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Experimental determination of the aerodynamic characteristics of ski-jumpers

Published online by Cambridge University Press:  04 July 2016

A. J. Ward-Smith
Affiliation:
Department of Mechanical Engineering, Brunei University, Uxbridge
D. Clements
Affiliation:
Department of Mechanical Engineering, Brunei University, Uxbridge

Summary

The aerodynamic pitching moment, lift and drag forces acting on a ski-jumper during the free flight and landing phases were measured using scaled models in a wind tunnel. Comparisons are made between those meaurements and observations of actual ski-jumps.

It is shown that the high angles of incidence (typically α varies from 35° to 55°) adopted by ski-jumpers during free flight is determined by the need to prevent tumbling. Over this range of incidence angles, the opposing moments due to weight distribution and aerodynamic pressure distribution are approximately in equilibrium, and small out-of-balance moments can be accommodated by arm movements. The maximum lift/drag ratio on a ski-jumper in free flight occurs at α ≃ 25°. If it were possible to avoid tumbling at low incidence angles, maximum jump lengths would be achieved at α ≃ 8°.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1982 

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References

1. Clements, D. The aerodynamic forces acting on a ski-jumper. Brunei University Project Report (unpublished) 1981.Google Scholar
2. Pryor, S. J. The trajectory of objects subject to aerodynamic forces. Section 2: Ski jumpers. Brunei University Project Report (unpublished) 1980.Google Scholar
3. Raine, A. E. Aerodynamics of skiing. Science Journal. March 1970, 6, No 3, 2630.Google Scholar
4. Maskell, E. C. A theory of the blockage effects on bluff bodies and stalled wings in a closed wind tunnel ARC. R&M 3400, 1965.Google Scholar
5. Hoerner, S. F. Aerodynamic Drag, 1951.Google Scholar