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不同马赫数的无粘和粘性流动高阶精度隐式计算方法
引用本文:赵兴艳,张楚华,苗永淼,苏莫明.不同马赫数的无粘和粘性流动高阶精度隐式计算方法[J].航空学报,2001,22(1):15-18.
作者姓名:赵兴艳  张楚华  苗永淼  苏莫明
作者单位:1. 西安交通大学 流体机械系,
2. 西北工业大学 航空动力系,
摘    要: 应用隐式时间推进法对不同马赫数的无粘和粘性流动进行数值分析,给出了基于预处理方法的高阶精度隐式求解方法。方程离散采用改进的高阶精度对流迎风分裂格式。该方法通过求解曲线坐标系可压缩Euler和 Navier-Stokes方程,对低速到超音速范围内的无粘和粘性流动的典型问题进行了数值分析。计算结果与文献的数值结果或实验数据对比分析表明,该方法对低速到超音速范围内的无粘和粘性流动问题进行数值分析是可行而有效的。

关 键 词:计算流体动力学  隐式时间推进法  预处理算法  高阶精度  曲线坐标系  
文章编号:1000-6893(2001)01-0015-04
修稿时间:1999年10月20

HIGH-ORDER-ACCURATE IMPLICIT COMPUTATIONAL METHOD OF INVISCID AND VISCOUS FLOWS AT VARIOUS MACH NUMBERS
ZHAO Xing-yan,ZHANG Chu-hua,MIAO Yong-miao,SU Mo-ming.HIGH-ORDER-ACCURATE IMPLICIT COMPUTATIONAL METHOD OF INVISCID AND VISCOUS FLOWS AT VARIOUS MACH NUMBERS[J].Acta Aeronautica et Astronautica Sinica,2001,22(1):15-18.
Authors:ZHAO Xing-yan  ZHANG Chu-hua  MIAO Yong-miao  SU Mo-ming
Institution:1. Department of Fluid Mach inery, Xi'an Jiao tong University, Xi'an 710049, China;2. Department of Aero space Power, Northw estern PolytechnicalU niversity, Xi'an 710072, China
Abstract:A high order accurate computational method based on a time derivative preconditioning algorithm is developed in order to calculate inviscid and viscous flows at various Mach numbers by using the implicit time marching method. The equations are discretized using a high order accurate AUSMPW scheme. The present algorithm is extended to the multidimensional curvilinear coordinates systems, and it is applied to numerical solution of the compressible Euler and Navier Stokes equations. Computational capabilities are demonstrated through computation of a wide variety of problems. Comparison of calculation with available numerical and experimental data in literature shows that the algorithm is accurate, self adaptive and stable for a wide range of flow conditions from inviscid to viscous flows and from low speed to supersonic flows.
Keywords:computational fluid dynamics  implicit time marching method  preconditioning algorithm  high  order  accuracy  curvilinear coordinate systems
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