Articles | Volume 6, issue 1
https://doi.org/10.5194/wes-6-221-2021
© Author(s) 2021. This work is distributed under
the Creative Commons Attribution 4.0 License.
the Creative Commons Attribution 4.0 License.
https://doi.org/10.5194/wes-6-221-2021
© Author(s) 2021. This work is distributed under
the Creative Commons Attribution 4.0 License.
the Creative Commons Attribution 4.0 License.
Pressure-based lift estimation and its application to feedforward load control employing trailing-edge flaps
Sirko Bartholomay
CORRESPONDING AUTHOR
Institute of Fluid Dynamics and Technical Acoustics, TU Berlin, Berlin, Germany
Tom T. B. Wester
ForWind, Institute of Physics, University of Oldenburg, Oldenburg, Germany
Sebastian Perez-Becker
Institute of Fluid Dynamics and Technical Acoustics, TU Berlin, Berlin, Germany
Simon Konze
Leibniz Institute of Polymer Research Dresden, Workgroup Complex Structural Components, Dresden, Germany
Christian Menzel
Institute of Fluid Dynamics and Technical Acoustics, TU Berlin, Berlin, Germany
Michael Hölling
ForWind, Institute of Physics, University of Oldenburg, Oldenburg, Germany
Axel Spickenheuer
Leibniz Institute of Polymer Research Dresden, Workgroup Complex Structural Components, Dresden, Germany
Joachim Peinke
ForWind, Institute of Physics, University of Oldenburg, Oldenburg, Germany
Christian N. Nayeri
Institute of Fluid Dynamics and Technical Acoustics, TU Berlin, Berlin, Germany
Christian Oliver Paschereit
Institute of Fluid Dynamics and Technical Acoustics, TU Berlin, Berlin, Germany
Kilian Oberleithner
Institute of Fluid Dynamics and Technical Acoustics, TU Berlin, Berlin, Germany
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Cited
13 citations as recorded by crossref.
- Development and assessment of a method to determine the angle of attack on an operating wind turbine by matching onboard pressure measurements with panel method simulations R. Soto-Valle et al. 10.1051/e3sconf/202131208003
- Experimental assessment of a blended fatigue‐extreme controller employing trailing edge flaps S. Bartholomay et al. 10.1002/we.2795
- Model-free control of the dynamic lift of a wind turbine blade section: experimental results L. Michel et al. 10.1088/1742-6596/2265/3/032068
- An Experimental Study on Rotor Aerodynamic Noise Control Based on Active Flap Control Z. Hu et al. 10.3390/aerospace10020121
- Rotational and blockage effects on a wind turbine model based on local blade forces R. Soto-Valle et al. 10.1088/1742-6596/2265/2/022102
- Validation of a RANS Turbulence Model for a S833 Wind Turbine Airfoil With a Trailing Edge Flap Using Oil Visualization and Pressure Taps R. Jami & D. Johnson 10.1115/1.4064853
- Pressure Feedback Control of Aerodynamic Loads on a Delta Wing in Transverse Gusts X. He & D. Williams 10.2514/1.J062442
- A Novel Lift Controller for a Wind Turbine Blade Section Using an Active Flow Control Device Including Saturations: Experimental Results L. Michel et al. 10.1109/TCST.2023.3345208
- On optimizing the sensor spacing for pressure measurements on wind turbine airfoils E. Fritz et al. 10.5194/wes-9-1713-2024
- Active flap control with the trailing edge flap hinge moment as a sensor: using it to estimate local blade inflow conditions and to reduce extreme blade loads and deflections S. Perez-Becker et al. 10.5194/wes-6-791-2021
- Interference mechanism of trailing edge flap shedding vortices with rotor wake and aerodynamic characteristics Y. LIU et al. 10.1016/j.cja.2024.07.036
- Repetitive model predictive control for load alleviation on a research wind turbine using trailing edge flaps S. Bartholomay et al. 10.1002/we.2730
- Lift coefficient estimation for a rapidly pitching airfoil X. An et al. 10.1007/s00348-020-03105-3
12 citations as recorded by crossref.
- Development and assessment of a method to determine the angle of attack on an operating wind turbine by matching onboard pressure measurements with panel method simulations R. Soto-Valle et al. 10.1051/e3sconf/202131208003
- Experimental assessment of a blended fatigue‐extreme controller employing trailing edge flaps S. Bartholomay et al. 10.1002/we.2795
- Model-free control of the dynamic lift of a wind turbine blade section: experimental results L. Michel et al. 10.1088/1742-6596/2265/3/032068
- An Experimental Study on Rotor Aerodynamic Noise Control Based on Active Flap Control Z. Hu et al. 10.3390/aerospace10020121
- Rotational and blockage effects on a wind turbine model based on local blade forces R. Soto-Valle et al. 10.1088/1742-6596/2265/2/022102
- Validation of a RANS Turbulence Model for a S833 Wind Turbine Airfoil With a Trailing Edge Flap Using Oil Visualization and Pressure Taps R. Jami & D. Johnson 10.1115/1.4064853
- Pressure Feedback Control of Aerodynamic Loads on a Delta Wing in Transverse Gusts X. He & D. Williams 10.2514/1.J062442
- A Novel Lift Controller for a Wind Turbine Blade Section Using an Active Flow Control Device Including Saturations: Experimental Results L. Michel et al. 10.1109/TCST.2023.3345208
- On optimizing the sensor spacing for pressure measurements on wind turbine airfoils E. Fritz et al. 10.5194/wes-9-1713-2024
- Active flap control with the trailing edge flap hinge moment as a sensor: using it to estimate local blade inflow conditions and to reduce extreme blade loads and deflections S. Perez-Becker et al. 10.5194/wes-6-791-2021
- Interference mechanism of trailing edge flap shedding vortices with rotor wake and aerodynamic characteristics Y. LIU et al. 10.1016/j.cja.2024.07.036
- Repetitive model predictive control for load alleviation on a research wind turbine using trailing edge flaps S. Bartholomay et al. 10.1002/we.2730
1 citations as recorded by crossref.
Latest update: 21 Nov 2024
Short summary
This paper presents two methods on how to estimate the lift force that is created by a wing. These methods were experimentally assessed in a wind tunnel. Furthermore, an active trailing-edge flap, as seen on airplanes for example, is used to alleviate fluctuating loads that are created within the employed wind tunnel. Thereby, an active flow control device that can potentially serve on wind turbines to lower fatigue or lower the material used for the blades is examined.
This paper presents two methods on how to estimate the lift force that is created by a wing....
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