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Numerical investigation of an airfoil under light dynamic stall

Grant number: 22/08567-9
Support Opportunities:Scholarships in Brazil - Master
Start date: September 01, 2022
End date: January 31, 2025
Field of knowledge:Engineering - Aerospace Engineering - Aerodynamics
Principal Investigator:William Roberto Wolf
Grantee:Lucas Feitosa de Souza
Host Institution: Faculdade de Engenharia Mecânica (FEM). Universidade Estadual de Campinas (UNICAMP). Campinas , SP, Brazil
Associated research grant:21/06448-0 - High-fidelity numerical simulations applied in unsteady aerodynamics, turbulence and aeroacoustics, AP.JP2
Associated scholarship(s):23/13599-0 - Study of numerical techniques for flow analysis and control of airfoils under dynamic stall, BE.EP.MS

Abstract

Dynamic stall occurs when a moving airfoil rapidly exceeds its static stall angle of attack. The outcome is an increase in the unsteady loads accompanied by large torsional forces and mechanical vibrations on the wing or blade. This condition has significant influence on the performance and fatigue of several mechanical systems, such as helicopter blades, wind turbines and flapping wing aerial vehicles. Hence, the study of dynamic stall on pitching airfoils is of paramount importance to predict the performance parameters. The process of dynamic stall is highly sensitive to flow conditions such as compressibility and inertial/viscous effects, rate of motion and airfoil geometry. The main objective of the present work is the study of airfoils under light dynamic stall for which negative aerodynamic damping occurs. In these cases, the structure absorbs energy from the unsteady aerodynamic flow. High fidelity numerical simulations will be conducted to investigate the effects of compressibility on aerodynamic damping and flow modal decomposition will be employed to understand the relevant frequencies associated with dynamic stall onset.

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Scientific publications (5)
(The scientific publications listed on this page originate from the Web of Science or SciELO databases. Their authors have cited FAPESP grant or fellowship project numbers awarded to Principal Investigators or Fellowship Recipients, whether or not they are among the authors. This information is collected automatically and retrieved directly from those bibliometric databases.)
FEITOSA, LUCAS; MIOTTO, RENATO; WOLF, WILLIAM. Analysis of coherent structures in dynamic stall via empirical mode decomposition and dynamic mode decomposition. AIAA AVIATION 2023 FORUM, v. N/A, p. 12-pg., . (22/08567-9, 13/08293-7, 21/06448-0, 22/09196-4, 13/07375-0)
FEITOSA, LUCAS; MIOTTO, RENATO; WOLF, WILLIAM. Analysis of dynamic stall for a simplified single blade vertical axis wind turbine configuration. AIAA AVIATION FORUM AND ASCEND 2024, v. N/A, p. 10-pg., . (22/08567-9, 13/07375-0, 13/08293-7, 22/09196-4, 21/06448-0)
DE SOUZA, LUCAS FEITOSA; WOLF, WILLIAM; SAFARI, MARYAM; YEH, CHI-AN. Control of Deep Dynamic Stall by Duty-Cycle Actuation Informed by Stability Analysis. AIAA JOURNAL, v. N/A, p. 12-pg., . (21/06448-0, 22/08567-9, 23/13599-0, 13/08293-7, 19/17874-0)
DE SOUZA, LUCAS FEITOSA; MIOTTO, RENATO FUZARO; WOLF, WILLIAM ROBERTO. Active flow control of vertical-axis wind turbines: Insights from large-eddy simulation and finite-time resolvent analysis. JOURNAL OF FLUIDS AND STRUCTURES, v. 139, p. 18-pg., . (19/17874-0, 24/20547-9, 13/08293-7, 22/08567-9, 22/09196-4, 21/06448-0)
FEITOSA, LUCAS; MIOTTO, RENATO; WOLF, WILLIAM. Analysis of intermittent vortex pairing for a transitional flow past a NACA0012 airfoil via a multidimensional empirical mode decomposition. AIAA AVIATION FORUM AND ASCEND 2024, v. N/A, p. 9-pg., . (13/08293-7, 22/09196-4, 21/06448-0, 22/08567-9)
Academic Publications
(References retrieved automatically from State of São Paulo Research Institutions)
SOUZA, Lucas Feitosa de. Análise de estol dinâmico por meio de abordagens baseadas em dados e princípios físicos. 2025. Master's Dissertation - Universidade Estadual de Campinas (UNICAMP). Faculdade de Engenharia Mecânica Campinas, SP.