两点边值问题的小波配点法

根据多分辨分析,提出用任意连续的尺度函数构造区间上的插值基函数,形成以尺度函数为基础的求解两点边值问题的小波配点法.该方法中,尺度函数不受紧支撑、插值等性质的限制,计算复杂度小,数值解收敛性由多分辨分析理论保证.同时,给出边值条件的积分处理方法,能够方便地处理任意边界条件,当尺度函数不具有高阶导数时,该方法也能有效使用.数值算例表明,该方法是一个高效、高精度的算法.     

求解Helmholtz方程基于核重构思想的最小二乘配点法

基于核重构思想构造近似函数，将配点法和最小二乘原理相结合对微分方程进行离散， 建立了Helmholtz方程的最小二乘配点格式，并分别研究了Helmholtz方程的波传播问题和 边界层问题. 通过数值算例可以发现，给出的数值计算结果非常接近于精确解，计算精度明显高于SPH 法的数值结果，且随着节点数目的增加，其精确度越来越高，具有良好的收敛性.     

基于拉格朗日插值的无网格直接配点法和稳定配点法

由于无网格法中大多数近似函数均为有理式,不具有Kronecker delta性质,因此难以精确地施加本质边界条件.边界误差较大容易导致整个求解域求解结果精度低,甚至引起数值不稳定现象.文章在无网格直接配点法和稳定配点法中引入拉格朗日插值函数作为形函数,构建了拉格朗日插值配点法(LICM)和拉格朗日插值稳定配点法(SLICM).由于拉格朗日插值具有Kronecker delta性质,可以像有限元法一样简单而精确地施加本质边界条件,提高这两种方法的数值求解精度.稳定配点法基于子域对强形式方程进行积分,可以满足高阶积分约束,即可以保证形函数在积分形式下也满足高阶一致性条件,实现精确积分.同时,进行子域积分还可以减少离散矩阵的条件数,从而提高算法的稳定性.进一步提高拉格朗日插值稳定配点法的精度和稳定性.通过数值算例验证这两种方法的精度、收敛性和稳定性,结果表明基于拉格朗日插值的配点法的精度优于基于重构核近似的配点法,拉格朗日插值稳定配点法的精度和稳定性均优于拉格朗日插值配点法.     

旋转薄壳转点频段的轴对称振动解

用渐近方法求解了含转点频段的旋转薄壳自由振动方程,重新定义了第一和第二类广义相关函数,求得了一致有效解.该解的新颖之处在于具有对称的耦合结构,即转点一侧的奇异无矩解在另一侧含有快变弯曲解成分,同时转点一侧的1个弯曲解在另一侧含有慢变无矩解成分.数值计算表明,所得一致有效解与有限元计算结果吻合.     

空间各向异性弹性问题的八节点理性单元

常规单元的插值函数通常仅考虑单元的几何形状与节点位置,而忽略了反映物理问题关键特性的物性参数,从而降低了其数值分析的效果。相反,理性有限元法是取问题微分控制方程的多项式基本解作为单元内的插值函数,其所形成的刚度阵与问题的物性参数紧密相关,因此它避免了常规有限元法对物理问题和数学问题的割裂,可显著提高数值分析的稳定性和精度。本文利用空间各向异性问题的基本解,构造出满足分片实验要求的八节点理性块体单元。数值算例表明,本文给出的理性单元不仅具有较高的求解精度,而且具有良好的数值稳定性,尤其是对较为畸形的单元反应不敏感。     

基于径向基函数配点法的梁板弯曲问题分析

采用径向基函数配点法分析考虑剪切效应的梁板弯曲问题,该方法利用径向基函数作为近似函数,基于配点法离散方程,通过最小二乘法求解。径向基函数配点法在离散和计算过程中不需要任何形式的网格划分,是一种真正的无网格法;径向基函数可以用一元函数来描述多元函数,存在明显的储存和运算简单的特点;而基于配点法求解不需要积分,提高了计算效率。分析考虑剪切效应的薄梁板问题时,传统的有限元法或无网格法求解均会存在剪切锁闭问题,而径向基函数在全域内存在无限连续性,能够准确地满足Kirchhoff约束条件,因此径向基函数配点法能够消除剪切锁闭现象,而且不会出现应力波动。该方法的优势在于,其不仅易于离散、精度高,而且具有指数收敛率,计算效率高。数值算例验证了上述结论和该方法的稳定性。     

空间各向异性弹性问题的八节点理性单元

常规单元的插值函数通常仅考虑单元的几何形状与节点位置,而忽略了反映物理问题关键特性的物性参数,从而降低了其数值分析的效果。相反,理性有限元法是取问题微分控制方程的多项式基本解作为单元内的插值函数,其所形成的刚度阵与问题的物性参数紧密相关,因此它避免了常规有限元法对物理问题和数学问题的割裂,可显著提高数值分析的稳定性和精度。本文利用空间各向异性问题的基本解,构造出满足分片实验要求的八节点理性块体单元。数值算例表明,本文给出的理性单元不仅具有较高的求解精度,而且具有良好的数值稳定性,尤其是对较为畸形的单元反应不敏感。     

用无网格局部径向点插值法分析非均质中厚板的弯曲问题

用无网格局部径向点插值法分析了非均质中厚板的弯曲问题.利用虚位移原理推导了中厚板的离散系统方程.采用径向基函数耦合多项式基函数来近似试函数,用四次样条函数作为加权残值公式中的权函数.所构造成的形函数具有Kronecker delta性质,可以很方便地施加本质边界条件.此方法不需要任何形式的网格划分,所有的积分都在规则形状的子域及其边界上进行,是一种真正的无网格方法.在计算过程中,取积分中的高斯点的材料参数来模拟问题域材料特性的变化.算例结果表明这种无网格方法具有效率高、精度高和易于实现等优点.     

有限覆盖径向点插值方法理论及其应用

数值流形方法能够统一地处理连续与非连续变形问题,有限覆盖技术是这种方法的核心。无网格方法前处理过程比较简单,径向点插值法是其中的一种计算格式。本文将有限覆盖技术与径向点插值方法相结合发展了有限覆盖径向点插值无网格方法,综合了数值流形方法与点插值方法的各自优点,能够有效地处理连续与非连续性问题,由此所构造的形函数具有Kronecker δ-函数属性,能够有效地处理位移边界条件。本文在阐述了这种方法基本原理的基础上,通过算例分析与数值计算论证了本文所建议方法的可靠性及其有效性。     

基于分区径向基函数配点法的大变形分析

无网格法因为不需要划分网格, 可以避免网格畸变问题,使得其广泛应用于大变形和一些复杂问题. 径向基函数配点法是一种典型的强形式无网格法,这种方法具有完全不需要任何网格、求解过程简单、精度高、收敛性好以及易于扩展到高维空间等优点,但是由于其采用全域的形函数, 在求解高梯度问题时 存在精度较低和无法很好地反应局部特性的缺点. 针对这个问题,本文引入分区径向基函数配点法来求解局部存在高梯度的大变形问题. 基于完全拉格朗日格式,采用牛顿迭代法建立了分区径向基函数配点法在大变形分析中的增量求解模式.这种方法将求解域根据其几何特点划分成若干个子域, 在子域内构建径向基函数插值, 在界面上施加所有的界面连续条件,构建分块稀疏矩阵统一求解. 该方法仍然保持超收敛性, 且将原来的满阵转化成了稀疏矩阵, 降低了存储空间,提高了计算效率. 相比较于传统的径向基函数配点法和有限元法, 这种方法能够更好地反应局部特性和求解高梯度问题.数值分析表明该方法能够有效求解局部存在高梯度的大变形问题.      

基于单位分解法的无网格数值流形方法

在数值流形方法和单位分解法的基础上，提出了无网格数值流形方法. 无网格数值流形 方法在分析时采用了双重覆盖系统，即数学覆盖和物理覆盖. 数学覆盖提供的节点形成求解 域的有限覆盖和单位分解函数；而物理覆盖描述问题的几何区域及其域内不连续性. 与原有 的数值流形方法相比，无网格数值流形方法的数学覆盖形状更加灵活，可以用一系列节点的 影响域来建立数学覆盖和单位分解函数，具有无网格方法的特性，从而摆脱了传统的数值流 形方法中网格所带来的困难. 与无网格方法相比，由于采用了有限覆盖技术，试函数的构造 不受域内不连续的影响，克服了原有的无网格方法在处理不连续问题时所遇到的困难. 详细推导了无网格数值流形方法的试函数和求解方程，最后给出了算例，验证了该方法的正 确性.     

A shape optimisation method of a body located in adiabatic flows

The purpose of this study is to derive an optimal shape of a body located in adiabatic flow. In this study, we use the equation of motion, the equation of continuity and the pressure–density relation derived from the Poisson’s law as the governing equation. The formulation is based on an optimal control theory in which a performance function of fluid force is taken into consideration. The performance function should be minimised satisfying the governing equations. This problem can be solved without constraints by using the adjoint equation with adjoint variables corresponding to the state equation. The performance function is defined by the drag and lift forces acting on the body. The weighted gradient method is applied as a minimisation technique, the Galerkin finite element method is used as a spatial discretisation and the implicit scheme is used as a temporal discretisation to solve the state equations. The mixed interpolation, the bubble function for velocity and the linear function for density, is employed as the interpolation. The optimal shape is obtained for a body in adiabatic flows.     

Shape optimisation of an oscillating body in fluid flow by adjoint equation and ALE finite element methods

The purpose of this paper is to determine the shape of an oscillating body by minimising drag and lift forces, located in a transient incompressible viscous fluid flow by means of the Arbitrary Lagrangian Eulerian finite element method and an optimal control theory. A performance function is expressed by the drag and lift forces. The performance function should be minimised satisfying the state equation and the constant volume condition. Therefore, this problem can be transformed into a minimisation problem without constraint by the Lagrange multiplier method. The adjoint equation and the gradient of the performance function are used to update the shape of the body. In this study, as a minimisation technique, the weighted gradient method is applied. The final shape is obtained of which drag and lift forces are reduced by 66.2% and 92.8%, respectively. The final shape obtained by this study is compared with the final shape of the non-oscillating body. The obtained final shape of the oscillating body is significantly different from the non-oscillating body.     

The improvement of numerical modeling in the solution of incompressible viscous flow problems using finite element method based on spherical Hankel shape functions

In this paper, the finite element method with new spherical Hankel shape functions is developed for simulating 2‐dimensional incompressible viscous fluid problems. In order to approximate the hydrodynamic variables, the finite element method based on new shape functions is reformulated. The governing equations are the Navier‐Stokes equations solved by the finite element method with the classic Lagrange and spherical Hankel shape functions. The new shape functions are derived using the first and second kinds of Bessel functions. In addition, these functions have properties such as piecewise continuity. For the enrichment of Hankel radial basis functions, polynomial terms are added to the functional expansion that only employs spherical Hankel radial basis functions in the approximation. In addition, the participation of spherical Bessel function fields has enhanced the robustness and efficiency of the interpolation. To demonstrate the efficiency and accuracy of these shape functions, 4 benchmark tests in fluid mechanics are considered. Then, the present model results are compared with the classic finite element results and available analytical and numerical solutions. The results show that the proposed method, even with less number of elements, is more accurate than the classic finite element method.     

势问题的重构核粒子边界无单元法

将重构核粒子法和势问题的边界积分方程方法结合，提出了势问题的重构核粒子边界无单元 法. 推导了势问题的重构核粒子边界无单元法的公式，研究其数值积分方案，建立了重构核 粒子边界无单元法的离散化边界积分方程，并推导了重构核粒子边界无单元法的内点位势的 积分公式. 重构核粒子法形成的形函数具有重构核函数的光滑性，且能再现多项式在插值点 的精确值，所以该方法具有更高的精度. 最后给出了数值算例，验证了所提方法的有效性 和正确性. }     

Timoshenko梁谐响应求解新方法探索

在空间域上采用只与结点有关的无网格方法离散，在时间域上采用精细积分方法求 解. 无网格离散过程中，利用伽辽金积分等效弱形式代替微分形式的控制方程，并 用修正变分原理满足位移边界条件，采用移动最小二乘法求解离散的形函数，把形 函数代入等效积分弱形式得到离散的二阶方程；精细积分过程中非齐次项采 用Romberg积分. 同时给出了两种不同边界条件的谐响 应求解的两个数值算例，得到了精确的数值结果.     

ELASTIC DYNAMIC ANALYSIS OF MODERATELY THICK PLATE USING MESHLESS LRPIM

A meshless local radial point interpolation method （LRPIM） for solving elastic dy-namic problems of moderately thick plates is presented in this paper. The discretized system equation of the plate is obtained using a locally weighted residual method. It uses a radial basis function （RBF） coupled with a polynomial basis function as a trial function,and uses the quartic spline function as a test function of the weighted residual method. The shape function has the properties of the Kronecker delta function,and no additional treatment is done to impose essen-tial boundary conditions. The Newmark method for solving the dynamic problem is adopted in computation. Effects of sizes of the quadrature sub-domain and influence domain on the dynamic properties are investigated. The numerical results show that the presented method can give quite accurate results for the elastic dynamic problem of the moderately thick plate.     

A FE‐based algorithm for the inverse natural convection problem

Several numerical algorithms for solving inverse natural convection problems are revisited and studied. Our aim is to identify the unknown strength of a time‐varying heat source via a set of coupled nonlinear partial differential equations obtained by the so‐called finite element consistent splitting scheme (CSS) in order to get a good approximation of the unknown heat source from both the measured data and model results, by minimizing a functional that measures discrepancies between model and measured data. Viewed as an optimization problem, the solutions are obtained by means of the conjugate gradient method. A second‐order CSS in time involving the direct problem, the adjoint problem, the sensitivity problem and a system of sensitivity functions is used in order to enhance the numerical accuracy obtained for the unknown heat source function. A spatial discretization of all field equations is implemented using equal‐order and mixed finite element methods. Numerical experiments validate the proposed optimization algorithms that are in good agreement with the existing results. Copyright © 2010 John Wiley & Sons, Ltd.     

Helmholtz方程的微分容积解法

用一种新型的数值技术－－微分容积法（Differential Cubature Method）求解二维Helmholtz方程的边值问题，几个数值算例表明，该方法稳定收敛，并具有较好的数值精度，本文方法适用于求解具有较小波数的Helmholtz方程。     

NEW TREATMENT OF ESSENTIAL BOUNDARY CONDITIONS IN EFG METHOD BY COUPLING WITH RPIM

One of major difficulties in the implementation of meshfree methods using the moving least square (MLS) approximation, such as element-free Galerkin method (EFG), is the imposition of essential boundary conditions as the approximations do not pass through the nodal parameter values. Another class of meshfree methods based on the radial basis point interpolation can satisfy the essential boundary conditions exactly since its approximation function passes through each node in an influence domain and thus its shape functions possess the properties of delta function. In this paper, a coupled element-free Galerkin(EFG)-radial point interpolation method (RPIM) is proposed to enhance their advantages and avoid their disadvantages. Discretized equations of equilibrium are obtained in the RPIM region and the EFG region, respectively. Then a collocation approach is introduced to couple the RPIM and the EFG method. This method satisfies the linear consistency exactly and can maintain the stiffness matrix symmetric. Numerical tests show that this method gives reasonably accurate results consistent with the theory.