin's method. Numerical solutions could be obtained by using the shooting method on the exact governing equation. Compared with numerical solutions, the approximate analytical solutions here show excellent accuracy and rapid convergence. Two different kinds of oscillating internal cantilever beam system on a steadily rotating ring are investigated by using the analytical approximate solutions. These include symmetric vibration through three equilibrium points, and asymmetric vibration through the only trivial equilibrium point. The effects of geometric and physical parameters on dynamic response are useful and can be easily applied to design practical engineering structures. In particular, the ring angular velocity plays a significant role on the period and periodic solution of the beam oscillation. In conclusion, the analytical approximate solutions presented here are sufficiently precise for a wide range of oscillation amplitudes.     

On new analytic free vibration solutions of rectangular thin cantilever plates in the symplectic space

In this paper, we obtain accurate analytic free vibration solutions of rectangular thin cantilever plates by using an up-to-date rational superposition method in the symplectic space. To the authors’ knowledge, these solutions were not available in the literature due to the difficulty in handling the complex mathematical model. The Hamiltonian system-based governing equation is first constructed. The eigenvalue problems of two fundamental vibration problems are formed for a cantilever plate. By symplectic expansion, the fundamental solutions are obtained. Superposition of these solutions are equal to that of the cantilever plate, which yields the analytic frequency equation. The mode shapes are then readily obtained. The developed method yields the benchmark analytic solutions with fast convergence and satisfactory accuracy by rigorous derivation, without assuming any trial solutions; thus, it is regarded as rational, and its applicability to more boundary value problems of partial differential equations represented by plates’ vibration, bending and buckling may be expected.     

Various methods of determining the natural frequencies and damping of composite cantilever plates. 1. Exact solution for the binomial model of deformation

On the basis of the classical theory of thin anisotropic laminated plates the article analyzes the free vibrations of rectangular cantilever plates made of fibrous composites. The application of Kantorovich's method for the binomial representation of the shape of the elastic surface of a plate yielded for two unknown functions a system of two connected differential equations and the corresponding boundary conditions at the place of constraint and at the free edge. The exact solution for the frequencies and forms of the free vibrations was found with the use of Laplace transformation with respect to the space variable. The magnitudes of several first dimensionless frequencies of the bending and torsional vibrations of the plate were calculated for a wide range of change of two dimensionless complexes, with the dimensions of the plate and the anisotropy of the elastic properties of the material taken into account. The article shows that with torsional vibrations the warping constraint at the fixed end explains the apparent dependence of the shear modulus of the composite on the length of the specimen that had been discovered earlier on in experiments with a torsional pendulum. It examines the interaction and transformation of the second bending mode and of the first torsional mode of the vibrations. It analyzes the asymptotics of the dimensionless frequencies when the length of the plate is increased, and it shows that taking into account the bending-torsion interaction in strongly anisotropic materials type unidirectional carbon reinforced plastic can reduce substantially the frequencies of the bending vibrations but has no effect (within the framework of the binomial model) on the frequencies of the torsional vibrations.Institute of Engineering Science Russian Academy of Sciences, St. Petersburg, Russia. St. Petersburg State University, Russia. Translated from Mekhanika Kompozitnykh Materialov, Vol. 32, No. 6, pp. 759–769, November–December, 1996.     

Bending of a nonlinear orthotropic cantilever beam

The method of elastic solutions is employed to investigate the plane problem of the deformation of a cantilever beam of orthotropic glass-reinforced plastic under a concentrated load with allowance for the non-linear properties of the material. The first approximation of the stress function is given and the stress distribution over the cross section is calculated for a specific GRP.Mekhanika Polimerov, Vol. 2, No. 5, pp. 773–778, 1966