2023
DOI: 10.1063/5.0139882
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Mode transition in fluid–structure interaction of piezoelectric membrane wings

Abstract: Flow-induced vibrations can be utilized to harvest energy for micro air vehicles (MAVs). A flexible membrane wing with an embedded piezoelectric energy harvester at an angle of attack of 12 degrees and Reynolds number (Re) of 8000 is studied by numerical simulations. An aero-electro-mechanical model is established to investigate the effect of the leading-edge (LE) and trailing-edge (TE) geometries on the fluid-structure interaction (FSI) modes, aerodynamic performance, and energy harvesting performance. A new … Show more

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