Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)Conselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)The aim of this study is to analyze the effects of trailing edge bluntness on airfoil tonal noise generation and propagation at low Reynolds numbers. Several simulations are conducted for a NACA0012 airfoil at four different free-stream Mach numbers, = 0.2-0.5. The angle of incidence is set equal to 3A degrees, and the Reynolds number based on the airfoil chord is = 5,000. The effects of compressibility on sound generation...
A theory is developed for the influence of airfoil thickness on sound generated by the interaction o...
High-fidelity numerical simulations are carried out alongside analytical methods to investigate the ...
A wall-resolved large-eddy simulation of a symmetric Joukowski aerofoil with a 12 % thickness at a R...
The aim of this study is to analyze the effects of trailing edge bluntness on airfoil tonal noise ge...
Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)Fundação de Amparo à Pesquisa do Estado...
AIAA 2011-2785A study of the effects of Reynolds number and angle of attack on the dominant acoustic...
Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)Conselho Nacional de Desenvolvimento Ci...
Direct numerical simulations are carried out to investigate the flow features responsible for second...
Airfoils operating at low-to-moderate Reynolds number may produce noise that contains one or more hi...
Aerodynamic sound generation and self-noise mechanisms from lifting surfaces such as airfoil involve...
This paper contains a detailed literature review of research findings regarding the cause of flow-in...
The main objective of the present work is to investigate the mechanism of trailing-edge airfoil nois...
Flow-induced noise from fully submerged lifting bodies experienc-ing turbulent trailing edge flows c...
The aerodynamic and acoustic testing of a NACA0012 airfoil section was performed in an open wind tun...
In this article, airfoil trailing edge bluntness noise is investigated using both computational aero...
A theory is developed for the influence of airfoil thickness on sound generated by the interaction o...
High-fidelity numerical simulations are carried out alongside analytical methods to investigate the ...
A wall-resolved large-eddy simulation of a symmetric Joukowski aerofoil with a 12 % thickness at a R...
The aim of this study is to analyze the effects of trailing edge bluntness on airfoil tonal noise ge...
Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)Fundação de Amparo à Pesquisa do Estado...
AIAA 2011-2785A study of the effects of Reynolds number and angle of attack on the dominant acoustic...
Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)Conselho Nacional de Desenvolvimento Ci...
Direct numerical simulations are carried out to investigate the flow features responsible for second...
Airfoils operating at low-to-moderate Reynolds number may produce noise that contains one or more hi...
Aerodynamic sound generation and self-noise mechanisms from lifting surfaces such as airfoil involve...
This paper contains a detailed literature review of research findings regarding the cause of flow-in...
The main objective of the present work is to investigate the mechanism of trailing-edge airfoil nois...
Flow-induced noise from fully submerged lifting bodies experienc-ing turbulent trailing edge flows c...
The aerodynamic and acoustic testing of a NACA0012 airfoil section was performed in an open wind tun...
In this article, airfoil trailing edge bluntness noise is investigated using both computational aero...
A theory is developed for the influence of airfoil thickness on sound generated by the interaction o...
High-fidelity numerical simulations are carried out alongside analytical methods to investigate the ...
A wall-resolved large-eddy simulation of a symmetric Joukowski aerofoil with a 12 % thickness at a R...