The formation process of leading-edge vortices has been investigated experimentally using Particle Image Velocimetry. Various airfoil kinematics have been tested, including asymmetric and peak-shifted plunging motions, and are evaluated for Re = 30,000 and a reduced frequency range of 0.2 <= k <= 0.33. By measuring the growth in the leading-edge vortex during the dynamic-stall process, the vortex pinch-off process is examined based on the concept of an optimal vortex formation time. The various kinematics are then evaluated with respect to their associated vortex strength, timing and convection into the wake.
The influence of airfoil kinematics on the formation of leading-edge vortices in bio-inspired flight
Einfluss der Flügelkinematik auf die Bildung der Vorderkantenwirbel beim biologisch inspirierten Flug
Experiments in Fluids ; 46 , 5 ; 823-833
2009
11 Seiten, 14 Bilder, 1 Tabelle, 16 Quellen
Aufsatz (Zeitschrift)
Englisch
Recovery of Energy from Leading- and Trailing-Edge Vortices in Tandem-Airfoil Configurations
Online Contents | 2011
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