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Jameson/TVD格式应用旋翼翼型绕流分析
引用本文:曹义华,王吉飞,苏媛,邓丹丹.Jameson/TVD格式应用旋翼翼型绕流分析[J].航空动力学报,2002,17(3):297-301.
作者姓名:曹义华  王吉飞  苏媛  邓丹丹
作者单位:北京航空航天大学,飞行器设计与应用力学系,北京,100083
基金项目:航空基础科学基金资助项目 (0 0 A5 10 5 0 )
摘    要:以一种常见的旋翼翼型为例 ,探讨了两种旋翼桨叶翼型绕流数值模拟方法 ,即 Jameson有限体积中心格式和有限体积通量修正 Jameson/ TVD混合格式。这两种格式的方法都采用有限体积法进行离散 ,并用龙格—库塔时间推进法求解。通过算例分析 ,比较了这两种方法的特点 ,为进一步有效地依靠求解湍流 Navier-Stokes方程来模拟完整的旋翼流场、旋翼阻力与功率奠定了基础

关 键 词:旋翼空气动力学  数值模拟  TVD格式  N-S方程
文章编号:1000-8055(2002)03-0297-05
收稿时间:2001/5/23 0:00:00
修稿时间:2001年5月23日

Jameson/TVD Schemes Applied to Simulating the Flow around Rotor Aerofoil
CAO Yi hu,WANG Ji fei,SU Yuan and DENG Dan dan.Jameson/TVD Schemes Applied to Simulating the Flow around Rotor Aerofoil[J].Journal of Aerospace Power,2002,17(3):297-301.
Authors:CAO Yi hu  WANG Ji fei  SU Yuan and DENG Dan dan
Institution:Beijing University of Aeronautics and Astronautics,Beijing100083,China;Beijing University of Aeronautics and Astronautics,Beijing100083,China;Beijing University of Aeronautics and Astronautics,Beijing100083,China;Beijing University of Aeronautics and Astronautics,Beijing100083,China
Abstract:Two methods based on Jameson scheme and Jameson/flux correction TVD (Total Variation Diminishing) mixed scheme are constructed to simulate the flow around rotor airfoil.By using finite volume approach for numerical approximation and Runge Kutta time stepping advance,Euler/Navier Stokes equations are solved.Through the analyses of examples,the characteristics of these two methods are concluded.Also,these methods can be further developed to simulate the turbulent flow around helicopter rotor and to calculate helicopter rotor drag and power.
Keywords:rotor aerodynamics  numerical simulation  TVD scheme  N  S equation
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