弹性理论中各种变分原理的分类

本文按弹性理论中各种变分原理的约束条件的不同,对所有变分原理进行分类.我们在前文中业已指出,应力应变关系这样的约束条件是不能用拉氏乘子法解除的.剩下的可能约束条件共有四种:(1)平衡方程,(2)应变位移关系,(3)边界外力已知的边界条件,和(4)边界位移已知的边界条件.弹性理论的各种变分原理中,有的只有一种约束条件,有的有两种或三种,最多只能有四种约束条件.这样一共可能有15种变分原理,但是每种变分原理既可以用应变能A表示,又可以用余能B表示.这样,我们一共应有30种形式完全不同的变分原理,我们全部列出了这三十种形式的变分原理.     

变厚度扁锥壳的非线性固有频率

借助于变厚度圆薄板非线性动力学变分方程和协调方程,给出了变厚度扁薄锥壳的非线性动力学变分方程和协调方程·　假设薄膜张力由两项组成,将协调方程化为两个独立的方程,选取变厚度扁锥壳中心最大振幅为摄动参数,采用摄动变分法,将变分方程和微分方程线性化·　对周边固定的圆底变厚度扁锥壳的非线性固有频率进行了求解;一次近似得到了变厚度扁锥壳的线性固有频率,三次近似得到了变厚度扁锥壳的非线性固有频率,且绘出了固有频率与静载荷、最大振幅、变厚度参数的特征曲线图·　为动力工程提供了有价值的参考·     

双层网格圆底扁球壳的非线性稳定问题

从基于等效夹层壳思想的双层网格扁壳,非线性弯曲理论的变分方程出发,利用坐标变换方法和驻值余能原理,导出双层网格圆底扁球壳,在均布压力作用下的轴对称大挠度方程和边界条件．采用修正迭代法,求得了两类边界条件下双层网格圆底扁球壳的非线性载荷-位移关系式和临界屈曲载荷的解析表达式,并讨论了几何参数对临界屈曲载荷的影响．     

大位移非线性弹性理论的变分原理和广义变分原理

在前文中[1],作者首次提出了大位移非线性弹性力学的位能原理和余能原理,以及各种完全的和不完全的广义变分原理.但在约束条件和欧拉条件上,证明和叙述都不很明确,有时甚至把原来应该是欧拉方程的误认为是约束条件,如余能驻值原理中,应力位移关系原应是欧拉方程,但把它当作了变分约束条件.这就是说:我们把余能驻值原理约束得超过了必要的要求.还有,在所有变分原理中,应力应变关系式都是不参加变分的约束条件,亦即,他们是从已定应力导出应变或从已定应变导出应力的约束条件.这一点,在文[1](1979)中,并未明确指出.本文并将用高阶拉氏乘子法,导出更一般的广义变分原理(1983)[2].本文使用V.V.Novozhilov的有关非线性弹性力学的成果(1958)[3].     

锥壳的位移解及应用*

本文提出求锥壳方程通解的另一种方法——位移法.文中根据文献[1]给出的壳体基本关系,导出锥壳一般弯曲问题的位移方程组,然后通过引入一个位移函数U(s,θ)(在极限情况下,就变为对于圆柱壳所引入的位移函数),从而将锥壳基本方程组化成关于位移函数U(s,θ)的8阶可解偏微分方程(控制微分方程).对于一般弯曲问题,该方程的一般解以广义超几何函数给出;对于轴对称弯曲问题,用Bessel函数给出其一般解.作为锥壳位移解法的应用,讨论了Winkler地基模式上的锥壳的轴对称弯曲问题,给出数值结果.     

变厚度夹层截顶扁锥壳的非线性稳定性分析

对具有变厚度夹层截顶扁锥壳的非线性稳定问题进行了研究。利用变分原理导出表层为等厚度而夹心为变厚度的夹层截顶扁锥壳的非线性稳定问题的控制方程和边界条件,采用修正迭代法求得了具有双曲型变厚度夹层截顶扁锥壳的非线性稳定性问题的解析解,得到了内边缘与一刚性中心固结而外边缘为可移夹紧固支的变厚度夹层截顶扁锥壳临界屈曲载荷的解析表达式,讨论了几何参数和物理参数对壳体屈曲行为的影响。     

变壁厚柱壳的轴对称问题

本文给出了壁厚按二次函数变化的轴对称柱壳的一般解.K.Federhofer[1]曾研究过壁厚按轴向坐标的二次函数变化的轴对称柱壳,并且给出了在某些情况下的解.本文也研究上述壳体.对于所有可能的情况,给出了控制微分方程的齐次解;对于控制微分方程的非齐次项可表示为自变量的多项式或收敛幂级数的情况,给出了方程的特解.     

具有不等厚表层的夹层旋转壳问题

本文探讨了具有各向同性夹心及不等厚表层组成的三层旋转壳的小挠度问题,采用广义变分法,在考虑表层抗弯刚度的情况下,导出了基本方程,其特例即为文献[3],[4]的结果. 根据所导出的基本方程,本文求解对称加载的夹层旋转壳问题,将其归结为只含一个广义位移的六阶微分方程. 本文的理论可应用于复合装甲及其它工程设计.     

复杂载荷下加筋圆柱壳非线性冲击屈曲研究

将加筋圆柱壳离散成为由圆柱壳和加强筋组成的壳体-肋骨系统,假设环向加筋与壳体在接触处刚性连接,由Hamilton变分原理推导出加筋圆柱壳结构的运动方程,以研究加筋圆柱壳在水下冲击载荷和静水压力以及动水压力组成的复杂载荷联合作用下的非线性屈曲行为。借助增量数值(在时域采用4阶Runge-Kutta方法)的方法来分析了加筋圆柱壳的非线性屈曲行为,经过算例分析验证了材料因素和初始缺陷对结构屈曲的重要影响。     

复合材料旋转壳非线性稳定性分析计算

利用前屈曲一致理论和能量变分法分析计算了复合材料旋转壳非线性稳定性.前屈曲应变-位移关系采用非线性的卡门方程,能量积分采用数值积分,用势能最小原理求解前屈曲位移和内力,提出了求解临界载荷的实用计算方法,用FORTRAN语言编制了相应的计算机程序,并给出了算例.     

只含两个独立变量的扁壳大挠度问题修正的海林格—赖斯内变分泛函

本文首先用海林格-赖斯内变分原理建立任意形状扁壳大挠度问题的泛函，然后用修正的变分原理导出适合于有限单元法的变分泛函表达式．泛函中只包含应力函数F和挠度W两个独立交量．其中也导出了在边界上用上述两个变量表示的中面位移的表达式．推导中考虑了边界的曲率，所以适用于任意形状的边界．     

构造容许位移的转换边界法

本文提出了在复杂边界条件下构造容许位移的转换边界法.所谓转换边界法,就是首先根据叠加原理将实际系统转换为基本系统及附加边界力和附加边界位移,然后应用变分原理于基本系统,最后应用级数转换的办法求得实际系统的容许位移.本文还给出了边界条件变化的混合能量原理.这边界条件变化的混合能量原理和边界条件变化的势能原理和余能原理都是转换边界法的主要理论基础.应用转换边界法我们构造了复杂边界条件平面应力问题和弯曲问题矩形板的容许位移.由于转换边界法构造容许位移是遵循着变分原理和确定的程序进行的,因而克服了Rayleigh-Ritz法猜测、拼凑容许位移的困难.     

叠层圆柱厚壳混合状态方程的弱形式及其边值问题

从Helinger-Reisner变分原理出发,在柱坐标系中,导出圆柱壳的弱形式混合状态方程和边界条件,联用状态空间法给出叠层柱壳的解析解,此法使得求解该类问题的形式得以扩大和统一。     

A Piezoelectric Finite Shell Element for the Geometrically Nonlinear Analysis of Sensors

A geometrically nonlinear finite element formulation to analyze piezoelectric shell structures is presented. The formulation is based on the mixed field variational functional of Hu–Washizu. Within this variational principle the independent fields are displacements, electric potential, strains, electric field, stresses and dielectric displacements. The mixed formulation allows an interpolation of the strains and the electric field through the shell thickness, which is an essential advantage when using a three dimensional material law. It is remarked that no simplification regarding the constitutive relation is assumed. The normal zero stress condition and the normal zero dielectric displacement condition are enforced by the independent resultant stress and resultant dielectric displacement fields. The shell structure is modeled by a reference surface with a four node element. Each node possesses six mechanical degrees of freedom, three displacements and three rotations, and one electrical degree of freedom, which is the difference of the electric potential through the shell thickness. The developed mixed hybrid shell element fulfills the in–plane, bending and shear patch tests, which have been adopted for coupled field problems. A numerical investigation of a smart antenna demonstrates the applicability of the piezoelectric shell element under the consideration of geometrical nonlinearity. (© 2008 WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim)     

Forced Vibration of Three-Layered Spherical and Ellipsoidal Shells under Axisymmetric Loads

A variant of vibration theory for three-layered shells of revolution under axisymmetric loads is elaborated by applying independent kinematic and static hypotheses to each layer, with account of transverse normal and shear strains in the core. Based on the Reissner variational principle for dynamic processes, equations of nonlinear vibrations and natural boundary conditions are obtained. The numerical method proposed for solving initial boundary-value problems is based on the use of integrodifferential approach for constructing finite-difference schemes with respect to spatial and time coordinates. Numerical solutions are obtained for dynamic deformations of open three-layered spherical and ellipsoidal shells, over a wide range of geometric and physical parameters of the core, for different types of boundary conditions. A comparative analysis is given for the results of investigating the dynamic behavior of three-layered shells of revolution by the equations proposed and the shell equations of Timoshenko and Kirhhoff-Love type, with the use of unified hypotheses across the heterogeneous structure of shells.     

组合型扁壳的一种广义变分原理及对幕壳的应用

本文提出一个带边梁的组合型扁壳弹性动力学广义变分原理,对它与相应的基本方程、脊线条件及边界条件的等价性作了论证.然后将这一变分原理应用于幕壳结构,利用多重级数给出幕壳在常见的边界条件下的静动力学近似解析解,将本文解析解同有限元计算及试验值作了比较,结果表明我们的解析解收敛性好,精确性令人满意.     

A mixed finite element formulation for piezoelectric shells

A finite element formulation to analyze piezoelectric shell problems is presented. A reference surface of the shell is modelled with a four node element. Each node possesses six mechanical degrees of freedom, three displacements and three rotations, and one electric degree of freedom, which is the difference of the electric potential in thickness direction. The formulation is based on the mixed field variational principle of Hu-Washizu. The independent fields are displacements u , electric potential φ, strains E , electric field E , stresses S and dielectric displacements D . The mixed formulation allows an interpolation of the strains and the electric field in thickness direction. Accordingly a three-dimensional material law is incorporated in the variational formulation. It is remarked that no simplification regarding the constitutive law is assumed. The formulation allows the consideration of arbitrary constitutive relations. The normal zero stress condition and the normal zero dielectric displacement condition are enforced by the independent stress and dielectric displacement fields. They are defined as zero in thickness direction. The present shell element fulfills the important patch tests: the in-plane, bending and shear test. Some numerical examples demonstrate the applicability of the present piezoelectric shell element. (© 2008 WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim)     

Contact statement of mechanical problems of reinforced on a contour sandwich plates with transversally-soft core

For the sandwich plates and shells with transversally-soft core and carrier layers having on the outer contour of the reinforcing rod, for small deformations, and middle displacements we construct refined geometrically nonlinear theory. This theory allows to describe the process of the subcritical deformation and identify all possible buckling of carrier layers and reinforcing rods. It is based on the introduction as unknown contact forces at the points of interaction mating surface of the outer layers with core and carrier layers and a core with reinforcing rods at all points of the surface of their conjugation to the shell contour. To derive the basic equations of equilibrium, static boundary conditions for the shell and reinforcing rods, as well as conditions of the kinematic coupling of the carrier layers with a core, the carrier layers and a core with reinforcing rods we use previously proposed generalized Lagrange variational principle.     

厚壁圆柱壳开孔应力集中问题的复变函数解法

本文基于考虑横向剪切变形影响的厚壳理论建立了求解圆柱壳开孔应力集中问题的复变函数方法，得到了此种问题的一般解和满足任意形开孔边界条件的表达式·该应力集中问题可以简化为求解无穷代数方程组的问题·用复变函数方法可以规范地求解应力集中问题·文中给出了圆柱壳开小圆孔和椭圆孔时应力集中系数的数值结果·