TY - GEN
T1 - Numerical investigation of self-sustained limit-cycle oscillations in a flapping-foil energy harvester
AU - Wang, Enhao
AU - Ramesh, Kiran
AU - Viola, Ignazio Maria
AU - Killen, Shaun
N1 - Funding Information:
The authors thank the Carnegie Trust for the Universities of Scotland who supported this project via the Collaborative Research Grant titled ”Investigation of Flapping Wings as a Means of Hydroelectric Power Generation”.
Publisher Copyright:
© 2017 International Forum on Aeroelasticity and Structural Dynamics (IFASD). All Rights Reserved.
Copyright:
Copyright 2018 Elsevier B.V., All rights reserved.
PY - 2017
Y1 - 2017
N2 - Two-degree-of-freedom (2DOF) fully passive motion of a flapping foil at a low Reynolds number Re = 10,000 is studied numerically. The simulations are conducted using open source computational fluid dynamics (CFD) toolbox OpenFOAM. The present research is mainly focused on the self-sustained limit-cycle oscillations of a flapping foil with potential application as a hydro-energy harvester. The effect of different parameters on the onset of linear flutter, the characteristics of the system response, the available power from a flapping foil and the flow patterns are investigated. It is found that given a small initial perturbation, the response of the foil is similar to that of classical linear flutter i.e., the oscillations converged to a constant value at reduced velocities lower than the flutter velocity and limit-cycle oscillations (LCOs) are observed once the reduced velocities are greater than the flutter velocity. The reduced frequency of the LCOs exhibits a decreasing trend with increasing reduced velocity. In contrast, the phase difference between pitch and plunge increases with the increase of the reduced velocity. The feasibility of power extraction is demonstrated and the time-averaged power shows a single peak at an intermediate reduced velocity. Limit-cycle oscillations are found to be influenced by leading-edge vortex shedding as well as trailing-edge flow separation.
AB - Two-degree-of-freedom (2DOF) fully passive motion of a flapping foil at a low Reynolds number Re = 10,000 is studied numerically. The simulations are conducted using open source computational fluid dynamics (CFD) toolbox OpenFOAM. The present research is mainly focused on the self-sustained limit-cycle oscillations of a flapping foil with potential application as a hydro-energy harvester. The effect of different parameters on the onset of linear flutter, the characteristics of the system response, the available power from a flapping foil and the flow patterns are investigated. It is found that given a small initial perturbation, the response of the foil is similar to that of classical linear flutter i.e., the oscillations converged to a constant value at reduced velocities lower than the flutter velocity and limit-cycle oscillations (LCOs) are observed once the reduced velocities are greater than the flutter velocity. The reduced frequency of the LCOs exhibits a decreasing trend with increasing reduced velocity. In contrast, the phase difference between pitch and plunge increases with the increase of the reduced velocity. The feasibility of power extraction is demonstrated and the time-averaged power shows a single peak at an intermediate reduced velocity. Limit-cycle oscillations are found to be influenced by leading-edge vortex shedding as well as trailing-edge flow separation.
KW - CFD
KW - Energy harvesting
KW - Flapping wings
KW - Fluid structure interaction
KW - Leading edge vortices
UR - http://www.scopus.com/inward/record.url?scp=85048612063&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:85048612063
T3 - 17th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2017
BT - 17th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2017
PB - International Forum on Aeroelasticity and Structural Dynamics (IFASD)
T2 - 17th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2017
Y2 - 25 June 2017 through 28 June 2017
ER -