二维非结构网格有限体积格式的壁热现象和人工热流方法

基于Noh人工热流方法的思想,推导出任意多边形网格人工热流的格式,将Noh的结构网格人工热流方法推广到任意多边形非结构网格的拉氏有限体积方法中,抑制或消除了壁热现象.几个数值实验,包括Noh激波反射问题和两块钢金属碰撞问题,验证了方法的可行性.     

飞机构型Euler绕流结构网格方法计算的可信度

采用三种方法验证飞机构型Ｅｕｌｅｒ绕流结构网格方法计算。第一,同一网格,采用不同的方法或程序进行计算,采用Ｊａｍｅｓｏｎ中心差分有限体积方法和Ｓｔｅｇｅｒ－Ｗａｒｍｉｎｇ流量分裂迎风格式有限体积方法,为计算提供容错手段;第二,网格细化和网格点重新分布,并通过网格收敛指标进行评估;第三,提出新的多块拼接网格拓朴,采用不同的网格拓扑进行计算。     

飞机构型Euler绕流结构网格方法计算的可信度

采用三种方法验证飞机构型Euler绕流结构网格方法计算。第一,同一网格,采用不同的方甚或程序进行计算;采用Jameson中心差分有限体积方法和Steger-warming流量分裂迎风格式有限体积方法,为计算提供容错手段;第二,网格细化和网格点重新分布,并通过网格收敛指标进行评估;第三,提出新的多块拼接网格拓扑,采用不同的网格拓扑进行计算。     

惯性约束聚变内爆中基于多块结构网格的高效辐射扩散并行算法

针对三维球形靶丸内爆高效模拟需求和传统笛卡尔正交网格上辐射加源困难的问题, 发展一种多块结构非正交网格生成方法, 并基于此种计算网格提出高效的三维扩散格式并行算法, 将其应用于辐射流体方程组的求解和三维内爆不对称性的数值模拟, 数值结果显示了算法的有效性。并行性能测试显示该算法可扩展到5400个核上, 并行效率达到69%。     

非结构网格上的B-B单方程模型湍流计算

研究如何在非结构网格上进行Navier Stokes(N-S)方程湍流计算.采用格心有限体积方法离散N-S方程.为了适应非结构网格,计算所用的湍流模型特别选用Baldwin Barth(B-B)单方程模型.此模型由一个单一的具有源项的对流扩散方程组成.为了能在非结构网格上求解B B单方程模型,提出一显式有限体积格式,并直接对带源项的格式进行稳定性分析,得到了相应的时间步长限制条件.最后以平板、RAE 2822翼型、多段翼型绕流等数值算例验证了计算方法的有效性.     

三维非结构网格Euler方程的LU-SGS算法及其改进

将LU-SGS隐式时间推进格式运用到非结构网格Euler方程的求解中,并对传统LU-SGS格式进行改进,结合网格重排序,发展了一套效率更高的三维Euler方程求解器.以M6机翼及超临界LANN机翼的跨音速无粘流场为算例,将改进LU-SGS格式与四步龙格-库塔显式格式及传统LU-SGS格式进行了比较.计算结果表明:所有格式的计算结果与实验结果都符合很好;传统LU-SGS格式计算效率为显式格式的3倍多,而改进LU-SGS格式计算效率为显式格式的7倍多.     

多点择优推进阵面法生成曲面三角形网格

在现有曲面非结构网格生成法的基础上,提出了一种新的曲面网格生成法——多点择优推进阵面法.它可在曲面上直接进行三角形网格划分,克服了映射法的网格变形问题,并且可以在网格生成结束后,对曲面网格直接进行Laplace格点松弛光顺.该方法使用简单,不受曲面块类型的限制,且网格质量高,可以为三维非结构网格生成提供高质量的初始阵面,并给出了若干个算例.     

BGK方法在三维非结构网格上的初步应用

将BGK计算方法从二维拓展到三维并且应用于三维非结构网格,具有重要的理论价值和实用价值.采用旋转局部座标的方法,发展了一种针对三维非结构网格的BGK计算方法.在计算过程中,将最小二乘法应用于三维非结构网格的导数计算.对三维激波管和三维欠膨胀垂直冲击射流等两个算例进行了细致分析.这两个算例的计算结果表明,该方法在三维非结构网格上的初步应用是成功的 关键词： 气动BGK方法 三维 非结构网格     

加权ENO格式的构造及数值模拟

将加权ENO格式推广到非结构三角形网格上,构造了一类加权ENO有限体积格式,提出的插值多项式的构造方式,可以减少计算时间.对于出现的病态方程组,给出了解决方法.此外还给出了插值点的选取方式及加权因子的构造方法.结合三阶TVD Runge Kutta时间离散,对二维欧拉方程组进行了数值试验.     

黏性激波管的有限体积WENO格式数值模拟

本文采用OpenFOAM软件下实现的一种可实现任意阶数,可应用于非结构网格的有限体积WENO格式对黏性激波管问题进行模拟。模拟中对流项离散采用3阶精度、4阶精度该类WENO格式,网格形式采用结构网格和三角形非结构网格。结果表明,采用该类格式,三角形非结构网格的算精度、效率优于结构网格,3阶精度格式计算效率优于4阶精度。该工作表明OpenFOAM下采用3阶精度该类格式及非结构网格对叶轮机械内部流动等复杂流场的模拟更具优势与应用潜力.     

A multi-block ADI finite-volume method for incompressible Navier–Stokes equations in complex geometries

An efficient second-order accurate finite-volume method is developed for a solution of the incompressible Navier–Stokes equations on complex multi-block structured curvilinear grids. Unlike in the finite-volume or finite-difference-based alternating-direction-implicit (ADI) methods, where factorization of the coordinate transformed governing equations is performed along generalized coordinate directions, in the proposed method, the discretized Cartesian form Navier–Stokes equations are factored along curvilinear grid lines. The new ADI finite-volume method is also extended for simulations on multi-block structured curvilinear grids with which complex geometries can be efficiently resolved. The numerical method is first developed for an unsteady convection–diffusion equation, then is extended for the incompressible Navier–Stokes equations. The order of accuracy and stability characteristics of the present method are analyzed in simulations of an unsteady convection–diffusion problem, decaying vortices, flow in a lid-driven cavity, flow over a circular cylinder, and turbulent flow through a planar channel. Numerical solutions predicted by the proposed ADI finite-volume method are found to be in good agreement with experimental and other numerical data, while the solutions are obtained at much lower computational cost than those required by other iterative methods without factorization. For a simulation on a grid with O(10⁵) cells, the computational time required by the present ADI-based method for a solution of momentum equations is found to be less than 20% of that required by a method employing a biconjugate-gradient-stabilized scheme.     

Stabilized seventh-order dissipative compact scheme for two-dimensional Euler equations

We derive in this paper a time stable seventh-order dissipative compact finite difference scheme with simultaneous approximation terms(SATs) for solving two-dimensional Euler equations. To stabilize the scheme, the choice of penalty coefficients for SATs is studied in detail. It is demonstrated that the derived scheme is quite suitable for multi-block problems with different spacial steps. The implementation of the scheme for the case with curvilinear grids is also discussed.Numerical experiments show that the proposed scheme is stable and achieves the design seventh-order convergence rate.     

Numerical simulation of wave effects around compound coastal structures

A new three-dimensional potential flow numerical method has been developed to study wave diffraction around compound coastal structures. This new method is based on a multi-block finiteanalytic scheme. A chimera domain decomposition technique is used to model complex geometry and to connect overlapped grids by interpolating information across block boundaries. Calculations were performed for three examples, including a harbor entrance, a single breakwater, and a combined breakwater and large floating platform, to illustrate the flexibility and effectiveness of the present method.     

结构型网格分块生成技术

构造了一种适用于模拟具有复杂几何特征的流动问题的结构型网格生成方法,该方法应用CAD技术中非均匀有理B样条(NURBS)曲面表达形式,根据给定物体的典型站位截面,首先对物体进行分片表面网格的构造与重构,同时根据物体几何特征及流场特性对绕流流场进行区域分解并构造其块边界,在此基础上再采用数值方法进行相应的分块网格生成,并给出了应用所建立的方法生成的几种天地往返运输系统流场网格.     

Relativistic Feynman-type integrals

It is shown that within the framework of the Kershaw stochastic model generalized by the author to the relativistic case a Feynman-type process may be constructed which can formally be understood as a diffusion phenomenon in Euclidean space. This makes it possible to introduce a real probability measure in the scheme of quantum mechanics proposed by Feynman.     

高超声速层流绕三维压缩拐角的数值模拟

通过数值模拟研究了高超声速来流绕过压缩拐角的层流分离三维流动特性.数值方法采用三维N-S方程,结合2阶精度Roe格式以及分区结构网格有限体积法进行离散.数值模拟的空间激波结构与实验纹影结果符合较好;激波/边界层干扰区内3条纵向线上的计算压力分布与实验结果进行了对比分析,计算获得在三维楔侧面存在低压力区,与实验结果反映的规律一致,计算结果表明低压力区是由楔体侧缘尖端发起的二次涡的抽吸作用造成的.此外,在楔体后端尾流区的低压沿边界层内的亚声速区往上游传递了一定距离.      

A high-resolution gas-kinetic scheme with minimized dispersion and controllable dissipation reconstruction

In order to simulate multiscale problems such as turbulent flows effectively, the high-order accurate reconstruction based on mini- mized dispersion and controllable dissipation (MDCD) is implemented in the second-order accurate gas-kinetic scheme (GKS) to improve the accuracy and resolution. MDCD is firstly extended to non-uniform grids through the modification of dissipation and dispersion coefficients for uniform grids based on the local stretch ratio. Remarkable improvements in accuracy and resolution are achieved on general grids. Then a new scheme, MDCD-GKS is constructed, with the help of MDCD reconstruction, not only for conservative variables, but also for their gradients. MDCD-GKS shows good accuracy and efficiency in typical numerical tests. MDCD-GKS is also coupled with the improved delayed detached-eddy simulation (IDDES) hybrid model and applied in the fine simulation of turbulent flow around a cylinder, and the prediction is in good agreement with experiments when using the relatively coarse grid. The high accuracy and resolution of the developed GKS guarantee its high efficiency in practical applications.     

各向异性扩散问题Kershaw格式的守恒保正修复算法

针对各向异性扩散方程Kershaw格式的数值解在正交网格及扭曲网格上计算出负的现象,给出一种守恒的保正修复算法（CENZ）,该算法对简单遇负置零（ENZ）方法进行改进,使修复后的数值解不仅具有非负性,而且保持法向通量的局部守恒性.数值算例表明,该方法不受计算网格类型和扩散系数各向异性比的限制,可用于对任意违背单调性（或保正性）的有限体积格式数值解的修复.     

四阶紧致差分格式对静力模式中垂直网格计算频散性的影响

为了说明四阶紧致差分格式在大气和海洋数值模式中的潜在价值,提出一种通用方法,推导静力线性斜压适应方程组在微分和差分情况下的频散关系,水平尺度分100 km,10 km和1 km三种情况,从频率、水平群速和垂直群速方面,对采用二阶中央差和四阶紧致差分格式情况下,非跳点网格(N网格)、Lorenz网格(L网格)、Charney-Phillips网格(CP网格)、Lorenz时间跳点网格(LTS网格)和Charney-Phillips时间跳点网格(CPTS网格)的计算特性进行比较,发现采用高精度的四阶紧致差分格式总体上可以明显减少上述三种水平尺度波动在N网格、CP网格、L网格和CPTS网格上的频率、水平群速和垂直群速误差,但对LTS网格,采用四阶紧致差分格式,会使得计算水平群速和垂直群速误差变大.