The contribution provides an overview on accomplished wind tunnel testing and simulation activity within the German national wind energy project BELARWEA. The project aimed at numerical tool development and validation to support the design of both aerodynamically efficient and low-noise wind turbine rotors. The focus was set on the tip region, herein defined as the outer 20 % of the rotor radius, i.e. addressing noise generation from the trailing-edge- and tip vortex regions. Aeroacoustically driven 2D profile design, 3D winglet design and 2D/3D CFD/CAA analysis were supplemented by the transfer of passive noise reduction technologies from aerospace applications to wind turbine blades. Validation experiments were performed in systematic e...
A major limitation on the use of wind turbines in Europe is their noise radiation. The amount of win...
Noise emission is one of the major concerns in wind turbine industry and especially for small scale ...
An experimental aero-acoustic characterisation of the NACA 633-018 airfoil is presented in this stud...
The trend to large wind turbines with increased blade diameters requires efficient noise reduction t...
The BMWi-funded wind energy project BELARWEA aims at the development and validation of improved meth...
Within the IEA Wind TCP Task 39 co-operational framework, aiming at consolidating knowledge on wind...
Results from a numerical and experimental aeroacoustic assessment of 2D wind turbine blade sections ...
Results from a numerical and experimental aeroacoustic assessment of 2D wind turbine blade sections ...
The here presented work is part of the HGF (Helmholtz Association of German Research Centres) -fund...
The aeroacoustic noise generated by wind turbines poses issues with the implementation of this renew...
This thesis deals with the acoustic simulation of wind turbine noise. Turbulent boundary layer trail...
Investigation of the effects blade pitch angle on noise emission from a horizontal axis wind turbine...
Investigation of blade tip shape effect on the noise emission from horizontal axis wind turbine is t...
The rotor of a large diameter wind turbine experiences more substantial and more dynamic loads due t...
Within the IEA Wind TCP Task 39 co-operational framework, aiming at consolidating knowledge on wind...
A major limitation on the use of wind turbines in Europe is their noise radiation. The amount of win...
Noise emission is one of the major concerns in wind turbine industry and especially for small scale ...
An experimental aero-acoustic characterisation of the NACA 633-018 airfoil is presented in this stud...
The trend to large wind turbines with increased blade diameters requires efficient noise reduction t...
The BMWi-funded wind energy project BELARWEA aims at the development and validation of improved meth...
Within the IEA Wind TCP Task 39 co-operational framework, aiming at consolidating knowledge on wind...
Results from a numerical and experimental aeroacoustic assessment of 2D wind turbine blade sections ...
Results from a numerical and experimental aeroacoustic assessment of 2D wind turbine blade sections ...
The here presented work is part of the HGF (Helmholtz Association of German Research Centres) -fund...
The aeroacoustic noise generated by wind turbines poses issues with the implementation of this renew...
This thesis deals with the acoustic simulation of wind turbine noise. Turbulent boundary layer trail...
Investigation of the effects blade pitch angle on noise emission from a horizontal axis wind turbine...
Investigation of blade tip shape effect on the noise emission from horizontal axis wind turbine is t...
The rotor of a large diameter wind turbine experiences more substantial and more dynamic loads due t...
Within the IEA Wind TCP Task 39 co-operational framework, aiming at consolidating knowledge on wind...
A major limitation on the use of wind turbines in Europe is their noise radiation. The amount of win...
Noise emission is one of the major concerns in wind turbine industry and especially for small scale ...
An experimental aero-acoustic characterisation of the NACA 633-018 airfoil is presented in this stud...