FRISBEE AERODYNAMICS
(AIAA-2002-3150)


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Jonathan R. Potts & William J. Crowther
Aerospace Group, School of Mechanical, Aerospace and Civil Engineering, University of Manchester, UK

Abstract
The frisbee-like flying sports disc is a spin-stabilised axi-symmetric wing of quite remarkable design. The disc generates lift through forward velocity just like a conventional wing. From a backhand throw, spin is naturally given to the disc, which stabilises it in free-flight. This experimental investigation of a typical flying disc shape outlines wind-tunnel data including plots of aerodynamic loads verses angle of attack (AoA) which are compared to existing data in the literature, the effect of spin is also presented. The surface pressure distribution is presented as pressure profiles at the halfspan station and colour filled contour plots for both the upper and cavity surfaces. Surface and smoke wire flow visualisation techniques provide an explanation of flow structures which compare well with the pressure distributions. The asymmetries observed in the trailing vortices, for a spinning disc, allow an explanation of the aerodynamic generation of the rolling moment and side force. The free-flight of a flying disc is discussed based on the above.

Reference in Full
Potts J.R. & Crowther W.J.: FrisbeeTM Aerodynamics, AIAA 2002-3150, 20th AIAA Applied Aero. Conf. & Exhibit, St. Louis, MO, June 2002.

The following document selection gives a detailed description of the research carried out up until January 2003. The more recent work will be posted as soon as possible.

FRISBEE AERODYNAMICS
(AIAA-2002-3150)

APPLICATION OF FLOW CONTROL TO A DISC-WING UAV

FLIGHT CONTROL OF A SPIN STABILISED AXI-SYMMETRIC DISC-WING (AIAA-2001-0253)

VISUALISATION OF THE FLOW OVER A DISC-WING (Paper 247)

THE FLOW OVER A ROTATING DISC-WING

STABILISING THE SPIN
(Magazine Article)

DISC-WING AERODYNAMICS
(Poster)

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