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Scaling of flow separation on a pitching low aspect ratio plate
Authors:T Yilmaz  M Ol  D Rockwell
Institution:1. Department of Mechanical Engineering and Mechanics, Lehigh University, Bethlehem, PA 18015, USA;2. US Air Force Research Laboratory, Air Vehicles Directorate, Wright-Patterson AFB, OH 45433-7542, USA;1. Division of Mechanical Engineering, Aeronautics Institute of Technology (ITA), Brazil;2. São Carlos School of Engineering, University of São Paulo, São Carlos, Brazil;1. University of Shanghai for Science and Technology, Shanghai, 200093, China;2. Shanghai Key Laboratory of Power Energy in Multiphase Flow and Heat Transfer, Shanghai, 200093, China;3. Marine Design and Research Institute of China, Shanghai, 200011, China
Abstract:We use two different dye injection approaches, in two different water tunnels, to visualize the formation and subsequent evolution of leading-edge vortices and related separated structures, for a pitching low aspect ratio plate. The motion is a smoothed linear pitch ramp from 0° to 40° incidence, brief hold, and return to 0°, executed at reduced pitch rates ranging from 0.1 to 0.35 and about various pivot locations. All cases evince a leading edge vortex with pronounced axial flow, which leads to formation of large-scale, three-dimensional flow structures, culminating in a large vortical structure centered at the wing symmetry plane. Pitch is also compared to plunge, where the plunge-induced angle of attack is taken as the geometric pitch incidence angle, ignoring pitch-rate effects. At successively increasing values of convective time C/U, the three-dimensional patterns of the flow structure are remarkably similar for the pitching and plunging motions. The similarity of these patterns persists, though they are shifted in time, for variation of either the location of the pitching axis or the dimensionless pitch rate.
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