This paper contains a detailed literature review of research findings regarding the cause of flow-induced noise created by airfoils operating at low to moderate Reynolds numbers. There are many important engineering applications that operate at these conditions. More investigation is required to understand why airfoils in this range of Reynolds numbers produce high levels of tonal noise. As discussed in this paper, there are still many uncertainties surrounding the nature of the source.E. J. G. Arcondoulis, C. J. Doolan, A. C. Zander and L. A. Brook
International audienceCascade broadband trailing-edge noise is investigated experimentaly in an aera...
Available online 30 November 2015This study is concerned with the flow-induced noise of a smooth wal...
This paper proposes to study the flow and corresponding noise around a segment of an automotive blad...
AIAA 2011-2785A study of the effects of Reynolds number and angle of attack on the dominant acoustic...
If technology such as aircraft, submarines and wind turbines are to further reduce their noise emiss...
This paper describes the airfoil trailing edge noise generation mechanism and how flow over an airfo...
Airfoils operating at low-to-moderate Reynolds number may produce noise that contains one or more hi...
Direct numerical simulations are carried out to investigate the flow features responsible for second...
The aim of this study is to analyze the effects of trailing edge bluntness on airfoil tonal noise ge...
Airfoil trailing-edge noise up to a Reynolds number based on chord of 2.96 x 10 to the 6th power was...
Airfoils in low-to-moderate Reynolds number flows produce discrete tones which can be annoying to th...
Paper Number 47In order to produce aircraft, turbo-machinery and helicopters with low acoustic signa...
© 2016, © The Author(s) 2016. The aerodynamic and acoustic testing of a NACA0012 airfoil section was...
Airfoils in low-to-moderate Reynolds number flows produce a series of tones that can be annoying to ...
International audienceCascade broadband trailing-edge noise is investigated experimentaly in an aera...
International audienceCascade broadband trailing-edge noise is investigated experimentaly in an aera...
Available online 30 November 2015This study is concerned with the flow-induced noise of a smooth wal...
This paper proposes to study the flow and corresponding noise around a segment of an automotive blad...
AIAA 2011-2785A study of the effects of Reynolds number and angle of attack on the dominant acoustic...
If technology such as aircraft, submarines and wind turbines are to further reduce their noise emiss...
This paper describes the airfoil trailing edge noise generation mechanism and how flow over an airfo...
Airfoils operating at low-to-moderate Reynolds number may produce noise that contains one or more hi...
Direct numerical simulations are carried out to investigate the flow features responsible for second...
The aim of this study is to analyze the effects of trailing edge bluntness on airfoil tonal noise ge...
Airfoil trailing-edge noise up to a Reynolds number based on chord of 2.96 x 10 to the 6th power was...
Airfoils in low-to-moderate Reynolds number flows produce discrete tones which can be annoying to th...
Paper Number 47In order to produce aircraft, turbo-machinery and helicopters with low acoustic signa...
© 2016, © The Author(s) 2016. The aerodynamic and acoustic testing of a NACA0012 airfoil section was...
Airfoils in low-to-moderate Reynolds number flows produce a series of tones that can be annoying to ...
International audienceCascade broadband trailing-edge noise is investigated experimentaly in an aera...
International audienceCascade broadband trailing-edge noise is investigated experimentaly in an aera...
Available online 30 November 2015This study is concerned with the flow-induced noise of a smooth wal...
This paper proposes to study the flow and corresponding noise around a segment of an automotive blad...