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The rolling up of a trailing vortex sheet

Published online by Cambridge University Press:  04 July 2016

R. R. Clements  and
D. J. Maull
R. R. Clements
Affiliation:
Cambridge University Engineering Department
D. J. Maull
Affiliation:
Cambridge University Engineering Department
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Extract

The rolling up of the vortex sheet shed from a finite aspect ratio wing into discrete vortices has been extensively investigated in the past. Most of these investigations have, however, considered wings having an elliptic loading.

The early design charts of Silvertstein et al gave downwash angles for a variety of flapped and unflapped aerofoils by considering the trailing vortex sheet to be composed of discrete line vortices but ignored the rolling up process that takes place.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 77 , Issue 745 , January 1973 , pp. 46 - 51
Copyright
Copyright © Royal Aeronautical Society 1973 

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References

1. Silverstein, et al. Design charts predicting downwash angles and wake characteristics behind plain and flapped wings. NACA Report 648. 1939.Google Scholar
2. Silverstein, et al. Downwash wake behind plain and flapped aerofoils. NACA Report 651. 1939.Google Scholar
3. Westwater, F. L. The rolling up of the surface of discontinuity behind an aerofoil of finite span. Aero. Res. Coun. R & M 1692. 1935.Google Scholar
4. Cone, C. A theoretical investigation of vortex sheet deformation behind a highly loaded wing. NASA TN-D-657 1960.Google Scholar
5. Rogers, A. W. Application of two-dimensional vortex theory to the predction of flow fields behind wings of wing-body combinations at subsonic and supersonic speeds. NACA TN 3227. 1954.Google Scholar
6. Hancock, G. J. On rolling up of a trailing vortex sheet. The Aeronautical Journal of the Royal Aeronautical Society, Vol 74, No 717. 1970.Google Scholar
7. Hancock, G. J. and Butter, D. J. A numerical method for calculating the trailing vortex system behind a sweptwing at low speed. The Aeronautical Journal of the Royal Aeronautical Society, Vol 75, No 728. 1971.Google Scholar
8. Hackett, J. F. and Evans, M. R. Vortex wakes behind high lift wings. Journal of Aircraft, Vol 8, No 5. 1971.Google Scholar