The design and testing of a winglet airfoil for low-speed aircraft

Mark David Maughmer, Timothy S. Swan, Steven M. Willits

Research output: Contribution to conferencePaper

5 Scopus citations

Abstract

The PSU 94-097 airfoil has been designed for use on winglets of high-performance sailplanes. The design problem is difficult because the airfoil must operate over a wide range of Reynolds numbers, and this range includes values that are relatively low. To validate the design tools, as well as the design itself, the airfoil was tested in the Penn State Low-Speed, Low-Turbulence Wind Tunnel from Reynolds numbers of 2.4 × 105 to 1.0 × 106. In addition to transition-free measurements, potential drag reductions using artificial turbulators were explored, although the benefits were found to be limited for this application. Finally, performance predictions from two well-known computer codes are compared to the data obtained experimentally, and both are found to generate results that are in good agreement with the wind-tunnel measurements.

Original languageEnglish (US)
StatePublished - Dec 1 2001
Event19th AIAA Applied Aerodynamics Conference 2001 - Anaheim, CA, United States
Duration: Jun 11 2001Jun 14 2001

Other

Other19th AIAA Applied Aerodynamics Conference 2001
CountryUnited States
CityAnaheim, CA
Period6/11/016/14/01

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Mechanical Engineering

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  • Cite this

    Maughmer, M. D., Swan, T. S., & Willits, S. M. (2001). The design and testing of a winglet airfoil for low-speed aircraft. Paper presented at 19th AIAA Applied Aerodynamics Conference 2001, Anaheim, CA, United States.