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Gurney Flaps in Transonic Flows

  • Henning Rosemann
  • Kai Richter
Part of the Fluid Mechanics and its Applications book series (FMIA, volume 73)

Abstract

The application of Gurney flaps to airfoils, high aspect ratio wings and delta wings in transonic flow is being investigated at the Institute of Aerodynamics and Flow Technology of DLR. The present paper gives an overview over these studies explaining the basic working principles and advantages of these trailing edge devices at transonic Mach numbers. Numerical studies confirmed by wind tunnel experiments show similar global effects as conventional trailing edge flaps, with the additional advantage of a reduction of the adverse pressure gradient on the upper side of the airfoil towards the trailing edge.

Keywords

Gurney Flaps Trailing Edge Device Transonic Airfoil Delta Wing 

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References

  1. Bechert, D. W., Meyer, R., and Hage, W. (2000). Drag Reduction of Airfoils with Miniflaps. Can We Learn from Dragonflies? AIAA-2000-2315, AIAA Fluids 2000 Conference and Exhibit, (Denver, CO).Google Scholar
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Copyright information

© Springer Science+Business Media Dordrecht 2003

Authors and Affiliations

  • Henning Rosemann
    • 1
  • Kai Richter
    • 1
  1. 1.Institute of Aerodynamics and Flow Technology DLRGöttingenGermany

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