Theoretical investigation of unsteady nonlinear aerodynamics

• Grant number: 18/05247-8
• Support Opportunities: Scholarships abroad - Research Internship - Doctorate (Direct)
• Start date: January 01, 2019
• End date: December 31, 2019
• Field of knowledge: Engineering - Aerospace Engineering - Aerospace Systems
• Principal Investigator: Flávio Donizeti Marques
• Grantee: Carlos Renan dos Santos
• Supervisor: Haithem Ezzat Mohammed Taha
• Host Institution: Escola de Engenharia de São Carlos (EESC). Universidade de São Paulo (USP). São Carlos , SP, Brazil
• Institution abroad: University of California, Irvine (UC Irvine), United States
• Associated to the scholarship: 17/09468-6 - Optimization of the energy harvesting from airfoil stall induced oscillations, BP.DD

Abstract

The optimization of an energy harvester from stall-induced oscillations, such as proposed in the ongoing doctoral project (FAPESP project 2017/09468-6), requires an accurate and fast aerodynamic model. This modeling must be able to capture non-linearities associated with dynamic stall effects. Furthermore, when a harvester with finite span is considered, the aerodynamic analyses need to account for three-dimensional wing effects. However, the development of low-cost methodologies for accurate and fast prediction of unsteady nonlinear loads in three-dimensional wings remains a challenge. In this sense, the present project proposes the implementation and validation of a computational model to predict the nonlinear unsteady aerodynamic behavior of a three-dimensional wing undergoing oscillations at high angles of attack. Such methodology will be validated against high-fidelity computations and experiments. The development of this research project will result in an aerodynamic code to be coupled to the aeroelastic model used for the optimization process of an energy harvester from stall-induced oscillations. (AU)

Scientific publications

(6)

(References retrieved automatically from Web of Science and SciELO through information on FAPESP grants and their corresponding numbers as mentioned in the publications by the authors)

DOS SANTOS, CARLOS RENAN; MARQUES, FLAVIO DONIZETI. Finite wing effects on the energy harvesting from stall-induced oscillations. JOURNAL OF VIBRATION AND CONTROL, v. N/A, p. 17-pg., 2022-05-12. (18/05247-8, 17/09468-6, 17/02926-9)

DOS SANTOS, CARLOS R.; MARQUES, FLAVIO D.. Stall-Induced Oscillations of Typical Aeroelastic Sections in Low Airspeeds. AIAA SCITECH 2019 FORUM, v. N/A, p. 11-pg., 2019-01-01. (17/09468-6, 17/02926-9, 18/05247-8)

IZQUIERDO, D. O. D.; DOS SANTOS, C. R.; MARQUES, F. D.; DESMET, W; PLUYMERS, B; MOENS, D; VANDEMAELE, S. Nonlinear oscillations of a low Reynolds SD7003 airfoil at higher angles of attack. PROCEEDINGS OF INTERNATIONAL CONFERENCE ON NOISE AND VIBRATION ENGINEERING (ISMA2020) / INTERNATIONAL CONFERENCE ON UNCERTAINTY IN STRUCTURAL DYNAMICS (USD2020), v. N/A, p. 12-pg., 2020-01-01. (18/05247-8, 17/09468-6, 17/02926-9)

DOS SANTOS, CARLOS R.; PACHECO, DOUGLAS R. Q.; TAHA, HAITHEM E.; ZAKARIA, MOHAMED Y.. Nonlinear modeling of electro-aeroelastic dynamics of composite beams with piezoelectric coupling. COMPOSITE STRUCTURES, v. 255, JAN 1 2021. (17/09468-6, 18/05247-8)

DOS SANTOS, C. R.; REZAEI, A. S.; TAHA, H. E.. iscous extension of vortex methods for unsteady aerodynamic. Physics of Fluids, v. 33, n. 10, OCT 2021. (18/05247-8, 17/09468-6)

DOS SANTOS, CARLOS R.; PACHECO, DOUGLAS R. Q.; ZAKARIA, MOHAMED Y.; TAHA, HAITHEM E.. Modeling Nonlinear Unsteady Aeroelastic Characteristics of Cantilevered Beams with Piezoelectric Coupling. AIAA SCITECH 2020 FORUM, v. N/A, p. 9-pg., 2020-01-01. (17/09468-6, 18/05247-8)