平行四边形加肋板自由振动分析的无网格法

基于一阶剪切理论,提出一种求解平行四边形加肋板自由振动问题的无网格法,通过用一系列点来离散平板及肋条,得到加肋板的无网格模型。基于一阶剪切理论及移动最小二乘近似求出位移场,以梁模拟肋条,求出平行四边形加肋板总动能及总势能。再由Hamilton原理导出加肋板自由振动的控制方程,采用完全转换法引入边界条件,求解方程得出结构自振频率。以不同参数的加肋板为例,将该文解与ABAQUS有限元解进行比较分析。研究表明,该方法能有效地分析平行四边形加肋板自由振动问题,在肋条位置改变时,又避免了网格重构。     

加肋板自由振动的移动最小二乘无单元分析

基于移动最小二乘近似,提出一种分析加肋板结构自由振动行为的无网格方法。将加肋板视为平板和肋条的集合,以梁模型来模拟肋条。从板和肋条位移场的移动最小二乘近似出发,先分别建立板和肋条自由振动情况下的势能泛函,再通过引入板和肋条之间的位移协调关系,将两者的势能叠加,建立描述整个加肋板自由振动行为的控制方程。本文方法的无网格特性让肋条可以配置在板上的任意位置,而肋条位置的改变也不会像有限元那样导致板网格的重构,应用于加肋板的优化设计中可极大的减轻分析负担。文末通过算例将本文方法解与ANSYS软件给出的有限元解及现有文献结果比较,验证本文方法的准确性     

弹性地基圆形加肋板静力弯曲及弯曲自由振动分析的无网格法

基于一阶剪切理论和移动最小二乘法,提出分析弹性地基圆形加肋板线性弯曲的静力和自由振动问题的无网格方法.对弹性地基采用Winkler地基模型,对圆形加肋板则将平板和肋条分开考虑,通过位移协调条件建立两者的参数转换方程.平板和肋条均采用一系列点来离散,用移动最小二乘法建立的形函数来分别描述两者的位移场,再分别通过最小势能原...     

弹性地基圆形加肋板静力弯曲及弯曲自由振动分析的无网格法EI北大核心CSCD

基于一阶剪切理论和移动最小二乘法,提出分析弹性地基圆形加肋板线性弯曲的静力和自由振动问题的无网格方法。对弹性地基采用Winkler地基模型,对圆形加肋板则将平板和肋条分开考虑,通过位移协调条件建立两者的参数转换方程。平板和肋条均采用一系列点来离散,用移动最小二乘法建立的形函数来分别描述两者的位移场,再分别通过最小势能原理和Hamilton原理导出弹性地基的静力弯曲和弯曲自由振动控制方程,最后采用完全转换法处理边界条件。以一系列不同基床系数、荷载、边界、肋条布置方式的弹性地基圆形加肋板为例,研究所提出方法的收敛性和稳定性,并将计算结果与有限元、文献结果对比。研究表明该方法可以有效分析弹性地基圆形加肋板线性弯曲的静力和自由振动问题,且肋条位置改变时,可避免网格重构。     

任意壳线性弯曲与自由振动分析的最小二乘无网格法

提出了一种求解任意壳结构线性弯曲与自由振动的最小二乘无网格法。利用映射技术并结合Mindlin板壳理论将三维任意壳参数化曲面转换成二维无网格模型。基于移动最小二乘法近似和一阶剪切变形理论求出其位移场,利用最小势能原理及Hamilton原理分别得到其弯曲及自由振动控制方程。由于该方法不能直接施加本质边界条件,故采用完全转换方法引入本质边界条件。文末以几种典型的不同形状壳结构算例表明,该研究的解与理论解或ABAQUS有限元解吻合良好,证明了该方法在计算任意壳的线性弯曲与自由振动的有效性及准确性。     

任意壳线性弯曲与自由振动分析的最小二乘无网格法EI北大核心CSCD

提出了一种求解任意壳结构线性弯曲与自由振动的最小二乘无网格法。利用映射技术并结合Mindlin板壳理论将三维任意壳参数化曲面转换成二维无网格模型。基于移动最小二乘法近似和一阶剪切变形理论求出其位移场,利用最小势能原理及Hamilton原理分别得到其弯曲及自由振动控制方程。由于该方法不能直接施加本质边界条件,故采用完全转换方法引入本质边界条件。文末以几种典型的不同形状壳结构算例表明,该研究的解与理论解或ABAQUS有限元解吻合良好,证明了该方法在计算任意壳的线性弯曲与自由振动的有效性及准确性。     

对称层合折板结构自由振动分析的移动最小二乘无网格法

提出了一种求解对称层合折板结构自由振动问题的移动最小二乘无网格法。以作者提出的折板无网格模型为基础,将对称层合折板结构视为由不同平面上对称层合板组成的复合结构。先基于一阶剪切变形理论,由移动最小二乘近似推导出各对称层合板的刚度和质量矩阵,再利用板与板间的位移协调条件,将各板的刚度和质量矩阵叠加得到整个结构的刚度和质量矩阵,推导出描述层合折板结构自由振动行为的控制方程。文末算例表明由本文方法得到的解与采用壳单元得到的ANSYS有限元解吻合良好,证明了本文方法的准确性。     

折板结构非线性弯曲分析的移动最小二乘无网格法

提出了一种研究折板结构非线性弯曲行为的移动最小二乘无网格法。先将折板结构模拟成不同平面上平板的集合体,再基于冯.卡门的大挠度理论,使用一阶剪切变形理论和移动最小二乘近似先分析各平板的几何非线性行为,最后将通过修正的各板的非线性刚度矩阵叠加得到整个折板结构的非线性刚度矩阵,研究整个结构的几何非线性行为。由于摆脱了网格的束...     

波纹夹层板线性弯曲分析的无网格伽辽金法

提出了一种求解波纹夹层板结构线性弯曲问题的无网格模型。将波纹夹层板看成两侧平板和中间波纹板核的复合结构,用正交各向异性板等效近似波纹板核。先基于一阶剪切变形理论,由无网格伽辽金法建立各板的刚度方程,再通过位移协调条件将各板刚度方程叠加,以得到整体刚度方程。采用全转换法处理位移边界。算例表明：该文所提出的无网格模型分析波...     

正交各向异性板剪切屈曲载荷的近似表达式研究

利用Rayleigh-Ritz法和通用有限元程序ANSYS分析了纵向边被转动弹簧或扭转加劲肋约束的正交各向异性长板的临界屈曲问题, 引入无量纲正交各向异性参数、约束系数和临界屈曲系数, 利用曲线拟合技术, 得到了这两类约束板在均匀剪力作用下的临界屈曲载荷近似解公式;利用临界纵横比, 把求得的针对转动弹簧约束的临界屈曲解应用到扭转加劲肋约束板的临界屈曲解中, 同样得到了扭转加劲肋约束板的临界屈曲载荷。将求得的近似表达式与有限元ANSYS数值解以及文献中的结果进行对比, 结果吻合良好。     

Buckling analysis of corrugated plates using a mesh-free Galerkin method based on the first-order shear deformation theory

This paper deals with elastic buckling analysis of stiffened and un-stiffened corrugated plates via a mesh-free Galerkin method based on the first-order shear deformation theory (FSDT). The corrugated plates are approximated by orthotropic plates of uniform thickness that have different elastic properties along the two perpendicular directions of the plates. The key to the approximation is that the equivalaent elastic properties of the orthotropic plates are derived by applying constant curvature conditions to the corrugated sheet. The stiffened corrugated plates are analyzed as stiffened orthotropic plates. The stiffeners are modelled as beams. The stiffness matrix of the stiffened corrugated plate is obtained by superimposing the strain energy of the equivalent orthotropic plate and the beams after implementing the displacement compatibility conditions between the plate and the beams. The mesh free characteristic of the proposed method guarantee that the stiffeners can be placed anywhere on the plate, and that remeshing is avoided when the stiffener positions change. A few selected examples are studied to demonstrate the accuracy and convergence of the proposed method. The results obtained for these examples, when possible, are compared with the ANSYS solutions or other available solutions in literature. Good agreement is evident for all cases. Some new results for both trapezoidally and sinusoidally corrugated plates are then reported.     

阻尼夹芯复合材料加筋板的振动分析与数值模拟

以阻尼夹芯复合材料加筋板为研究对象,依据一阶剪切变形理论(FSDT)和Hamilton原理,推导板和加强筋的应变能、动能表达式,采用变分原理建立控制微分方程,根据相关边界条件和傅里叶级数求解方程。建立了ANSYS阻尼夹芯复合材料加筋板的有限元模型,该模型考虑到阻尼夹芯复合材料加筋板中阻尼材料与纤维预浸料间的结合方式,用模态应变能有限元数值模拟方法研究了结构的动力学性能,并通过对数值模拟结果与理论解的比较,验证了模型的合理性和有效性。探讨了不同的筋条尺寸、不同的筋条数量、不同的筋条分布方式对阻尼夹芯复合材料加筋板动力学性能的影响,得出了阻尼夹芯复合材料加筋板的一阶模态频率和损耗因子随不同参数的变化曲线,其结论为阻尼夹芯复合材料加筋板的优化设计提供参考。     

Buckling of the composite laminates containing through-the-width delaminations using different plate theories

The buckling behavior of the composite laminates with through-the-width delaminations is studied by using different plate theories. The analytical method is based on the CLPT, FSDT and HSDT plate theories. The formulation is developed on the basis of the Rayleigh–Ritz technique by the implementation of the simple polynomial series. The contact among sublaminates is handled. The three-dimensional FEM analysis is also performed by using ANSYS5.4 commercial software, and the results are compared with those obtained by the analytical models. The agreement between the results is very good.     

斜卷边冷弯薄壁槽钢轴压柱弹性畸变屈曲计算

畸变屈曲是冷弯薄壁卷边槽钢的一种重要屈曲模式,弹性畸变屈曲临界应力是目前一些主要规范计算畸变屈曲的关键。该文首先推导出畸变屈曲模式下,构件纵向翘曲位移的显式计算公式,从而简化计算过程;然后基于经典的薄板理论,计算平面内位移,确定构件平面内的变形,在现有研究基础上得到斜卷边冷弯薄壁槽钢轴压柱弹性畸变屈曲计算公式;最后与有限条法、近似模型计算法进行对比,验证了该文计算方法的正确和有效性。该文中的弹性畸变屈曲计算公式简单,便于手算,可供工程设计人员参考。     

Levy Solution for Buckling Analysis of Functionally Graded Rectangular Plates

In this article, an analytical method for buckling analysis of thin functionally graded (FG) rectangular plates is presented. It is assumed that the material properties of the plate vary through the thickness of the plate as a power function. Based on the classical plate theory (Kirchhoff theory), the governing equations are obtained for functionally graded rectangular plates using the principle of minimum total potential energy. The resulting equations are decoupled and solved for rectangular plate with different loading conditions. It is assumed that the plate is simply supported along two opposite edges and has arbitrary boundary conditions along the other edges. The critical buckling loads are presented for a rectangular plate with different boundary conditions, various powers of FGM and some aspect ratios.     

Semi-analytical mechanical and thermal buckling analyses of 2D-FGM circular plates based on the FSDT

In the present paper, mechanical and thermal buckling analyses of two-directional functionally graded material (2D-FGM) circular plate are investigated. The motion equations have been derived based on the first-order shear deformation theory (FSDT) and power series method has been employed to solve the motion equations. Two different kinds of boundary condition including simply supported and fixed are considered. The material properties are assumed to vary in both transverse and radial directions according to power and exponential laws, respectively. Comparisons with available studies in the literature confirm the high accuracy of the current approach. The effects of geometrical parameters and 2D-FG power indices on the critical buckling load have been studied. It is shown that increase of modulus of elasticity of outer layers of plate due to higher presence of hard phase of FGM, in radius and thickness directions of the plate makes it possible to attain a more solid structure against mechanical buckling loads, while increase of coefficient of thermal expansion and coefficient of thermal conduction of outer layers of plate results in less stability against thermal buckling loads.     

Thermal buckling behavior of laminated composite plates with temperature-dependent properties

The thermal buckling behavior of composite laminated plates subjected to a uniform temperature field is investigated by the finite element method. Temperature-dependent elastic and thermal properties are considered. The stiffness and geometry matrices are derived based on the principle of minimum potential energy. The assumed displacement state over the middle surface of the plate element is expressed as the product of one-dimensional, first-order Hermitian polynomials. An iterative method is employed to determine the thermal buckling load. It is shown by numerical results that the influence of temperature-dependent mechanical properties on the thermal buckling behavior is significant.     

基于一阶剪切变形理论的新型复合材料层合板单元

基于一阶剪切变形理论(FSDT),本文构造一种新型的20自由度(每结点5个自由度),四边形复合材料层合板单元,适合于任意铺设情形的层合板的计算。它是按如下方式构造的:(1) 单元每边的转角和剪应变由Timoshenko层合厚梁理论来确定;(2) 对单元域内的转角场和剪应变场进行合理的插值;(3) 引入平面内双线性位移场来体现层合板面内与弯曲的耦合作用。本文单元,记为TMQ20,不存在剪切闭锁现象,在计算单层的各向同性板时可以退化为文[1]中优质的中厚板单元TMQ。在文[2]中将给出本文单元对于层合板问题的详细数值算例。