一种基于TV分裂的真正多维Riemann解法器

给出了一种真正多维的HLL Riemann解法器.采用TV(Toro-Vázquez)分裂将通量分裂成对流通量和压力通量,其中对流通量的计算采用类似于AUSM格式的迎风方法,压力通量的计算采用波速基于压力系统特征值的HLL格式,并将HLL格式耗散项中的密度差用压力差代替,来克服传统的HLL格式不能分辨接触间断的缺点.为了实现数值格式真正多维的特性,分别计算网格界面中点和角点上的数值通量,并且采用Simpson公式加权中点和角点上的数值通量来得到网格界面上的数值通量.采用基于SDWLS(solution dependent weighted least squares)梯度的线性重构来获得空间的二阶精度,时间离散采用二阶Runge-Kutta格式.数值实验表明,相比于传统的一维HLL格式,该文的真正多维HLL格式具有能够分辨接触间断,消除慢行激波波后振荡以及更大的时间步长等优点.并且,与其他能够分辨接触间断的格式（例如HLLC格式）不同的是,真正多维的HLL格式在计算二维问题时不会出现数值激波不稳定现象.     

基于AUSM分裂的二维通量分裂格式

基于对流迎风分裂思想构造的AUSM类格式具有简单、高效、分辨率高等优点,在计算流体力学中得到了广泛的应用.传统的AUSM类格式在计算界面数值通量时只考虑网格界面法向的波系,忽略了网格界面横向波系的影响.使用Liou-Steffen通量分裂方法将二维Euler方程的通量分裂成对流通量和压力通量,采用AUSM格式来分别计算对流数值通量和压力数值通量.通过求解考虑了横向波系影响的角点数值通量来构造一种真正二维的AUSM通量分裂格式.在计算一维算例时,该格式保留了精确捕捉激波和接触间断的优点.在计算二维算例时,该格式不仅具有更高的分辨率而且表现出更好的鲁棒性,可以消除强激波波后的不稳定现象.此外,在多维问题的数值模拟中,该格式大大地提高了稳定性CFL数,具有更高的计算效率.因此,它是一种精确、高效并且强鲁棒性的数值方法.     

关于高阶精度WCNS格式的无粘通量分裂方法

高阶精度加权紧致非线性格式(WCNS)越来越广泛地应用于复杂流动数值模拟.WCNS可以与多种无粘通量分裂方法结合起来使用.但是,常见的通量分裂方法都是基于低阶格式发展起来的,目前还不清楚哪些通量分裂方法最适合WCNS,也不知道这些方法与高阶格式结合时将会产生什么效果.表面热流计算是高超声速流动数值模拟的难点之一,为了在热流计算时选择合适的通量,研究了多种通量分裂方法的耗散大小.每种通量都可以表示成中心部分与耗散部分之和.这些通量的中心部分相同且非常简单,但是耗散部分较为复杂,且不同的通量分裂方法可导致不同的耗散表达式.通过对通量耗散进行分析可以发现耗散大小与网格界面两侧的物理量跳跃近似线性正相关.数值计算表明高阶格式得到的网格界面左右两侧的物理量跳跃通常远比低阶格式小,因而带来的通量耗散小.通过3个典型算例考察了通量耗散对热流计算的影响,其中包括高超激波/边界层干扰算例.基于对van Leer通量、Steger-Warming通量、KFVS通量、Roe通量、AUSM类通量和HLL类通量的考察,给出了通量选择建议.     

关于高阶精度WCNS格式的无粘通量分裂方法（英文）

高阶精度加权紧致非线性格式(WCNS)越来越广泛地应用于复杂流动数值模拟.WCNS可以与多种无粘通量分裂方法结合起来使用.但是,常见的通量分裂方法都是基于低阶格式发展起来的,目前还不清楚哪些通量分裂方法最适合WCNS,也不知道这些方法与高阶格式结合时将会产生什么效果.表面热流计算是高超声速流动数值模拟的难点之一,为了在热流计算时选择合适的通量,研究了多种通量分裂方法的耗散大小.每种通量都可以表示成中心部分与耗散部分之和.这些通量的中心部分相同且非常简单,但是耗散部分较为复杂,且不同的通量分裂方法可导致不同的耗散表达式.通过对通量耗散进行分析可以发现耗散大小与网格界面两侧的物理量跳跃近似线性正相关.数值计算表明高阶格式得到的网格界面左右两侧的物理量跳跃通常远比低阶格式小,因而带来的通量耗散小.通过3个典型算例考察了通量耗散对热流计算的影响,其中包括高超激波/边界层干扰算例.基于对van Leer通量、Steger-Warming通量、KFVS通量、Roe通量、AUSM类通量和HLL类通量的考察,给出了通量选择建议.     

一种治愈强激波数值不稳定性的混合方法

HLLC（Harten-Lax-Leer-contact）格式是一种高分辨率格式,能够准确捕捉激波、接触间断和稀疏波.但是使用HLLC格式计算多维问题时,在强激波附近会出现激波不稳定现象.FORCE（first-order centred）格式在强激波附近表现出很好的稳定性,并且其数值耗散比HLL（Harten-Lax-Leer）格式小.分析了HLLC格式和FORCE格式在特定流动条件下的稳定性,构造了HLLC-FORCE混合格式并且进一步结合开关函数来消除HLLC格式的激波不稳定现象.数值试验表明新构造的混合格式不仅能够消除HLLC格式的激波不稳定现象,还最大程度地保留HLLC格式高分辨率的优点.     

求解二维Euler方程的旋转通量混合格式

为提高求解二维Euler方程数值结果的分辨率,提出了一种旋转通量混合格式.该算法采用旋转通量法的类一维处理思想,通量函数选用满足热力学第二定律的熵稳定数值通量和具有良好鲁棒性的HLL数值通量耦合的混合格式,时间方向采用三阶强稳定Runge-Kutta方法进行推进.该旋转通量混合格式具有结构简单、分辨率高的优点,数值结果表明了该算法的良好特性.     

一维气液两相漂移模型的AUSMV算法研究

将AUSMV(advection upstream splitting method V)格式从计算气体动力学问题扩展至一维等温瞬态气液两相管流.阐述了采用AUSMV格式构建气液两相漂移模型数值通量的方法及边界单元的处理方法.采用Runge Kutta方法与经典的保单调MUSCL(monotone upstream centred schemes for conservation laws)方法结合Van Leer限制器,构建具有二阶时间和空间精度的数值计算方法.计算经典Zuber-Findlay激波管问题和复杂漂移关系变质量流动问题并与可靠的参考结果进行了对比.分析表明:AUSMV格式应用于气液两相流动漂移模型时计算效率高、精度高、耗散效应和色散效应小,低流速条件下能够精确地描述间断.     

一种改进的Roe格式及其稳定性分析

低耗散的激波捕捉方法,包括流行的Roe格式,在计算多维强激波问题时会遭遇激波不稳定现象的困扰,这会严重影响格式对于高超声速流动问题的精确模拟.对Roe格式进行小扰动分析,结果表明:激波面纵向所有物理量的扰动均会衰减,而横向的密度扰动和剪切速度扰动不会衰减.在横向数值通量上增加与熵波和剪切波相对应的黏性来抑制Roe格式不稳定现象的发生.为了防止不合适的黏性影响格式对于接触间断和剪切层的分辨率,定义两个开关函数,使得黏性仅仅添加在激波层亚声速区的横向数值通量上.数值测试的结果表明:改进的Roe格式不仅保留了原始Roe格式高分辨率的优点,而且具有更好的鲁棒性,消除了激波不稳定现象.     

A Well-Balanced HLL Scheme for Hyperbolic Conservation Systems With Source Terms北大核心CSCD

针对含源项的双曲守恒方程给出了一种新的有限体积格式.经典的有限体积格式不能正确地模拟对流通量项和外力之间的平衡所产生的动力学问题.为解决这个问题,仿照经典的HLL近似Riemann求解器设计思路设计了含源项的近似Riemann求解器.针对含重力源项的一维流体Euler方程和理想磁流体方程,通过对通量计算格式的修正得到了保平衡HLL格式（WB-HLL）,并给出了保平衡的证明.针对一维Euler方程和理想磁流体给出了两个算例,比较了传统HLL格式和提出的WB-HLL格式的计算精度.计算结果表明,WB-HLL格式精度更高,收敛更快.     

求解双曲守恒律方程的三阶修正模板WENO格式北大核心CSCD

为了降低经典的三阶加权本质无振荡(WENO)格式的数值耗散,提出了一种新的三阶WENO格式的修正模板近似方法.改进了经典WENO-JS格式中各候选模板上数值通量的一阶多项式逼近,通过加入二次项使模板逼近达到三阶精度.计算了相应的候选通量,并且通过引入可调函数φ(x),使得新的格式具有ENO性质.最后给出了一系列数值算例,证明了该方法的有效性.     

一维气液两相漂移模型全隐式AUSMV算法研究

气液两相漂移模型显式AUSMV（advection upstream splitting method combined with flux vector splitting method）算法的时间步长受限于CFL（Courant-Friedrichs-Lewy）条件，为了提高计算效率，建立了一种全隐式AUSMV算法求解气液两相漂移模型.采用AUSM格式结合FVS（flux vector splitting）格式构造连续方程和运动方程的对流项数值通量，AUSM格式构造压力项数值通量.离散控制方程是非线性方程组，采用六阶Newton(牛顿)法结合数值Jacobi矩阵求解.计算经典算例Zuber-Findlay激波管问题和复杂漂移关系变质量流动问题，结果分析表明:全隐式AUSMV算法，色散效应小，无数值震荡，计算精度高.在压力波波速高的条件下，可以显著提高计算效率，耗散效应小.     

A shock-capturing model based on flux-vector splitting method in boundary-fitted curvilinear coordinates

In this paper, a robust and accurate high-resolution finite-volume scheme is presented which employs flux-vector splitting (FVS) as the building block for solution of shallow water equations in boundary-fitted curvilinear coordinates. Eddy viscosity approach is used to accommodate shear stresses due to turbulence. Splitting of the convective terms is achieved via flux Jacobians whereas Liou–Steffen Splitting (LSS) technique, but in transformed coordinates, is used to split pressure terms. Limited flux gradients are also used to increase the computational accuracy of evaluation of interface fluxes and decrease the excessive numerical dissipation associated with FVS. This will completely remove spurious oscillations in high-gradient regions without introducing too much numerical dissipations. The method is tested for some classic simulations including hydraulic jump, 1D dam break and 2D dam break problems. The results show very satisfactory agreement with experimental data, analytical solutions and other numerical results.     

A finite volume scheme for a model coupling free surface and pressurised flows in pipes

A model is derived for the coupling of transient free surface and pressurized flows. The resulting system of equations is written under a conservative form with discontinuous gradient of pressure. We treat the transition point between the two types of flows as a free boundary associated to a discontinuity of the gradient of pressure. The numerical simulation is performed by making use of a Roe-like finite volume scheme that we adapted to such discontinuities in the flux. The validation is performed by comparison with experimental results.     

Low dissipative entropy stable schemes using third order WENO and TVD reconstructions

A low dissipative framework is given to construct high order entropy stable flux by addition of suitable numerical diffusion operator into entropy conservative flux. The framework is robust in the sense that it allows the use of high order reconstructions which satisfy the sign property only across the discontinuities. The third order weighted essentially non-oscillatory (WENO) interpolations and high order total variation diminishing (TVD) reconstructions are shown to satisfy the sign property across discontinuities. Third order accurate entropy stable schemes are constructed by using third order WENO and high order TVD reconstructions procedures in the diffusion operator. These schemes are efficient and less diffusive since the diffusion is actuated only in the sign stability region of the used reconstruction which includes discontinuities. Numerical results with constructed schemes for various test problems are given which show the third order accuracy and less dissipative nature of the schemes.     

l 1-error estimates on the immersed interface upwind scheme for linear convection equations with piecewise constant coefficients: A simple proof

Abstract A linear convection equation with discontinuous coefcients arises in wave propagation through interfaces.An interface condition is needed at the interface to select a unique solution.An upwind scheme that builds this interface condition into its numerical flux is called the immersed interface upwind scheme.An l1-error estimate of such a scheme was frst established by Wen et al.(2008).In this paper,we provide a simple analysis on the l1-error estimate.The main idea is to formulate the solution to the underline initial-value problem into the sum of solutions to two convection equations with constant coefcients,which can then be estimated using classical methods for the initial or boundary value problems.     

Numerical Study of Oscillatory Solutions of the Gas-Dynamic Equations

Solutions of the one-dimensional gas-dynamic equations with oscillatory initial data are studied numerically. A fourth-order ENO scheme is used, together with an artificial compression method to effectively eliminate the smearing of contact discontinuities. The numerical results show that the oscillations die out in velocity and pressure, and persist in density. A system of equations governing the propagation of these oscillations is derived.     

Hybrid Simulation of Space Plasmas: Models with Massless Fluid Representation of Electrons. III. Shockless Discontinuities

This is the third article in a series of reviews on hybrid simulation of low-frequency processes in space plasmas. It deals with shockless (contact, tangential, and rotational) discontinuities. A hybrid model is described with ions represented by particles and electrons by a massless fluid. The Hamiltonian scheme for the numerical implementation of this model is discussed in detail. The first part of the article provides basic background information, which covers MHD models (ideal, resistive, and Hall models) as well as a classification of shockless discontinuities and their main properties. The review part of the article surveys the literature on simulation of the structure and properties of nonpropagating (contact and tangential) discontinuities and the structure of the magnetopause as a complex domain consisting of multiple discontinuities and waves. We also review the literature on hybrid simulation of rotational discontinuities and the structure of the reconnection layer—the configuration of the reconnecting magnetic forcelines in the dayside magnetopause and in the distant magnetotail. The concluding sections examine studies on hybrid simulation of the penetration of plasma inhomogeneities from the solar wind into the magnetosphere. The following issues are considered: the interaction of the bow shock with interplanetary discontinuities; the "hot flow anomaly"; the interaction of pressure pulses with the bow shock; impulsive plasma penetration through a tangential discontinuity (the magnetopause) as a result of a "collision" of a magnetosheath plasmoid (plasma current sheet) with the magnetopause.