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三角翼上分离及涡流的数值模拟
引用本文:阎超,李亭鹤,黄贤禄.三角翼上分离及涡流的数值模拟[J].力学进展,2001,31(2):227-244.
作者姓名:阎超  李亭鹤  黄贤禄
作者单位:北京航空航天大学国家CFD实验室
基金项目:国家自然科学基金,国防预研基金资助项目&&
摘    要:综述了三角翼(包括双三角翼,边条-三角翼,近距耦合鸭翼)上分离及涡流问题的数值模拟进展,介绍了用Euler方程、N-S方程的数值方法模拟不同三角翼,在不同攻角、不同来流M数等多种条件下的复杂涡流形态和流动结构,研究了控制方程、网格、湍流模型和计算方法等对计算结果的影响。 

关 键 词:三角翼    数值模拟    涡流    分离流
修稿时间:1999年12月13

NUMERICAL SIMULATION OF SEPARATION AND VORTICAL FLOWS ON DELTA WINGS
Yan Chao, Li Tinghe, Huang Xianlu Beijing University of Aeronautics and Astronautics,Beijing ,China.NUMERICAL SIMULATION OF SEPARATION AND VORTICAL FLOWS ON DELTA WINGS[J].Advances in Mechanics,2001,31(2):227-244.
Authors:Yan Chao  Li Tinghe  Huang Xianlu Beijing University of Aeronautics and Astronautics  Beijing  China
Institution:Yan Chao, Li Tinghe, Huang Xianlu Beijing University of Aeronautics and Astronautics,Beijing 100083,China
Abstract:The progress in numerical simulations of separation and vortical flows on delta wings (including double-delta wings, strake-delta wings and close-coupled canards) was summarized in this paper. The numerical methods using Euler equations and N-S equations in the simulations for the configurations of complex vortical flows and structures of separation flows on different delta wings under the conditions of different angle of attack and flow M numbers are reviewed. The effects of control equations, grids, turbulence model and numerical methods on the results were also discussed.
Keywords:delta wings  numerical simulation  vortical flows  separation flows
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