Skip to main content

On the Effectiveness of Retrofitted Airfoil Leading Edge Devices to Limit Lift

  • Conference paper
  • First Online:
New Results in Numerical and Experimental Fluid Mechanics XIII (STAB/DGLR Symposium 2020)

Part of the book series: Notes on Numerical Fluid Mechanics and Multidisciplinary Design ((NNFM,volume 151))

Included in the following conference series:

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.

This is a preview of subscription content, log in via an institution to check access.

Access this chapter

Chapter
USD 29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD 169.00
Price excludes VAT (USA)
  • Available as EPUB and PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD 219.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info
Hardcover Book
USD 219.99
Price excludes VAT (USA)
  • Durable hardcover edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Purchases are for personal use only

Institutional subscriptions

References

  1. 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)

    Google Scholar 

  2. Terreblanche, T.: Optimization of profile polars for wind turbine rotor blades with the use of leading-edge vortex generators. TU Braunschweig, Master Thesis (2017)

    Google Scholar 

  3. Sun, Y.: Wind Turbine Blade with Tripping Device and Method Thereof, European Patent Application, EP 3 133 281 A1 (2017)

    Google Scholar 

  4. 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)

    Google Scholar 

  5. Jones, B.M.: The Measurement of Profile Drag by the Pitot Traverse Method. ARC Rep. and Mem. Nr. 1688 (1936)

    Google Scholar 

  6. Garner, H.C., Rogers, E.W.E., Acum, W.E.A., Maskell, E.C. (ed.) Subsonic Wind Tunnel Wall Corrections, AGARDograph 109, NATO (1966)

    Google Scholar 

  7. Tüchsen, Th.: Analyse des Göttinger Windkanals zur Bestimmung von Profilpolaren und Validierung der 2D-Windkanalkorrekturen. Master Thesis, Universität der Bundeswehr München (2020)

    Google Scholar 

  8. Drela, M., Youngren, H.: Xfoil 6.9, General Description. MIT, Cambridge (2001)

    Google Scholar 

Download references

Acknowledgements

The author would like to thank M.Eng. Marten Danker, staff member of the authors Fluid Dynamics group, for his support and contribution of the graphics in Fig. 10 and measurement data for Fig. 11.

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Oliver Meyer .

Editor information

Editors and Affiliations

Rights and permissions

Reprints and permissions

Copyright information

© 2021 The Author(s), under exclusive license to Springer Nature Switzerland AG

About this paper

Check for updates. Verify currency and authenticity via CrossMark

Cite this paper

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

Download citation

  • DOI: https://doi.org/10.1007/978-3-030-79561-0_69

  • Published:

  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-030-79560-3

  • Online ISBN: 978-3-030-79561-0

  • eBook Packages: EngineeringEngineering (R0)

Publish with us

Policies and ethics