Power and efficiency analysis of a flapping wing wind energy harvester

Energy harvesting from flowing fluids using flapping wings and fluttering aeroelastic structures has recently gained significant research attention as a possible alternative to traditional rotary turbines, especially at and below the centimeter scale. One promising approach uses an aeroelastic flutter instability to drive limit cycle oscillations of a flexible piezoelectric energy harvesting structure. Such a system is well suited to miniaturization and could be used to create self-powered wireless sensors wherever ambient flows are available. In this paper, we examine modeling of the aerodynamic forces, power extraction, and efficiency of such a flapping wing energy harvester at a low Reynolds number on the order of 1000. Two modeling approaches are considered, a quasi-steady method generalized from existing models of insect flight and a modified model that includes terms to account to the effects of dynamic stall. The modified model is shown to provide better agreement with CFD simulations of a flapping energy harvester.

[1]  C. T. Tran,et al.  Semi-empirical model for the dynamic stall of airfoils in view of the , 1980 .

[2]  J. Delaurier,et al.  The wingmill - An oscillating-wing windmill , 1980 .

[3]  M. Dickinson,et al.  The aerodynamic effects of wing rotation and a revised quasi-steady model of flapping flight. , 2002, The Journal of experimental biology.

[4]  Christopher E. Brennen,et al.  A Review of Added Mass and Fluid Inertial Forces , 1982 .

[5]  Timothy C. Green,et al.  Energy Harvesting From Human and Machine Motion for Wireless Electronic Devices , 2008, Proceedings of the IEEE.

[6]  Yuan-Cheng Fung,et al.  An introduction to the theory of aeroelasticity , 1955 .

[7]  Matthew Bryant,et al.  Aeroelastic flutter energy harvester design: the sensitivity of the driving instability to system parameters , 2011 .

[8]  Z. J. Wang,et al.  Unsteady aerodynamics of fluttering and tumbling plates , 2005, Journal of Fluid Mechanics.

[9]  T. Theodorsen General Theory of Aerodynamic Instability and the Mechanism of Flutter , 1934 .

[10]  Max F. Platzer,et al.  Oscillating-wing Power Generation , 1999 .

[11]  Ronald E. Gormont A Mathematical Model of Unsteady Aerodynamics and Radial Flow for Application to Helicopter Rotors , 1973 .

[12]  Jeffrey A. Walker,et al.  Rotational lift: something different or more of the same? , 2002, The Journal of experimental biology.

[13]  Gordon J. Berman,et al.  Energy-minimizing kinematics in hovering insect flight , 2007, Journal of Fluid Mechanics.

[14]  J. G. Leishman,et al.  A Semi-Empirical Model for Dynamic Stall , 1989 .

[15]  Z. J. Wang,et al.  Unsteady forces and flows in low Reynolds number hovering flight: two-dimensional computations vs robotic wing experiments , 2004, Journal of Experimental Biology.

[16]  T. Kinsey,et al.  Parametric Study of an Oscillating Airfoil in a Power-Extraction Regime , 2008 .

[17]  Qiang Zhu,et al.  Optimal frequency for flow energy harvesting of a flapping foil , 2011, Journal of Fluid Mechanics.

[18]  Matthew Bryant,et al.  Modeling and Testing of a Novel Aeroelastic Flutter Energy Harvester , 2011 .