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Numerical simulation on aerodynamic of the wing in ground effect
Wu, Rong ; Liang, Feng ; Wu R(吴榕)
2012
关键词Angle of attack Electrical engineering Finite volume method Ground effect Insulating materials Navier Stokes equations Turbulence models
英文摘要Conference Name:2012 International Conference on Electrical Insulating Materials and Electrical Engineering, EIMEE 2012. Conference Address: Shenyang, Liaoning, China. Time:May 25, 2012 - May 27, 2012.; Aerodynamic characteristics of the wing NACA5312 in ground effect are investigated with the numerical simulation method. The N-S equations and the k-螘 turbulence model are solved by the finite volume method in CFD software. This paper computes the flying states under different clearances, steam velocities and angles of attack. Compared with results under the unbounded flow, it studies the relations between the aerodynamic performances and the angles of attack, the steam velocity, and the relative heights. The aerodynamic performances include the lift coefficient, drag coefficient, and lift-drag ratio. 漏 (2012) Trans Tech Publications, Switzerland.
语种英语
出处http://dx.doi.org/10.4028/www.scientific.net/AMR.546-547.200
出版者Trans Tech Publications
内容类型其他
源URL[http://dspace.xmu.edu.cn/handle/2288/86258]  
专题物理技术-会议论文
推荐引用方式
GB/T 7714
Wu, Rong,Liang, Feng,Wu R. Numerical simulation on aerodynamic of the wing in ground effect. 2012-01-01.
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