Vortex dynamics around pitching plates

被引:43
|
作者
Jantzen, Ryan T. [1 ,2 ]
Taira, Kunihiko [1 ,2 ]
Granlund, Kenneth O. [3 ]
Ol, Michael V. [3 ]
机构
[1] Florida State Univ, Dept Mech Engn, Tallahassee, FL 32310 USA
[2] Florida State Univ, Florida Ctr Adv Aeroprop, Tallahassee, FL 32310 USA
[3] US Air Force, Res Lab, Aerosp Syst Directorate, Wright Patterson AFB, OH 45433 USA
关键词
IMMERSED BOUNDARY METHOD; WINGS; GENERATION;
D O I
10.1063/1.4879035
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Vortex dynamics of wakes generated by rectangular aspect-ratio 2 and 4 and two-dimensional pitching flat plates in free stream are examined with direct numerical simulation and water tunnel experiments. Evolution of wake vortices comprised of tip, leading-edge, and trailing-edge vortices is compared with force history for a range of pitch rates. The plate pivots about its leading edge with reduced frequency from p/8 to p/48, which corresponds to pitching over 1 to 6 chord lengths of travel. Computations have reasonable agreement with experiments, despite large differences in Reynolds number. Computations show that the tip effects are confined initially near the wing tips, but begin to strongly affect the leading-edge vortex as the motion of the plate proceeds, with concomitant effects on lift and drag history. Scaling relations based on reduced frequency are shown to collapse aerodynamic force history for the various pitch rates. (C) 2014 AIP Publishing LLC.
引用
收藏
页数:17
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