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Thick, two-dimensional wake roll-up behind a wing of finite span—extended calculations

Published online by Cambridge University Press:  04 July 2016

H. Portnoy*
Affiliation:
Department of Aeronautical Engineering, Technion-lsrael Institute of Technology, Haifa

Extract

Reference 1 describes a numerical procedure for calculating the roll-up of the wake behind a wing of finite span, when the wake vorticity is assumed to occur within a layer of finite thickness with thin elliptic cross-section normal to the stream. The vorticity is assumed to be a function of spanwise position only (corresponding to a linear transverse velocity profile when the wake is thin), the process is treated as a two-dimensional unsteady one, as in the work of Westwater, Moore and others, and viscous and turbulence effects are ignored.

In Ref. 1 the technique was applied to the classical elliptic loading, to calculate the very early stages of the roll-up. In the present paper these calculations are extended to larger values of the dimensionless time t* and the results are seen to tally fairly well with those of Moore, which were obtained by using a point-vortex model. Similar calculations have also been carried out for a particular non-elliptic loading which was dealt with by Clements and Maull by a two-dimensional, point-vortex method. They gave this loading as an example of a distribution which produces two roll-up cores on each half span, with an induced drag only 10% greater than that of the elliptic loading having the same Ch. The results of the new calculations are presented here, and are seen to be similar to those of Ref. 4 in a general way, both qualitatively and quantitatively.

Type
Technical note
Copyright
Copyright © Royal Aeronautical Society 1977 

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References

1. Portnoy, H. The initial roll-up of a thick, two-dimensional wake behind a wing of finite span. The Aeronautical Journal, Vol 80, No 790, pp 442447, October 1976.Google Scholar
2. Westwater, F. L. The rolling up of the surface of discontinuity behind an aerofoil of finite span. British ARC R&M 1692, 1935.Google Scholar
3. Moore, D. W. A numerical study of the roll-up of a finite vortex sheet. Fluid Mech, Vol 63, Part 2, pp 225235, 1974.Google Scholar
4. Clements, R. R. and Maull, D. J. The rolling-up of a trailing vortex sheet. The Aeronautical Journal, Vol 77, No 745, pp 4651, January 1973.Google Scholar
5. Kaden, H. Aufwicklung eines unstabilen Unstetigkeits- flache. Ing Archiv, Vol 2, pp 140168, May 1931.Google Scholar
6. Cliffone, D. L. and Orloff, K. L. Far-field wake- vortex characteristics of wings. Journal of Aircraft, Vol 12, pp 464470, May 1975.Google Scholar