Unsteady lift and drag forces acting on the elliptic cylinder

被引:10
|
作者
Kim, MS
Park, YB
机构
[1] School of Aerospace and Mechanical Engineering, Hankuk Aviation University
[2] Department of Aerospace Engineering, Hankuk Aviation University
关键词
unsteady force; SIMPLER method; elliptic cylinder; Navier-Stokes equations incompressible viscous flow; angle of attack;
D O I
10.1007/BF02916210
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
A parametric study has been accomplished to figure out the effects of elliptic cylinder thickness, angle of attack, and Reynolds number oil the unsteady lift and drag forces exerted on the elliptic cylinder. A two-dimensional incompressible Navier-Stokes flow solver is developed based on the SIMPLER method in the body-intrinsic coordinates system to analyze the unsteady viscous flow over elliptic cylinder. Thickness-to-chord ratios of 0.2, 0.4, and 0.6 elliptic cylinders are simulated at different Reynolds numbers of 400 and 600, and angles of attack of 10 degrees, 20 degrees, and 30 degrees. Through this study, it is observed that the elliptic cylinder thickness, angle of attack, and Reynolds number are very important parameters to decide the lift and drag forces. All these parameters also affect significantly the frequencies of the unsteady force oscillations.
引用
收藏
页码:167 / 175
页数:9
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