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点隐式龙格-库塔方法的应用研究 被引量:2

Some Investigations on Applications of Point-implicit Runge-Kutta Method
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摘要 为了提高求解器的效率,在显式龙格-库塔时间推进的欧拉方程求解器之上,发展了点隐式龙格-库塔时间推进格式。给出了其推导过程和非结构网格下中心格式和迎风格式(Roe和Van Leer格式)预处理算子的构造方法。NACA0012翼型和RAE2822翼型的跨音速无粘流动模拟表明:与显式龙格-库塔方法相比,方法能提高求解效率且内存需求相当,具有一定的工程应用价值。 In order to improve the efficiency of flow solver,a point-implicit Runge-Kutta method is raised on the basis of the Euler solver with an explicit Runge-Kutta method time marching.The derivation of preconditioner is presented.Its constructions,according to the central and upwind(Roe-and Van Leer-scheme) spatial discretization,based on unstructured grid are given,respectively.The simulations of the transonic inviscid flow around NACA0012 and RAE2822 show that comparing with the explicit Runge-Kutta method,the efficientcy is improved by the presented algorithm with a moderate memory increment.
作者 李典 杨永
出处 《航空计算技术》 2011年第3期66-70,共5页 Aeronautical Computing Technique
关键词 显式龙格-库塔方法 点隐式龙格-库塔方法 欧拉方程 point-implicit Runge-Kutta method Euler equations
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参考文献8

  • 1Dimitri J Mavriplis.On Convergence Acceleration Techniques for Unstrctured Meshes[A].AIAA Paper 98-2966,1998.
  • 2Bijl H.Time Integration Schemes for the Unsteady NavierStokes Equations[A].AIAA-2001-2612.
  • 3John C Butcher.Numerical Methods for Ordinary Differential Equations[M].Second Edition.Chichester,UK:WileyBlackwell,2003.
  • 4Blazek J.Computational Fluid Dynamics:Principles and Applications[M].Amsterdam:Elsevier Science,2001.
  • 5Pierce N A,Giles M B.Preconditioning on Stretched Meshes[R].Oxford,England:Oxford University Computing Laboratory Numerical Analysis Group,1995.
  • 6Swanson R C,Turkel E.On Central Difference and Upwind Schemes[J].J.Comput.Physics,1992,101 (2):292-306.
  • 7Roe P L.Approximate Riemann Solvers,Parameter Vectors and Difference Schemes[J].Journal of Computational Physics,1981,43(2):357-372.
  • 8Van B Leer.The Flux-Vector splitting for the Euler equations[C].Aachen,West Germany:International Conference on Numerical in Fluid Dynamics 8th,1982.

同被引文献27

  • 1袁先旭.非定常流动数值模拟及飞行器动态特性研究[D].中国空气动力研究与发展中心,2002.
  • 2Roger Peyret. Handbook of Computational Fluid Mechanics [ M ]. New York: Academic Press Limited, 1996.
  • 3T H Pulliam, D S Chaussee. A Diagonal Form an Implicit Approx- imate Factofization Algorithms[ J]. Journal of Computational Phys- ics, 1981,39:347-363.
  • 4S Yoon, A Jameson. Lower-upper symmetric Gauss-Sediel meth- od for the Euler and Navier-Stokes equations[ J ]. AIAA Journal, 1988,26(9).
  • 5A Pueyo, D W Zingg. Efficient Newton-Krylov Solver for Aerody- namic Computations[J]. AIAA journal, 1998,36( 11 ).
  • 6国义军.旋转钝锥高超声速绕流的数值模拟与定性分析研究[D].中国空气动力研究与发展中心,1994.
  • 7H Bijl. Time Integration schemes for the unsteady Navier-Stokes Equations[ J ]. AIAA-2001-2612, 2001.
  • 8阎超.计算流体力学方法及其应用[M].北京:北京航空航天大学出版社,2012.
  • 9Vahidi B, Esmaeeli E. MATLAB - SIMULINK - based simulation for digital differential relay protection of power transformer for educational purpose [ J ]. Computer Applications in Engineering Education,2013, 21 (3) :475 -483.
  • 10Zuliani P, Platzer A, Clarke E M. Bayesian statistical model chec- king with application to Stateflow/Simulink verification [ J ]. Formal Methods in System Design,2013,43 (2, SI) :338 - 367.

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