Flow about a slotted cylinder-airfoil combination in a wind tunnel

被引:2
作者
Cizmas, PGA [1 ]
Tang, D [1 ]
Dowell, EH [1 ]
机构
[1] DUKE UNIV,DEPT MECH ENGN & MAT SCI,DURHAM,NC 27708
来源
JOURNAL OF AIRCRAFT | 1996年 / 33卷 / 04期
关键词
D O I
10.2514/3.47006
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The flowfield around a gust generator device, an airfoil/rotating slotted cylinder (RSC) system, is numerically simulated using the general-purpose finite element program FIDAP. The how is assumed to be quasisteady, turbulent, incompressible, and two dimensional, The turbulence is modeled far from the walls by a high Reynolds number k-epsilon model. In the near-wall region, which includes the viscous sublayer, the mixing length concept is used to model turbulence, The numerical analysis treats the time-varying flow around the gust generator device as quasisteady and solves the flow position by-position as the RSC rotates. The variation of lift and drag as a function of the rotation angle and as a function of the gap between the airfoil and the rotating slotted cylinder is calculated.
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页码:716 / 721
页数:6
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