首页 | 本学科首页   官方微博 | 高级检索  
     检索      

点隐式龙格-库塔方法的应用研究
引用本文:李典,杨永.点隐式龙格-库塔方法的应用研究[J].航空计算技术,2011,41(3):66-70.
作者姓名:李典  杨永
作者单位:西北工业大学,航空学院,流体力学系,陕西,西安,7100721
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。

关 键 词:显式龙格-库塔方法  点隐式龙格-库塔方法  欧拉方程

Some Investigations on Applications of Point-implicit Runge-Kutta Method
LI Dian,YANG Yong.Some Investigations on Applications of Point-implicit Runge-Kutta Method[J].Aeronautical Computer Technique,2011,41(3):66-70.
Authors:LI Dian  YANG Yong
Institution:(Department of Aerodynamics,School of Aeronautics,Northwestern Polytechnical Universtity,Xi′an 710072,China)
Abstract: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.
Keywords:point-implicit Runge-Kutta method  Euler equations
本文献已被 CNKI 维普 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号