TY - GEN
T1 - Simulations of flow past a mirrored airfoil configuration inspired by an energy-harvester
AU - Abidi, Zavar A.
AU - Goza, Andres
AU - Houchens, Brent C.
N1 - Publisher Copyright:
© 2022, American Institute of Aeronautics and Astronautics Inc. All rights reserved.
PY - 2022
Y1 - 2022
N2 - A novel wind energy harvesting system has recently been designed to capture distributed wind energy. This design abandons the traditional turbine design that is standard for wind energy, and instead adopts two mirrored airfoils and extracts energy from the low pressure region between the foils. During experimental testing, the system showed high potential, with an increase in harvesting capacity as the angle-of-attack of the airfoils increased. This benefit, however, disappeared for sufficiently high angle-of-attack, commensurate with a shift from a symmetric to a directed wake. To investigate this detrimental transition, we present here simulations for the mirrored airfoil configuration at a Reynolds Number of 1000. Using this data, we provide a regime map that conveys the system dynamics for a sweep of the angle-of-attack and spacing between the mirrored airfoils. Our results indicate that the transition to the asymmetric wake is due to a linear instability—absent in the single airfoil case—that is due to the aerodynamic coupling of the foils. We explore this instability mechanism using detailed analysis of the time-varying flow-field and comment on potential implications on harvesting potential for this wind energy system.
AB - A novel wind energy harvesting system has recently been designed to capture distributed wind energy. This design abandons the traditional turbine design that is standard for wind energy, and instead adopts two mirrored airfoils and extracts energy from the low pressure region between the foils. During experimental testing, the system showed high potential, with an increase in harvesting capacity as the angle-of-attack of the airfoils increased. This benefit, however, disappeared for sufficiently high angle-of-attack, commensurate with a shift from a symmetric to a directed wake. To investigate this detrimental transition, we present here simulations for the mirrored airfoil configuration at a Reynolds Number of 1000. Using this data, we provide a regime map that conveys the system dynamics for a sweep of the angle-of-attack and spacing between the mirrored airfoils. Our results indicate that the transition to the asymmetric wake is due to a linear instability—absent in the single airfoil case—that is due to the aerodynamic coupling of the foils. We explore this instability mechanism using detailed analysis of the time-varying flow-field and comment on potential implications on harvesting potential for this wind energy system.
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U2 - 10.2514/6.2022-2203
DO - 10.2514/6.2022-2203
M3 - Conference contribution
AN - SCOPUS:85123892783
SN - 9781624106316
T3 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
BT - AIAA SciTech Forum 2022
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
Y2 - 3 January 2022 through 7 January 2022
ER -