Mitigating dynamic stall with a movable leading-edge: the NACA0012-IK30 wing (2024)
- Authors:
- Autor USP: MARQUES, FLAVIO DONIZETI - EESC
- Unidade: EESC
- Subjects: ROTOR; ASAS DE AERONAVES; PROPULSÃO; AERODINÂMICA DE AERONAVES; ENGENHARIA MECÂNICA
- Agências de fomento:
- Language: Inglês
- Imprenta:
- Publisher place: Edinburgh, UK
- Date published: 2024
- Source:
- Título: Proceedings
- Conference titles: Congress of the International Council of the Aeronautical Sciences - ICAS
-
ABNT
CAMACHO, Emanuel A. R. e SILVA, Andre R. R e MARQUES, Flavio Donizeti. Mitigating dynamic stall with a movable leading-edge: the NACA0012-IK30 wing. 2024, Anais.. Edinburgh, UK: Escola de Engenharia de São Carlos, Universidade de São Paulo, 2024. Disponível em: https://repositorio.usp.br/directbitstream/8eedf42a-b8a2-445f-9ead-f598734f1a02/icas2024_0595_paper.pdf. Acesso em: 12 jan. 2026. -
APA
Camacho, E. A. R., Silva, A. R. R., & Marques, F. D. (2024). Mitigating dynamic stall with a movable leading-edge: the NACA0012-IK30 wing. In Proceedings. Edinburgh, UK: Escola de Engenharia de São Carlos, Universidade de São Paulo. Recuperado de https://repositorio.usp.br/directbitstream/8eedf42a-b8a2-445f-9ead-f598734f1a02/icas2024_0595_paper.pdf -
NLM
Camacho EAR, Silva ARR, Marques FD. Mitigating dynamic stall with a movable leading-edge: the NACA0012-IK30 wing [Internet]. Proceedings. 2024 ;[citado 2026 jan. 12 ] Available from: https://repositorio.usp.br/directbitstream/8eedf42a-b8a2-445f-9ead-f598734f1a02/icas2024_0595_paper.pdf -
Vancouver
Camacho EAR, Silva ARR, Marques FD. Mitigating dynamic stall with a movable leading-edge: the NACA0012-IK30 wing [Internet]. Proceedings. 2024 ;[citado 2026 jan. 12 ] Available from: https://repositorio.usp.br/directbitstream/8eedf42a-b8a2-445f-9ead-f598734f1a02/icas2024_0595_paper.pdf - Aeroelastic analysis and nonlinear characterization of three-degree-of-freedom systems with discontinuous nonlinearities
- Fast flapping aerodynamics prediction using a recurrent neural network
- Predicting the NACA0012-IK30 airfoil propulsive capabilities with a panel method
- Nonlinear supersonic post-flutter motion of panels with adjacent bays and thermal effects
- Nonlinear multibay panel flutter evaluation of composite laminates with curvilinear fibers
- The South Atlantic aerial crossing of João Ribeiro de Barros in 1927
- Aeroelastic tailoring of nonlinear typical section using the method of multiple scales to predict post-flutter stable LCOs
- Modeling and dynamic characterization of nonlinear non-smooth aeroviscoelastic systems
- Nonlinear finite element aeroelastic analysis of multibay panels in supersonic flow regime
- Power extraction from stall-induced oscillations of an airfoil
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