The subject of this paper is the investigation of flow induced broadband noise generated due to unsteady loading of an airfoil. This is done in an experimental way based on acoustic measurements made on a rod-airfoil-configuration. The configuration is varied by changing the diameter of the rod and adjusting different gaps between the rod and the airfoil leading edge. Additionally, two types of airfoils are used sucessively. In total, 75 configurations are tested. All measurements are conducted in the aeroacoustic wind tunnel of the Brandenburg University of Technology at Cottbus for flow speeds between 26 m/s and 72 m/s. A 38 channel microphone array is used to record the acoustic data. The data are then processed using DAMAS, a complex be...
We experimentally investigate the comparability of airfoil trailing-edge noise measurements in an op...
The generation of tones from a NACA 0012 airfoil at zero angle of attack and Reynolds numbers of 50,...
AIAA 2014-3290This paper presents the results of an experimental investigation of the sound produced...
Paper Number 47In order to produce aircraft, turbo-machinery and helicopters with low acoustic signa...
International audienceIn open rotor applications, such as wind turbines and propellers, the angle of...
Airfoils in low-to-moderate Reynolds number flows produce a series of tones that can be annoying to ...
AIAA 2011-2785A study of the effects of Reynolds number and angle of attack on the dominant acoustic...
Airfoils in low-to-moderate Reynolds number flows produce discrete tones which can be annoying to th...
Trailing-edge serrations are passive noise reduction add-ons widely used in wind-turbine application...
The rod-airfoil configuration is a benchmark test case for aeroacoustic assessments of vortex- struc...
© 2016, © The Author(s) 2016. The aerodynamic and acoustic testing of a NACA0012 airfoil section was...
The broadband noise generated by the scattering of turbulent flow at the trailing edge of a NACA 001...
This thesis describes an investigation into the aeroacoustic noise produced by an aerofoil using ex...
The paper presents an experimental investigation of a turbulent boundary-layer interaction over a si...
International audienceThe present work investigates the noise emitted by an airfoil oscillating abov...
We experimentally investigate the comparability of airfoil trailing-edge noise measurements in an op...
The generation of tones from a NACA 0012 airfoil at zero angle of attack and Reynolds numbers of 50,...
AIAA 2014-3290This paper presents the results of an experimental investigation of the sound produced...
Paper Number 47In order to produce aircraft, turbo-machinery and helicopters with low acoustic signa...
International audienceIn open rotor applications, such as wind turbines and propellers, the angle of...
Airfoils in low-to-moderate Reynolds number flows produce a series of tones that can be annoying to ...
AIAA 2011-2785A study of the effects of Reynolds number and angle of attack on the dominant acoustic...
Airfoils in low-to-moderate Reynolds number flows produce discrete tones which can be annoying to th...
Trailing-edge serrations are passive noise reduction add-ons widely used in wind-turbine application...
The rod-airfoil configuration is a benchmark test case for aeroacoustic assessments of vortex- struc...
© 2016, © The Author(s) 2016. The aerodynamic and acoustic testing of a NACA0012 airfoil section was...
The broadband noise generated by the scattering of turbulent flow at the trailing edge of a NACA 001...
This thesis describes an investigation into the aeroacoustic noise produced by an aerofoil using ex...
The paper presents an experimental investigation of a turbulent boundary-layer interaction over a si...
International audienceThe present work investigates the noise emitted by an airfoil oscillating abov...
We experimentally investigate the comparability of airfoil trailing-edge noise measurements in an op...
The generation of tones from a NACA 0012 airfoil at zero angle of attack and Reynolds numbers of 50,...
AIAA 2014-3290This paper presents the results of an experimental investigation of the sound produced...