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Energy harvesting of a heaving and forward pitching wing with a passively actuated trailing edge
Institution:1. Swinburne University of Technology, Hawthorn, Victoria 3122, Australia;2. Université de Toulouse; INP; IMFT (Institut de Mécanique des Fluides de Toulouse), Allée Camille Soula, F-31400 Toulouse, France;3. CNRS; IMFT, F-31400 Toulouse, France;4. Fluids Laboratory for Aeronautical and Industrial Research (FLAIR), Department of Mechanical and Aerospace Engineering, Monash University, Melbourne, Victoria 3800, Australia;1. Laboratoire de Physique et Mécanique des Milieux Hétérogènes (PMMH UMR 7636), CNRS, France;2. ESPCI Paris, PSL Research University, Sorbonne Université, France;3. Université Paris Diderot, Barre Cassan Bât. A, 7-9 quai St Bernard, 75252 Paris Cedex 05, France;1. Department of Aerodynamics, Nanjing University of Aeronautics and Astronautics Yudao Street 29, Nanjing, Jiangsu 210016, China;2. School of Engineering and Information Technology, University of New South Wales Canberra, ACT 2600, Australia;3. Aerodynamics Development Department, AVIC Aerodynamics Research Institute Yangshan Street 1, Shenyang, Liaoning 110034, China
Abstract:This study experimentally investigates the energy harvesting capabilities of an oscillating wing with a passively actuated trailing edge. The oscillation kinematics are composed of a combined heaving and forward pitching motions, where the pitching axis is well behind the wing center of mass. Passive actuation is attained by connecting the trailing edge with the wing body using a torsion rod. The degree of flexibility of the trailing edge is represented by the Strouhal number based on the trailing edge natural frequency. The trailing edge passive response is studied for oscillation Strouhal numbers of 0.017, 0.025 and 0.033. Instantaneous aerodynamic forces are measured in a closed loop wind tunnel at a Reynolds number of 40 000, based on the free stream velocity and the wing chord length. Measured results include the effective angle of attack induced by the trailing edge actuation as well as the lift and moment during the oscillation cycle. For the imposed kinematics in this study, the pitching motion has a positive contribution to the mean power output whereas the heaving motion has a relatively small but negative contribution. Additionally, by decreasing the natural frequency of the trailing edge closer to that of the imposed oscillation frequency, the magnitude of the lift and moment forces and hence the mean power output, increases. It is found that there exists a strong correlation between mean power output and the effective angle of attack, shown through the passive trailing edge response, resulting in an increase in energy harvesting potential.
Keywords:Energy harvesting  Flexible trailing edge  Forward pitching
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