Abstract
Horizontal Axis Wind Turbines are operated with different safety mechanisms which protect the wind turbines from overloading during strong wind situations. However, wind turbines may collapse due to sudden gust events or other overload situations. An additional safety measure may be an aerodynamic load limit of the airfoils themselves by adding passive lift limiting devices to the wing. Ideally, these devices would not add extra drag and the aerodynamic performance will maintain in the normal operation range of the wings. The investigated small radii or ‘noses’ added to the leading edge of a laminar airfoil shows very promising results: the lift limit can be adjusted by the shape, position and spanwise distribution of the added ‘nose’. Additional drag can be kept to a minimum within a certain operation range of the airfoil, depending on the geometrical characteristics of the added nose.
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References
Meyer, O., Terreblanche, T., Klein, M.: Optimized experimental environment for wing profile investigations in the low speed wind tunnel. In: Proceedings of the 5th International Conference on Experimental Fluid Mechanics, Munich, Germany, pp. 728–733 (2018)
Terreblanche, T.: Optimization of profile polars for wind turbine rotor blades with the use of leading-edge vortex generators. TU Braunschweig, Master Thesis (2017)
Sun, Y.: Wind Turbine Blade with Tripping Device and Method Thereof, European Patent Application, EP 3 133 281 A1 (2017)
Meyer, O., Terreblanche, T., Klein, M.: Wing Profile Investigations in the Low Speed Wind Tunnel of the UniBwM, Deutscher Luft- und Raumfahrtkongress 2018. In: Conference Proceedings (2018)
Jones, B.M.: The Measurement of Profile Drag by the Pitot Traverse Method. ARC Rep. and Mem. Nr. 1688 (1936)
Garner, H.C., Rogers, E.W.E., Acum, W.E.A., Maskell, E.C. (ed.) Subsonic Wind Tunnel Wall Corrections, AGARDograph 109, NATO (1966)
Tüchsen, Th.: Analyse des Göttinger Windkanals zur Bestimmung von Profilpolaren und Validierung der 2D-Windkanalkorrekturen. Master Thesis, Universität der Bundeswehr München (2020)
Drela, M., Youngren, H.: Xfoil 6.9, General Description. MIT, Cambridge (2001)
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Meyer, O. (2021). On the Effectiveness of Retrofitted Airfoil Leading Edge Devices to Limit Lift. In: Dillmann, A., Heller, G., Krämer, E., Wagner, C. (eds) New Results in Numerical and Experimental Fluid Mechanics XIII. STAB/DGLR Symposium 2020. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol 151. Springer, Cham. https://doi.org/10.1007/978-3-030-79561-0_69
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DOI: https://doi.org/10.1007/978-3-030-79561-0_69
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