The study of visualization by smoke of vortex structures on the upper surface of an aircraft fuselage
Article Type: Research Article

Abene Abderrahane

University of Valenciennes and Hainaut Cambresis, France

Corresponding Author:

Dr. Abene Abderrahane

ISTV, University of Valenciennes

Mont- Huy, F-593014 Valenciennes


Received: 2015-11-03 ; Accepted: 2015-12-03 ; Published: 2015-12-14
Citation: Abderrahane A (2015) The study of visualization by smoke of vortex structures on the upper surface of an aircraft fuselage. JEn Sc ReTch 1:10441.
Copyright: © 2015 Abderrahane A. This is an open-access article distributed under the terms of the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original author and source are credit
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This study of the vortical structures developed on the upper surface of a double-delta wing has revealed that these vortex flows are quite complex and that vortex structures interact with one another. Indeed, it would seem that vortex behaviour has something of a universal nature. An angular conformity between primary and secondary vortex torques and the leading edges of the wing can be expressed by the law of filiation [1,2]. Intervortex angles evolve with increasing incidence while fragmentation is a function of the apex angle. It would be interesting to recall that this particular spatial organization of vortex structures, citing the concept of preferential angles, also appears in standard theories on aerodynamics as, for example, in those governing aerodynamic drag. Nevertheless, the link between interior and exterior vortex structures remains to be investigated further. Such studies might even prove the existence of a supplementary torque. In addition, the least resistance of secondary vortices in relation to their fragmentation inevitably calls for experiments to be undertaken with other possible combinations of slender bodies although these areas of research are beyond the scope of this article.

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