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Finite wing effects on the energy harvesting from stall-induced oscillations

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Author(s):
dos Santos, Carlos Renan ; Marques, Flavio Donizeti
Total Authors: 2
Document type: Journal article
Source: JOURNAL OF VIBRATION AND CONTROL; v. N/A, p. 17-pg., 2022-05-12.
Abstract

The modeling of aeroelastic harvesters usually employs methods for two-dimensional aerodynamics. Such convenient practice reflects the lack in the literature of efficient tools with low computational cost to assess unsteady and nonlinear aerodynamics loads accounting for three-dimensional wing effects. In this sense, the present work aims to fulfill this gap by developing a nonlinear unsteady lifting line to investigate finite wing effects on the power generation from stall-induced oscillations. The aerodynamic model links the Beddoes-Leishman dynamic stall method to a linear unsteady lifting line. The optimization of energy harvesters from stall-induced pitching oscillations is revisited considering the three-dimensional aerodynamic model. Results reveal that the three-dimensional harvester's dynamic behavior may differ from the two-dimensional case, and the harvested power reduction is observed. (AU)

FAPESP's process: 18/05247-8 - Theoretical investigation of unsteady nonlinear aerodynamics
Grantee:Carlos Renan dos Santos
Support Opportunities: Scholarships abroad - Research Internship - Doctorate (Direct)
FAPESP's process: 17/09468-6 - Optimization of the energy harvesting from airfoil stall induced oscillations
Grantee:Carlos Renan dos Santos
Support Opportunities: Scholarships in Brazil - Doctorate (Direct)
FAPESP's process: 17/02926-9 - Airfoil unsteady aerodynamic loading assessment under dynamic stall for semi-empirical model validation
Grantee:Flávio Donizeti Marques
Support Opportunities: Regular Research Grants