Timoshenko梁弹塑性有限元分析的无迭代算法

本文从虚功原理出发,给出了 Timoshenko 梁不分层弹塑性有限元分析的一种无迭代算法——线性互补方法.该法精度高,计算量少,对于线性强化材料,若无卸载,只需一个载荷增量步即可求得解答.     

基于虚功原理的弹性接触问题的线性互补方法

在将接触条件表为具有惩罚因子的线性互补形式后，本文详细推导了适用于弹性接触问题的虚功方程，在此基础上，结合有限元离散技术，简捷地导出了一种求解有摩擦弹性接触问题的线性互补方法；这种方法不必迭代，在无卸载时，只要一个增量步即可求得解答，计算效率较高，文末通过实例，说明了方法的正确性及有效性。     

正交各向异性弹塑性摩擦接触问题的数值求解

采用正交各向异性摩擦定律对三维弹塑性摩擦接触问题进行分析,基于参变量变分原理,经过有限元离散,将问题化为线性互补问题模型,之后给出一个求解互补问题的非内点光滑化算法．对三维接触问题,滑动方向的确定一直是个难点,为此,该文采用作者提出的组合规划法和迭代法对各向异性摩擦本构模型进行分析,数值结果说明了模型与算法的正确性。     

工程力学中的互补问题:模型

对互补问题在非线性力学中的一些应用情况给出了较概括的介绍，重点放在了静态接触问题、弹塑性问题以及结构优化问题的互补模型上。将力学问题写成互补模型的好处主要有两点：一是使力学问题有更自然、更精确的数学描述；二是可以考虑用互补问题的有效和强健的数值算法来求解。     

解Drucker-Prager塑性问题的二阶锥互补法

基于经典弹塑性理论中多数屈服准则具有凸锥数学结构的事实,将在大规模计算中更具潜力的锥规划法引入弹塑性分析。考虑到弹塑性流动理论有关联与非关联之分,本文提出利用锥型互补法求解弹塑性问题。具体以Drucker-Prager弹塑性模型为例,首先利用最大塑性功耗散原理和圆锥对偶理论等工具,建立了弹塑性本构方程的等价二阶锥互补模型;然后,基于参变量变分原理和有限元技术,建立了弹塑性增量分析的二阶锥线性互补模型;最后,利用一类半光滑Newton算法求解。数值算例表明了本文方法的有效性。     

三维摩擦接触问题的增量线性互补方法

借助罚因子建立了三维摩擦接触本构模型,接触条件被表示为类似于非关联流动的弹塑性本构关系的形式。采用增量描述,对Coulomb摩擦定律采用Taylor展开作线性近似,导出了接触问题的互补虚功方程,然后基于有限元离散建立了三维摩擦接触问题的增量线性互补方法。数值算例表明了本文方法的有效性。     

弹塑性问题的边界元—流动因子线性互补解

1.前言尽管求解弹塑性问题已有许多方法,但一般来说,如不采用迭代法则不可避免地会产生有效应力偏离屈服面的“漂移”现象.从近代发展起来的变分不等式和参变量变分原理出发所建立起来的有限元方程,较成功地把数学规划理论应用到非线性本构关系的应力分析中.本文方法与以往方法的最大区别在于,将边界元方程与弹塑性屈服准则联立,导出了按增量求解的线性互补方程.因此对任一荷载增量步,通过求解一次线性互补方程,将使边界元方程和屈服准则同时满足,从而既无须迭代又避免了有效应力的漂移.并且也适用于非法向的屈服流动、随机强化模型及Drucker-Prager 模型等.与文献[1-4]的     

改进的速度迭代弹塑性大变形动力半显式算法

提出了基于速度迭代的弹塑性大变形动力半显式算法，并且在此基础上采用拟弯曲膜单元，结合有模卸载方式数值模拟了U形弯曲以及S形导轨回弹过程，着重比较了动力半显式算法与动力显式算法和实验的回弹结果．给出了动力半显式算法的迭代格式和收敛标准．     

一致切线刚度法在三维弹塑性有限元分析中的应用

本文提出了一致切线刚度法，并把它应用于三维弹塑性有限元分析问题。从而解决了增量迭代弹塑性有限元分析方法中长期存在的速度慢、精度低问题，一致切线刚度法满足加卸载互补准则，即没有应力漂移现象，具有一阶精度、二阶迭代收敛速度、计算量少和无条件稳定等优点，借助算例对一致切线刚度法和传统切线刚度法（包括路径相关和路径无关两种结构变量更新格式）从计算精度、迭代收敛速度和计算量等几方面进行了比较。     

基于线性互补模型的梯度塑性连续体无网格方法

对梯度塑性连续体提出了一个归结为线性互补问题的数值分析方法. 塑性乘子与位移均 为主要未知变量，并采用基于移动最小二乘的无网格方法分别在积分点与节点上插值. 联立 弱形式下的平衡方程与积分点上逐点满足的非局部本构方程和屈服准则可以导出一个线性互 补问题，并通过Lexico-Lemke算法求解. 构造了一个基于N-R方法的迭代方案，使得不需要 形成一致性切线刚度矩阵而仍保持二阶收敛性. 一维和二维的数值算例证明了所提出的方 法处理由应变软化引起的应变局部化问题的有效性.     

A non-iterative transformation method for Newton's free boundary problem

In book II of Newton's Principia Mathematica of 1687 several applicative problems are introduced and solved. There, we can find the formulation of the first calculus of variations problem that leads to the first free boundary problem of history. The general calculus of variations problem is concerned with the optimal shape design for the motion of projectiles subject to air resistance. Here, for Newton's optimal nose cone free boundary problem, we define a non-iterative initial value method which is referred in the literature as a transformation method. To define this method we apply invariance properties of Newton's free boundary problem under a scaling group of point transformations. Finally, we compare our non-iterative numerical results with those available in the literature and obtained via an iterative shooting method. We emphasize that our non-iterative method is faster than shooting or collocation methods and does not need any preliminary computation to test the target function as the iterative method or even provide any initial iterate. Moreover, applying Buckingham Pi-Theorem we get the functional relation between the unknown free boundary and the nose cone radius and height.     

A non-iterative transformation method for Blasius equation with moving wall or surface gasification

We define a non-iterative transformation method for Blasius equation with moving wall or surface gasification. The defined method allows us to deal with classes of problems in boundary layer theory that, depending on a parameter, admit multiple or no solutions. This approach is particularly convenient when the main interest is on the behaviour of the considered models with respect to the involved parameter. The obtained numerical results are found to be in good agreement with those available in the literature.     

Variational approach to the study of processes of geophysical hydro-thermodynamics with assimilation of observation data

This paper presents a variational approach to solving direct and inverse problems based on the joint use of mathematical models and data monitoring of processes of geophysical hydro-thermodynamics. This approach is used to solve problems related to environmental protection. A variational principle with weak constraints is formulated to account for uncertainties and errors in models and data. The inclusion of uncertainties makes it possible to develop direct non-iterative algorithms for sequential assimilation of data obtained by various observation systems. Some criteria and functions for controlling the quality of the natural environment are introduced into the modeling system to solve inverse problems of environmental risk assessment. A problem with data assimilation is considered for the Novosibirsk agglomeration.     

A Note on the Numerical Treatment of the k-epsilon Turbulence Model*

Numerical solution of the equations arising from the κ mdash; ε turbulence model has difficulties inherent to nonlinear convection-reaction-diffusion equations with strong reaction terms, resulting in that numerical schemes easily become unstable. We present a formulation that stresses on the robustness of the solution method, tackling common problems that produce instability. The main contribution concerns the loss of positivity of κ and ε, which is addressed by acting on the coefficients of the reaction and diffusion terms rather than on the turbulent variables themselves. In addition, a linearized implicit, non-iterative, treatment of the wall law is proposed.     

Minimum principle of complementary energy of cable networks by using second-order cone programming

The minimum principle of complementary energy is established for cable networks involving only stress components as variables in geometrically nonlinear elasticity. It is rather amazing that the complementary energy always attains minimum value at the equilibrium state irrespective of the stability of cable networks, contrary to the fact that only the stationary principles have been presented for elastic trusses and continua even in the case of stable equilibrium state. In order to show the strong duality between the minimization problems of total potential energy and complementary energy, the convex formulations of these problems are investigated, which can be embedded into a primal–dual pair of second-order cone programming problems. The existence and uniqueness of solution are also investigated for the minimization problem of complementary energy.     

Reduced projection augmented Lagrange bi-conjugate gradient method for contact and impact problems

Based on the numerical governing formulation and non-linear complementary conditions of contact and impact problems,a reduced projection augmented Lagrange bi- conjugate gradient method is proposed for contact and impact problems by translating non-linear complementary conditions into equivalent formulation of non-linear program- ming.For contact-impact problems,a larger time-step can be adopted arriving at numer- ical convergence compared with penalty method.By establishment of the impact-contact formulations which are equivalent with original non-linear complementary conditions,a reduced projection augmented Lagrange bi-conjugate gradient method is deduced to im- prove precision and efficiency of numerical solutions.A numerical example shows that the algorithm we suggested is valid and exact.     

材料弹塑性性能数值模拟的多尺度方法

将均匀化方法和渐近分析(Asymptotic Analysis)与参变量变分原理相结合提出了一种模拟复合材料非线性性能的多尺度数值方法.该方法用渐近分析建立宏-细观变量之间的联系,利用参变量变分原理计算非线性响应,求解过程采用迭代算法.为提高计算精度,针对Von-Mises准则和Tsai-Hill准则,提出了一个基于参变量变分原理的改进算法,算例表明该方法可以显著消除传统方法采用线性展开式构造线性互补条件所带来的误差.     

The application of 2D base force element method (BFEM) to geometrically non-linear analysis

Based on the concept of the base forces by Gao, a new finite element method – the base force element method (BFEM) on complementary energy principle for two-dimensional geometrically non-linear problems is presented. A 4-mid-node plane element model of the BFEM for geometrically non-linear problem is derived by assuming that the stress is uniformly distributed on each sides of a plane element. The explicit formulations of the control equations for the BFEM are derived using the modified complementary energy principle. The BFEM is naturally universal for small displacement and large displacement problems. A number of example problems are solved using the BFEM and the results are compared with corresponding analytical solutions and those obtained from the standard displacement finite element method. A good agreement of the results, and better performance of the BFEM, compared to the displacement model, in the large displacement and large rotation calculations, is observed.     

FINITE ELEMENT ANALYSIS FOR CONSOLIDATION IN INTERACTION BETWEEN STRUCTURE AND SATURATED SOIL FOUNDATION

The consolidation analysis of interaction between structure and saturated soil foundation is discussed. With the use of substructure technique, the structure is condensed onto the interface of the soil, and then the consolidation governing equations to describe the interaction between soil and structure are derived, The solution with non-iterative algorithm is proposed in this paper. The pressure Master-Slave relation method is used to deal with the non-permeability conditions on soil boundaries. A numerical example is illustrated. Based on this paper, the interactive consolidation analysis between large structure and soil has been more practical.     

Efficient implicit algorithm for the equations of 2-D viscous compressible flow: application to shock-boundary layer interaction

A fully implicit algorithm has been developed to time integrate the equations of 2-D compressible viscous flow. The algorithm was constructed so as to optimize computational efficiency. The time-consuming block matrix inversions usually associated with implicit algorithms have been reduced to the trivial non-iterative inversion of four sets of scalar bidiagonal matrices. Thus, the algorithm requires virtually no more computer storage than an explicit algorithm. The efficient structure of the implicit algorithm is reflected in comparative timings which slow that it requires only a factor of two more computer time per point per time step than a typical explicit algorithm. Therefore, the algorithm allows more economical solution of given flows than existing explicit methods and also allows more difficult problems to be attempted using available computer resources. Application of the algorithm to the problem of shock-boundary layer interaction produces results consistent with both experimental measurements and other calculations.