推进－迭代算法计算效率的研究

本文对求解三维定常超音速动性流场的一次空间推进，在每一个推进站沿伪时间层局部迭代的推进－迭代算法作了进一步的研究．在每一推进站（侧向平面）沿伪时间层局部迭代时，给出了四种不同的隐式迭代方法，即沿侧面两个方向（法向和周向）全用隐式；法向隐式而周向采用Ｇａｕｓｓ－Ｓｉｌｄｌｅ来回扫描迭代；法向隐式而周向显式及以系数矩阵谱半径代替系数矩阵的简化标量隐式算法．用这四种算法模拟了三维球锥黏性绕流，给出了四种不同算法的计算效率和收敛特性比较．     

树形多体系统动力学的隐式数值算法

研究了树形多体系统动力学的隐式算法．用矩阵形式给出了多体系统的正则方程及其右端函数的Ｊａｃｏｂｉ矩阵，并给出该矩阵的分块算法和对角隐式Ｒｕｎｇｅ－Ｋｕｔａ法（ＤＩＲＫＭ）以及隐式辛Ｒｕｎｇｅ－Ｋｕｔａ法（ＩＳＲＫＭ）．该算法便于编程计算，能提高计算效率，保持长期计算的稳定性．并用算例说明该算法的有效性     

结构性软土弹塑性模型的隐式算法实现

对于考虑软土结构性的高度非线性弹塑性本构模型,在采用Newton-CPPM隐式算法对模型进行数值实现的过程中容易出现Jacobian矩阵奇异和不收敛问题。为此,本文提出了两种改进隐式算法。考虑到Newton-CPPM隐式算法是局部收敛性算法,因此引入大范围收敛的同伦延拓算法对Newton-CPPM算法的迭代初值进行改进,形成了同伦-Newton-CPPM算法。考虑到Newton-CPPM隐式算法单个迭代步的计算量过大,因此借鉴显式算法的思想提出一种两阶段迭代算法,第一阶段先求出一致性参数,第二阶段采用类似于显示算法的方法进行回代得出状态变量的值。然后,以考虑软土结构性的SANICLAY模型为例,从弹塑性本构模型的组成和算法的特点两个角度分析了引起Jacobian矩阵奇异和不收敛问题的原因,并且在单单元计算的基础上,对全显式算法、传统隐式算法和两种改进隐式算法在计算收敛性、计算精度和计算效率方面进行了对比。最后,将同伦-Newton-CPPM算法和传统隐式算法用于地基承载力多单元计算中,结果表明该算法能够有效地解决Jacobian矩阵奇异和不收敛问题。      

带约束多体系统动力学方程的隐式算法

研究了带约束多体系统隐式算法,用子矩阵的形式推导出了多体系统正则方程的Ｊａｃｏｂｉ矩阵,它适用于多种隐式算法并给出了隐式Ｒｕｎｇｅ－Ｋｕｔｔａ算法,最后用一算例表明了隐式算法的计算效率和精度明显优于算法。     

高阶紧致格式求解二维粘性不可压缩复杂流场

提出了一种求解二维不可压缩复杂流场的高精度算法．控制方程为原始变量、压力Ｐｏｉｓｓｏｎ方程提法．在任意曲线坐标下，采用四阶紧致格式求解Ｎａｖｉｅｒ－Ｓｔｏｋｅｓ方程组，时间推进采用交替方向隐式（ＡＤＩ）格式，在非交错网格上用松弛法求解压力Ｐｏｉｓｓｏｎ方程．对于复杂的流场，采用了区域分解方法，并在每一时间步对各子域实施松弛迭代使之能精确地反映非定常流场．利用该算法计算了二维受驱空腔流动，弯管流动和垂直平板的突然起动问题．计算结果与实验结果和其他研究者的计算结果相比较吻合良好．对于平板起动流动，成功地模拟了流场中旋涡的生成以及Ｋａｒｍａｎ涡街的形成     

蠕变—弹塑性—损伤耦合响应的有限元分析

本文处理各向异性非线性材料的蠕变－弹塑性－损伤耦合响应的数值计算。建议了一个计算应力的三维向后欧拉积分处，导出一个利用Ｎｅｗｔｏｎ－Ｒａｐｈｓｏｎ迭代的一般的直接应力返回映射算法。同时求解应力向量和里面变、塑性、损伤的内状态变量。也导出了用于全局Ｎｅｗｔｏｎ－Ｒａｐｈｓｏｎ迭代过程的一致性切线矩阵公式。给出的数值例题结果表明所提出的算法和公式在模拟耦合本构行为上的能力和可靠性。     

蠕变－弹塑性－损伤耦合响应的有限元分析

本文处理各向异性非线性材料的蠕变。弹塑性－损伤耦合响应的数值计算。建议了一个计算应力的三级向后欧拉积分算法。导出了一个利用Ｎｅｗｔｏｎ－Ｒａｐｈｓｏｎ迭代的一般的直接应力返回映射算法。同时求解应力向量和蠕变、塑性、损伤的内状态变量。也导出了用于全局Ｎｅｗｔｏｎ－Ｒａｐｈ－ｓｏｎ迭代过程的一致性切线矩阵公式。给出的数值例题结果表明所提出的算法和公式在模拟耦合本构行为上的能力和可靠性。     

带约束平面多刚体系统动力学方程的隐式算法

在多体系统动力学正则方程的基础上建立了平面多体系统正则方程的隐式数值算法。利用平面运动的特性，对正则方程进行了简化，导出了该方程的Ｊａｃｏｂｉ矩阵的一般表达式，给出了Ｒｕｎｇｅ－Ｋｕｔａ多体系统动力学方程隐式数值计算方法。算例表明，该方法是一种计算速度和精度均理想的数值方法。     

近似平衡多项式加速度动力显式算法

利用已知初始时刻的信息，建立一种可以取到任意阶高精度的多项式加速度单步隐式算法。在该隐式方法中，待采解方程纽系数矩阵中质量阵的系数远远大于阻尼阵和剐度阵的系数，略去非对角阻尼阵和非对角刚度阵对方程组的影响，得到一种近似平衡多项式加速度动力显式计算方法。此方法的精度主要由加速度多项式插值的项数、步长、质量阵的每件数、质量刚度比（质量阵和刚度阵的范数之比）决定。在此基础上给出了这种算法的通式，进行了精度分析，结果表明：如果时间步长h足够短，n次加速度近似平衡动力显式算法的精度可以达到O（hn＋1）。算例采用5次加速度近似平衡显式算法，计算结果的精确性证明了本算法的可行性。     

层合圆柱厚壳热应力分析的状态方程及其半解析法

通过对Ｈｅｌｌｉｎｇｅｒ－Ｒｅｉｓｓｎｅｒ变分原理的修正，导出了变温作用下层合圆柱厚壳的状态方程及其半解析法，该方法在ｚ－θ曲面内采用通常的有限元离散，而沿壳厚（ｒ）方向采用状态空间法给出解析解答，且通过采用状态转移矩阵，建立了层合圆柱壳内外表面应力和位移之间的关系式，然后利用打靶法进行求解，从而大大降低了计算中的未知量数目。     

壁面湍流发卡涡包空间模态的TRPIV实验研究

运用高时间分辨率粒子图像测速(Time-resolved PIV简称TRPIV),测量得到平板湍流边界层流向/法向平面内瞬时速度矢量空间分布的时间序列;采用空间局部平均速度结构函数的概念,识别和提取湍流边界层中大尺度发卡涡包结构的空间特征。发现在湍流边界层中不同法向位置多个正负发卡涡包结构同时交替存在。这些分布在不同法向高度的发卡涡包结构之间通过倾斜的涡量剪切层相联系,构成了湍流边界层中内、外区紧密相连、相互作用的一种稳态的分布方式。     

利用有限元构造Michell桁架的一种方法

提出了一种新的形成Michell桁架的有限元分析方法.该方法以纤维增强正交各向异性复合板为材料模型,根据有限元分析结果调整各单元的纤维密度和方向.采用所提出的一种迭代格式,经过少量迭代,形成满足Michell准则的应变、内力场.该方法适于不同几何形状、支撑条件及荷载情况.算例结果表明该方法是有效的.     

A mass‐conservative staggered immersed boundary model for solving the shallow water equations on complex geometries

In this work, an approach is proposed for solving the 3D shallow water equations with embedded boundaries that are not aligned with the underlying horizontal Cartesian grid. A hybrid cut‐cell/ghost‐cell method is used together with a direction‐splitting implicit solver: Ghost cells are used for the momentum equations in order to prescribe the correct boundary condition at the immersed boundary, while cut cells are used in the continuity equation in order to conserve mass. The resulting scheme is robust, does not suffer any time step limitation for small cut cells, and conserves fluid mass up to machine precision. Moreover, the solver displays a second‐order spatial accuracy, both globally and locally. Comparisons with analytical solutions and reference numerical solutions on curvilinear grids confirm the quality of the method. Copyright © 2015 John Wiley & Sons, Ltd.     

Efficient ADI and spline ADI methods for the steady-state Navier-Stokes equations

The present paper provides an improved alternating direction implicit (ADI) technique as well as high-order-accurate spline ADI method for the numerical solution of steady two-dimensional incompressible viscous flow problems. The vorticity-stream function Navier-Stokes equations are considered in a general curvilinear coordinate system, which maps an arbitrary two-dimensional flow domain in the physical plane into a rectangle in the computational plane. The stream function equation is parabolized in time by means of a relaxation-like time derivative and the steady state solution is obtained by a time-marching ADI method requiring to solve only 2 × 2 block-tridiagonal linear systems. The difference equations are written in incremental form; upwind differences are used for the incremental variables, for stability, whereas central differences approximate the non-incremental terms, for accuracy, so that, at convergence, the solution is free of numerical viscosity and second-order accurate. The high-order-accurate spline ADI technique proceeds in the same manner; in addition, at the end of each two-sweep ADI cycle, the solution is corrected by means of a fifth-order spline interpolating polynomial along each row and column of the computational grid, explicitly. The validity and the efficiency of the present methods are demonstrated by means of three test problems.     

Numerical simulation analysis for migration-accumulation of oil and water

ＩｎｔｒｏｄｕｃｔｉｏｎＴｈｅｎｕｍｅｒｉｃａｌｓｉｍｕｌａｔｉｏｎｏｆｔｈｅｅｖｏｌｕｔｉｏｎａｒｙｈｉｓｔｏｒｙｏｆｔｈｅｂａｓｉｎｉｓｃｏｎｄｕｃｔｅｄａｃｏｒｄｉｎｇｔｏｔｈｅｍｅｃｈａｎｉｓｍｏｆｐｅｔｒｏｌｅｕｍｇｅｏｌｏｇｙａｎｄｍｅｃ...     

On unconditionally positive implicit time integration for the DG scheme applied to shallow water flows

We present a new unconditionally positivity‐preserving (PP) implicit time integration method for the DG scheme applied to shallow water flows. This novel time discretization enhances the currently used PP DG schemes, because in the majority of previous work, explicit time stepping is implemented to deal with wetting and drying. However, for explicit time integration, linear stability requires very small time steps. Especially for locally refined grids, the stiff system resulting from space discretization makes implicit or partially implicit time stepping absolutely necessary. As implicit schemes require a lot of computational time solving large systems of nonlinear equations, a much larger time step is necessary to beat explicit time stepping in terms of CPU time. Unfortunately, the current PP implicit schemes are subject to time step restrictions due to a so‐called strong stability preserving constraint. In this work, we hence give a novel approach to positivity preservation including its theoretical background. The new technique is based on the so‐called Patankar trick and guarantees non‐negativity of the water height for any time step size while still preserving conservativity. In the DG context, we prove consistency of the discretization as well as a truncation error of the third order away from the wet–dry transition. Because of the proposed modification, the implicit scheme can take full advantage of larger time steps and is able to beat explicit time stepping in terms of CPU time. The performance and accuracy of this new method are studied for several classical test cases. Copyright © 2014 John Wiley & Sons, Ltd.     

风沙两相流跃移层中沙粒相的速度分布

从单个跃移沙粒在气流中的运动方程出发导出了风沙两相流中沙粒相速度分布函数的Boltzmann方程，对风沙流研究中几种不同的分布函数及其相应的统计平均值等基本概念给出了严密的数学定义，指出了不同分布函数之间的区别和联系，在略去铅垂方向空气阻力的情况下，给出了沙粒相速度分布函数沿铅垂方向的边缘分布，作为风沙流中跃移理论的主要基础之一。利用结果对前人在风沙流研究中发现的某些重要规律和现象进行了解释。     

Symmetry of Ground States of p‐Laplace Equations via the Moving Plane Method

. In this paper we use the moving plane method to get the radial symmetry about a point of the positive ground state solutions of the equation in , in the case . We assume f to be locally Lipschitz continuous in and nonincreasing near zero but we do not require any hypothesis on the critical set of the solution. To apply the moving plane method we first prove a weak comparison theorem for solutions of differential inequalities in unbounded domains. (Accepted September 21, 1998)     

Spatial Evolution of Nonstationary Perturbations in Hamel Flow

The propagation of small perturbations in longitudinally inhomogeneous flows is investigated. The evolution of the perturbations is studied with reference to the radial flow of a viscous incompressible fluid between plane nonparallel walls, the simplest inhomogeneous flow. Using a generalized method of variation of constants, the corresponding boundary-value problem is reduced to an infinite-dimensional evolutionary system of ordinary differential equations for the complex amplitudes of the eigensolutions of a locally homogeneous problem. Physically, the method can be interpreted as a representation of the perturbation evolution process via two concomitant processes: the independent amplification (attenuation) of normal modes of the locally homogeneous problem and the rescattering of these modes into each other on local inhomogeneities of the base flow. The calculations show that reduced versions of the method are promising for describing the linear stage of laminar-turbulent transition in a boundary layer.