Steady aerodynamic simulation of a high-lift geometry by meams of a hybrid euler/integral boundary layer code (2011)
- Authors:
- USP affiliated authors: MEDEIROS, MARCELLO AUGUSTO FARACO DE - EESC ; SOUZA, DANIEL SAMPAIO - EESC
- Unidade: EESC
- Subjects: AERODINÂMICA DE AERONAVES; ENGENHARIA AERONÁUTICA
- Language: Inglês
- Imprenta:
- Publisher: ABCM
- Publisher place: Rio de Janeiro, RJ
- Date published: 2011
- Source:
- Título: Proceedings of COBEM
- ISSN: 2176-5480
- Conference titles: International Congress of Mechanical Engineering - COBEM
-
ABNT
SOUZA, Daniel Sampaio e MEDEIROS, Marcello Augusto Faraco de. Steady aerodynamic simulation of a high-lift geometry by meams of a hybrid euler/integral boundary layer code. 2011, Anais.. Rio de Janeiro, RJ: ABCM, 2011. Disponível em: https://repositorio.usp.br/directbitstream/6e49e879-a73f-4d4f-9de3-7fab0c7cc644/trabalho%2047%20-%20Steady%20Aerodynamic%20Simulation%20of%20a%20High-Lift%20Geometry%20by%20Means%20of%20a%20Hybrid%20Euler-IBL%20Code%20%28COBEM%202011%29.pdf. Acesso em: 29 dez. 2025. -
APA
Souza, D. S., & Medeiros, M. A. F. de. (2011). Steady aerodynamic simulation of a high-lift geometry by meams of a hybrid euler/integral boundary layer code. In Proceedings of COBEM. Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/6e49e879-a73f-4d4f-9de3-7fab0c7cc644/trabalho%2047%20-%20Steady%20Aerodynamic%20Simulation%20of%20a%20High-Lift%20Geometry%20by%20Means%20of%20a%20Hybrid%20Euler-IBL%20Code%20%28COBEM%202011%29.pdf -
NLM
Souza DS, Medeiros MAF de. Steady aerodynamic simulation of a high-lift geometry by meams of a hybrid euler/integral boundary layer code [Internet]. Proceedings of COBEM. 2011 ;[citado 2025 dez. 29 ] Available from: https://repositorio.usp.br/directbitstream/6e49e879-a73f-4d4f-9de3-7fab0c7cc644/trabalho%2047%20-%20Steady%20Aerodynamic%20Simulation%20of%20a%20High-Lift%20Geometry%20by%20Means%20of%20a%20Hybrid%20Euler-IBL%20Code%20%28COBEM%202011%29.pdf -
Vancouver
Souza DS, Medeiros MAF de. Steady aerodynamic simulation of a high-lift geometry by meams of a hybrid euler/integral boundary layer code [Internet]. Proceedings of COBEM. 2011 ;[citado 2025 dez. 29 ] Available from: https://repositorio.usp.br/directbitstream/6e49e879-a73f-4d4f-9de3-7fab0c7cc644/trabalho%2047%20-%20Steady%20Aerodynamic%20Simulation%20of%20a%20High-Lift%20Geometry%20by%20Means%20of%20a%20Hybrid%20Euler-IBL%20Code%20%28COBEM%202011%29.pdf - A study of the sources of slat noise using proper orthogonal decomposition
- On detrimental effects of excrescences on the slat noise
- Proper orthogonal decomposition analysis of noise generation mechanisms in the slat cove
- On the small effect of boundary layer thicknesses on slat noise
- Large scale structures and noise generation in leading edge slat of high lift airfoils
- Experimental investigation on the effect of slat geometrical configurations on aerodynamic noise
- Numerical study of the large scale turbulent structures responsible for slat noise generation
- Simulação numérica de ruído de eslate em configurações práticas usando um código comercial
- Estudo experimental do efeito aeroacústico de uma excrescência bidimensional na cova do eslate
- Computational analysis of a aeroacoustic effect of a seal on slat cove for different angles of attack
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