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Applied Energy
journal homepage: www.elsevier.com/locate/apenergy
Role of the galloping force and moment of inertia of inclined square
cylinders on the performance of hybrid galloping energy harvesters
U. Javed
a
, A. Abdelkefi
b,
⁎
a
Department of Mechanical and Manufacturing Engineering, Saint Cloud State University, Saint Cloud, 56301 MN, USA
b
Department of Mechanical and Aerospace Engineering, New Mexico State University, Las Cruces, NM 88003, USA
HIGHLIGHTS
•
Hybrid Energy harvesting by inclined square cylinder prone to galloping oscillations is investigated.
•
A reduced-order model is developed for the beam-cylinder harvester using Galerkin discretization.
•
The performance of the energy harvester for various inclination angles are carried out.
•
An upright zero inclined or a slight angle of cylinder is preferable for energy harvesting.
•
Any backward angle of cylinder is not suitable for attaining high levels of harvested power.
ARTICLE INFO
Keywords:
Hybrid energy harvesting
Inclined square cylinders
Transverse galloping
Aerodynamic force representation
ABSTRACT
Energy harvesting by a square cross-section cylinder, inclined at different angles from the incoming wind flow,
prone to galloping oscillations is investigated. The cylinder is fixed at the tip of a cantilever beam at a definite
angle, to which is attached a piezoelectric layer and a permanent magnet placed in the close vicinity of a coil.
Existing aerodynamic-coefficient experimental values as a function of the incident angle of attack are utilized for
determining the aerodynamic force on each inclined cylinder. Seven-order polynomial is recognized to be a
convenient choice for performing the analyses in this study. After establishing the galloping aerodynamic force
of each case, a reduced-order model is developed for the beam-cylinder energy harvester using Galerkin dis-
cretization. Moment of inertia of each case is calculated using transformation matrix and its impact on the
natural frequency is determined. It is shown that the moment of inertia affects the linear characteristics of the
galloping-based energy harvester when the inclination of the cylinder is changed. The nonlinear characteristics
and performance of the energy harvester for various inclination angles are carried out. It is indicated that an
upright zero inclined or a slight angle of cylinder till ten or fifteen degrees towards the wind flow is preferable
for energy harvesting. Any forward inclination towards the wind flow greater than that or any backward angle of
cylinder away from the wind flow are not suitable for attaining high levels of harvested power. This behavior
actually opens the doors for using a movable cylinder at the tip of a beam with lock mechanism that can be tilted
at a high forward or backward angle for extreme windy conditions to have reasonable practical power harvesting
without damaging the harvester.
1. Introduction
Localized energy production is on the rise due to the arrival and
applicability of electronic gadgets, microelectro-mechanical systems,
actuators [1,2], health monitoring and wireless sensors [3], and med-
ical implants [4]. Researchers have shown tremendous interest in both
base [5–7] as well as flow-induced vibrations [8–14] for effective en-
ergy harvesting. Abdelkefi [15] talks in length about utilizing
aeroelastic oscillations, such as flutter exhibited by airfoil sections,
galloping vibrations of prismatic cylinders, vortex-induced vibrations
(VIV) present in circular cylinders, or wake galloping using different
transduction mechanisms including piezoelectric [5–7], electro-
magnetic [8,16,17], and electrostatic [18]. The concept of using hybrid
transduction comprising of a functional piezoelectric layer and an
electromagnet-coil arrangement for aeroelastic oscillations have re-
cently been proposed [16,17].
https://doi.org/10.1016/j.apenergy.2018.09.141
Received 25 April 2018; Received in revised form 25 August 2018; Accepted 13 September 2018
⁎
Corresponding author.
E-mail address: abdu@nmsu.edu (A. Abdelkefi).
Applied Energy 231 (2018) 259–276
0306-2619/ © 2018 Elsevier Ltd. All rights reserved.
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