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预处理方法在全速度流场中的应用研究
引用本文:夏树宁,吴宗成,朱自强.预处理方法在全速度流场中的应用研究[J].计算力学学报,2011,28(Z1):79-83.
作者姓名:夏树宁  吴宗成  朱自强
作者单位:北京航空航天大学,航空科学与工程学院,北京,100191
基金项目:国家重点基础研究发展计划(973)
摘    要:应用预处理方法求解二维可压缩Navier-Stokes方程,发展出一套既适用于低速流动,也可用于可压缩流动的全速度流场解算方法.空间格式选用Ausm类格式,并采用多步Runge-Kutta时间推进方法.数值模拟了鼓包(Bump),RAE2822翼型,多段高升力翼型的不同速度绕流流场,并与实验数据进行了对比.结果表明预处...

关 键 词:预处理  Navier-Stokes方程  低速流动  多段翼型

Study of preconditioning methods applied to flowfield at all speeds
XIA Shu-ning,WU Zong-cheng,ZHU Zi-qiang.Study of preconditioning methods applied to flowfield at all speeds[J].Chinese Journal of Computational Mechanics,2011,28(Z1):79-83.
Authors:XIA Shu-ning  WU Zong-cheng  ZHU Zi-qiang
Institution:XIA Shu-ning~*,WU Zong-cheng,ZHU Zi-qiang (School of Aeronautic Science and Engineering,Beihang University,Beijing 100191,China)
Abstract:The preconditioning methods are used for solving two-dimensional compressible Navier-Stokes equations and an all-speed flow field numerical simulation method which can be used for both low-speed flows and compressible flows is developed.Ausm family schemes and multi-step Runge-Kutta time marching method are utilized to discretize Navier-Stokes equations.Numerical simulation results of flow field of a Bump,RAE2822 airfoil and multi-element high lift airfoil at different speeds are presented and are compared ...
Keywords:preconditioning  navier-stokes equations  low speed flow  multi-element airfoil  
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