Winkler地基上四边自由正交各向异性矩形薄板弯曲问题的辛叠加解

研究Winkler地基上正交各向异性矩形薄板弯曲方程所对应的Hamilton正则方程, 计算出其对边滑支条件下相应Hamilton算子的本征值和本征函数系, 证明该本征函数系的辛正交性以及在Cauchy主值意义下的完备性, 进而给出对边滑支边界条件下Hamilton正则方程的通解, 之后利用辛叠加方法求出Winkler地基上四边自由正交各向异性矩形薄板弯曲问题的解析解. 最后通过两个具体算例验证了所得解析解的正确性.     

各向异性矩形薄板弯曲问题的一般解

给出了各向异性矩形薄板弯曲问题微分方程的一般解。可以求解任意载荷作用下各种边界的弯曲问题。以四边固支的正方形板为例进行了数值计算。     

相邻两边固支其余两边自由矩形正交各向异性薄板弯曲的辛叠加解

应用辛叠加方法,求出相邻两边固支其余两边自由矩形正交各向异性薄板在均匀荷载下弯曲问题的解析解。先将原方程转换成Hamilton正则方程;用辛方法计算出一边滑支对边简支条件下对应Hamilton算子的辛本征值和辛本征函数系,证明该辛本征函数系的辛正交性,进而在Cauchy主值意义下证明了它的完备性;根据辛本征函数系的完备性,得到了对应Hamilton正则方程的通解,再应用叠加方法计算出原弯曲问题的解析解;最后通过两个具体矩形薄板的数值算例,验证了所得辛叠加解的正确性。     

基于等效系统假定的变厚度板弯曲广义积分变换解

针对等厚度薄板的弯曲问题,研究人员已给出了基于不同数值算法的经典数值解。针对变厚度薄板弯曲问题的解答较少,且以有限元数值模拟计算为主,计算耗时较大。本文基于广义积分变换原理建立了求解变厚度等效系统的广义积分变换算法,分析了线性和二次变化的变厚度板在多种边界条件下的弯曲问题,利用文献已发表结果同本文建立的广义积分变换解进行验证。计算结果表明,本文建立的基于广义积分变换的变厚度板弯曲求解方法具有较高准确性。同时,通过参数化分析手段,分别利用广义积分变换方法和有限元数值模拟方法讨论了不同边界约束和长宽比等条件对中心点处挠度的影响,计算结果具有较好的一致性,证明本文建立的广义积分变换方法可用于求解变厚度板弯曲问题,且具有较高的准确性。     

弹性半空间地基上正交异性矩形板弯曲通解

本文先对受任意边界约束的正交各向异性矩形薄板,在各种形式荷载作用下的弯曲问题,构造了四次逐项可导的带有补充项的双重正弦傅里叶级数新通解.该解析解既不需要叠加,对不同的物性参数又不需要分类,而且待定系数少又具有明确的物理含义,这使得正交各向异性矩形薄板的弯曲问题求解统一化、简单化、规律化.然后将新通解与弹性半空间受任意竖向荷载作用下的静力位移积分变换解相结合,得出弹性半空间地基上受任意边界约束的正交各向异性矩形板,在任意竖向荷载作用下的弯曲解析解.本文还给出了算例分析,其结果与文献吻合良好,证明本文的方法是切实可行的.     

横观各向同性弹性半空间地基上四边自由各向异性矩形薄板弯曲解析解

选用更具广泛性的横观各向同性弹性半空间地基模型,来分析四边自由各向异性矩形地基板的弯曲解析解．将异性薄板的弯曲控制方程,与基于横观各向同性弹性半空间地基位移解建立的板与地基变形协调方程相结合,先按对称性分解,然后用三角级数法,得出横观各向同性弹性半空间地基上四边自由各向异性矩形薄板的弯曲解析解,包括地基反力、板的挠度及内力的解析表达式．该解析解克服了数值法的弊端,取消了对地基反力的假设,板的内力及地基反力求解更切实际．算例结果与文献结果吻合良好,证明本文方法的可行性．     

层状横观各向同性地基上异性矩形薄板的弯曲解析解

选用更具广泛性的层状横观各向同性弹性地基模型,来分析四边自由各向异性矩形地基板的弯曲解析解。先基于直角坐标下横观各向同性体的静力胡海昌通解,借助双重傅里叶变换及矩阵传递法,获得层状横观各向同性地基的静力位移场和应力场;然后将异性薄板的弯曲控制方程,与基于层状横观各向同性弹性地基的位移解建立的板与地基变形协调方程相结合,先按对称性分解,再用三角级数法,得出层状横观各向同性弹性地基上四边自由各向异性矩形薄板的弯曲解析解,包括地基反力、板的挠度及板的内力的解析表达式。克服了数值法的弊端,取消了对地基反力的假设,且避免了矩阵指数函数的计算;同时考虑了地基的层状性及板和地基的各向异性,从而得到板的内力及地基反力更切实际的分布规律。算例结果与文献的有限元结果吻合良好,证明本文方法是切实可行的。     

非均匀圆柱型正交各向异性圆板的弯曲

研究了非均匀圆柱型正交各向异性圆板在均布横向载荷作用下的弯曲问题，求得了折算刚度随半径按指数规律变化的非均匀圆柱型正交各向异性圆板弯曲问题的渐近解，给出了周边固支和简支条件下的渐近解．通过算例可以看出，这种非均匀性对圆板中心挠度的影响是显著的     

层状横观各向同性地基上异性矩形薄板的弯曲解析解

选用更具广泛性的层状横观各向同性弹性地基模型,来分析四边自由各向异性矩形地基板的弯曲解析解。先基于直角坐标下横观各向同性体的静力胡海昌通解,借助双重傅里叶变换及矩阵传递法,获得层状横观各向同性地基的静力位移场和应力场;然后将异性薄板的弯曲控制方程,与基于层状横观各向同性弹性地基的位移解建立的板与地基变形协调方程相结合,先按对称性分解,再用三角级数法,得出层状横观各向同性弹性地基上四边自由各向异性矩形薄板的弯曲解析解,包括地基反力、板的挠度及板的内力的解析表达式。克服了数值法的弊端,取消了对地基反力的假设,且避免了矩阵指数函数的计算;同时考虑了地基的层状性及板和地基的各向异性,从而得到板的内力及地基反力更切实际的分布规律。算例结果与文献的有限元结果吻合良好,证明本文方法是切实可行的。     

各向异性板结构横向弯曲一般解析解

提出了一种求解四阶线性椭圆型偏微分方程黑社会问题的新方法：复级数展开法，产散于求解各向异性板横向弯曲问题，运用得级数展开法首次给出承受任意载荷具有任意边界的各向异性矩形、圆形板横向弯曲一般解析解，同时对各向异性板对称性进行了探讨，指出当板边界约束、载荷呈中心对称时，矩性板挠度呈中心对称，文中亦给出一些数值算例。     

Exact solution of problem of deflection of an anisotropic plate with an aperture

The exact solution of the problem of the deflection of an anisotropic plate weakened by an aperture is known only for the case in which the aperture has the shape of a circle or an ellipse [1, 2]. An exact solution has not been derived for any other aperture shapes. Approximate methods [3–6] which are widespread for the case of multiply connected anisotropic plates [7] are applied to the determination of the bending moments in an anisotropic plate near an aperture differing little from an elliptical or circular one.Translated from Zhurnal Prikladnoi Mekhaniki i Tekhnicheskoi Fiziki, No. 5, pp. 168–177, September–October, 1977.     

复变形式的各向异性板弯曲问题的基本解

提出了求解各向异性板弯曲问题基本解的新方法。得到的基本解简捷明了，相应的法向弯矩和相当剪力的表达式易求，故便于应用在一般边界条件的各向异性板弯曲问题的边界积分方程。     

Series solution for elastic behavior of corrugated circular plates in large deflection under arbitrary loads

Chebyshev polynomials are used to solve the problem of large deflection for corrugated circular plates with a plane central region under arbitrary loads based on the nonlinear bending theory of anisotropic circular plates. Numerical results are compared with those available in the literature. The present method shows higher accuracies and larger application ranges.     

Closed-form solution of an arbitrarily laminated,anisotropic, elliptic plate under uniform pressure

A closed-form solution for an arbitrarily laminated, anisotropic plate subjected to uniform loading is presented here for the first time. The theory used is the well-established theory of thin, heterogeneous, anisotropic plates due to Reissner and Stavsky. All components of the stretching, bending-stretching coupling, and bending stiffness matrices are included. The specific geometry considered is an elliptic plate clamped both flexurally and in-plane at its edge.     

Vibrations of highly prestressed anisotropic plates via a numerical-perturbation technique

The method of matched asymptotic expansions is used to reduce the problem of the transverse vibrations of a highly prestressed anisotropic plate into the simpler problem of the vibration of an anisotropic membrane with modified boundary conditions that account for the bending effects. In the absence of an exact solution the membrane problem can be solved by any well-known numerical technique. The numerical-perturbation results for a clamped circular plate with rectangular orthotropy and a uniform tensile stress applied on its boundary show an excellent correlation with finite-element solutions for the original problem. Furthermore, the solutions obtained for annular plates form the basis for solutions to problems involving near-annular plates.     

FREE VIBRATION OF ANISOTROPIC RECTANGULAR PLATES BY GENERAL ANALYTICAL METHOD

According to the differential equation for transverse displacement function of anisotropic rectangular thin plates in free vibration, a general analytical solution is established. This general solution, composed of the composite solutions of trigonometric function and hyperbolic function, can satisfy the problem of arbitrary boundary conditions along four edges. The algebraic polynomial with double sine series solutions can also satisfy the problem of boundary conditions at four corners. Consequently, this general solution can be used to solve the vibration problem of anisotropic rectangular plates with arbitrary boundaries accurately. The integral constants can be determined by boundary conditions of four edges and four corners. Each natural frequency and vibration mode can be solved by the determinate of coefficient matrix from the homogeneous linear algebraic equations equal to zero. For example, a composite symmetric angle ply laminated plate with four edges clamped has been calculated and discussed.     

Approximate determinations of the center of shear by use of the St. Venant solution for the flexure problem of plates of variable thickness

Summary We extend a recent analysis of the shear center problem in the context of the linear theory of transverse bending of orthotropic elastic plates by an explicit comparison of results based on several differing definitions of the center of shear within the framework of the St. Venant flexure solution for the problem of orthotropic plates. We also consider transverse bending of anisotropic plates where we find a significant aspect ratio effect not present in the orthotropic, case, and the shear center problem for plates with combined midplane bending and stretching as a consequence of constitutive coupling.

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Näherungsweise Bestimmungen des Schubmittelpunks für Platten variabler Dicke im Rahmen der St. Venant'schen Querkraft-Biegungslösung

Übersicht Eine kürzliche Analyse des Schubmittelpunktproblems als ein Problem der linearen Theorie orthotroper elastischer Platten wird erweitert durch einen Vergleich von Resultaten auf Grund von verschiedenen Definitionen des Schubmittelpunkts im Rahmen des St. Venant'schen Ansatzes für das Querkraft-Biegeproblem. In Ergänzung dieser Betrachtungen wird eine Bestimmung des Schubmittelpunkts anisotroper Platten ausgeführt, welche, im Unterschied zum orthotropen Fall, einen ausgeprägten Einfluß der Plattenlänge zeigt. Weiterhin behandelt wird das Schubmittelpunktproblem für Platten, für welche Biegung und Streckung durch das Stoffgesetz gekoppelt sind.

     

Exact solutions for magneto-electro-elastic laminates in cylindrical bending

Analytical solutions are derived for the cylindrical bending of multilayered, linear, and anisotropic magneto-electro-elastic plates under simple-supported edge conditions. We construct the general solution in terms of a simple formalism for any homogeneous layer, from which any physical quantities can be solved for the given boundary conditions. For multilayered plates, we derive the solution in terms of the propagator matrices. A special feature of cylindrical bending, which distinguishes itself from the three-dimensional plate problem, is that the associated eigenvalues for any homogeneous layer are independent of the sinusoidal mode, and thus need to be solved only once. Typical numerical examples are also presented for a piezomagnetic plate, a two-layered piezoelectric/piezomagnetic plate, and a four layered piezoelectric/piezomagnetic plate, with different span-to-thickness ratios. In particular, the piezoelectric and piezomagnetic fields show certain interesting features, which give guidance on the development of piezoelectric/piezomagnetic thin-plate theories. Furthermore, it is shown that the variations of the elastic, electric, and magnetic quantities with thickness depend strongly upon the material property and layering, which could be useful in the analysis and design of smart composite structures with sensors/actuators.     

Structure and properties of the solution space of general anisotropic laminates

The algebraic structure of the solution space of all types of anisotropic laminates is determined. The full space is shown to be the direct sum of a number of orthogonal eigenspaces, one for each simple or multiple eigenvalue, whose dimension equals the multiplicity. There are eight different types of eigenvalues, which combine to yield eleven distinct types of laminates with peculiar representations of the general solution. All such representations are explicitly obtained, along with the pseudo-metrics based on the binary product of the eigenvectors. This leads to the projection operators in the solution space, spectral sums and intrinsic tensors analogous to the Stroh–Barnett–Lothe tensors in 2-D elasticity. The present theoretical results are obtained by adopting a mixed formulation involving the deflection function and Airy’s stress function, and by using new laminate elasticity matrices different from the conventional stiffness matrices A, B and D. The new formulation also discloses an isomorphism relating each anisotropic laminate to an image laminate, such that every equilibrium solution of the former directly yields an image solution of the latter by interchanging the kinematical and kinetic variables and the in-plane and out-of-plane variables. This implies, in particular, that the classical bending theory of homogeneous plates and symmetric laminates is not a distinct subject, despite its historical development and pedagogical recognition, but is mathematically identical to the plane stress problem of anisotropic elasticity.