Abstract
AbstractThe three-dimensional structure of the leading-edge vortex on a rotating wing is addressed using a technique of particle image velocimetry. Organized patterns of chordwise-oriented vorticity, which exist within the vortex, arise from the spanwise flow along the surface of the wing, which can attain a velocity the same order as the velocity of the wing at its radius of gyration. These patterns are related to the strength (circulation) and coherence of the tip and root vortices. The associated distributions of spanwise-oriented vorticity along the leading-edge vortex are characterized in relation to the vorticity flux and downwash along the wing.
Publisher
Cambridge University Press (CUP)
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics
Reference23 articles.
1. 15. Ozen C. A. 2012 Unsteady flow structure on rotating and flapping wings. PhD thesis, Lehigh University, Bethlehem, PA.
2. The effects of corrugation and wing planform on the aerodynamic force production of sweeping model insect wings
3. Leading-edge vortices in insect flight
4. Three-dimensional flow structures and evolution of the leading-edge vortices on a flapping wing
5. 7. Eldredge J. D. , Wang C. J. & Ol M. 2009 A computational study of a canonical pitch-up, pitch-down wing maneuver. AIAA Paper 3687.
Cited by
81 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献