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A COMPUTATIONAL METHOD FOR THE NAVIER-STOKES EQUATIONS AT ALL SPEEDS
引用本文:赵兴艳,苏莫明,苗永淼. A COMPUTATIONAL METHOD FOR THE NAVIER-STOKES EQUATIONS AT ALL SPEEDS[J]. 应用数学和力学(英文版), 2002, 23(4): 479-486. DOI: 10.1007/BF02436217
作者姓名:赵兴艳  苏莫明  苗永淼
作者单位:ZHAO Xing-yan,SU Mo-ming,MIAO Yong-miao (1 Department of Fluid Machinery,Xi'an Jiaotong University,Xi'an 710049,P R China; 2.Department of Aerospace Power,Northwestern Polytechnical University,Xi'an 710072,P R China
摘    要:
IntroductionForcomputationoftheviscouscompressibleflowstheNavier_Stokesequationsaregenerallyrepresentedintheconservationlawformasahyperbolicsystem .Lackingthemathematicaltooltoanalyzethisnonlinearsystem ,thenumericalmethodsusedinsolvingthenonlinearhype…

收稿时间:1999-10-13

A computational method for the Navier-Stokes equations at all speeds
Zhao Xing-yan Lecturer, Doctor,Su Mo-ming,Miao Yong-miao. A computational method for the Navier-Stokes equations at all speeds[J]. Applied Mathematics and Mechanics(English Edition), 2002, 23(4): 479-486. DOI: 10.1007/BF02436217
Authors:Zhao Xing-yan Lecturer   Doctor  Su Mo-ming  Miao Yong-miao
Affiliation:1. Department of Fluid Machinery, Xi'an Jiaotong University, Xi'an 710049, P R China
2. Department of Aerospace Power, Northwestern Polytechnical University, Xi'an 710072, P R China
Abstract:
A PLU-SGS method based on a time-derivative preconditioning algorithm and LU-SGS method is developed in order to calculate the Navier-Stokes equations at all speeds. The equations were discretized using AUSMPW scheme in conjunction with the third-order MUSCL scheme with Van Leer limiter. The present method was applied to solve the multidimensional compressible Navier-Stokes equations in curvilinear coordinates. Characteristic boundary conditions based on the eigensystem of the preconditioned equations were employed. In order to examine the performance of present method, driven-cavity flow at various Reynolds numbers and viscous flow through a convergent-divergent nozzle at supersonic were selected to test this method. The computed results were compared with the experimental data or the other numerical results available in literature and good agreements between them are obtained. The results show that the present method is accurate, self-adaptive and stable for a wide range of flow conditions from low speed to supersonic flows.
Keywords:nonlinear hyperbolic system  computational fluid dynamic  preconditioning algorithm  implicit time marching method  characteristic boundary condition  high-order-accuracy
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