Abstract
The long term goal of this study is the modelling of vortex breakdown that occurs in some aerodynamic configuration at high angles of attack, (fighters highly swept delta wings or missiles for example). Experimental and theoretical work done at ONERA [1,2] and elsewhere [3] has not yet provided a full understanding of the phenomenon
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References
J. Délery: “Etat des études sur les écoulements tourbillonnaires effectués par la division d’Aérodynamique Fondamentale. ONERAR.T. n° 21/7252 AN - Mars 1988.
Benay R., Pagan D.: “Etude numérique de l’éclatement de tourbillons soumis à des gradients de pression”. La Recherche Aérospatiale n° 1988–1, p.15–27 (English and French edition).
Newsome R.W., Kandil O.A.: “Vortical flow aerodynamics. Physical aspects and numerical simulation”. AIAA Paper 87–0205, AIAA 25th Aerospace Science Metting. Reno, Nevada. January 12–15, 1987.
Lê T.H.,Mège Ph., Morchoisne Y.: “Numerical simulation of vortex breakdown by solving the Euler equations for an incompressible fluid”. La Recherche Aérospatiale n° 1989–5 (English and French edition).
Dang K., Deschamps V.: “Numerical simulations of transitional channel flow”. 5th International conference on numerical methods in laminar and turbulent flow. Montréal 6–10 Juillet 1987. TP ONERA n° 1987–98.
Mège Ph.: “Simulation numérique de l’éclatement tourbillonnaire”. Rapport de stage de DEA de Mécanique (Paris VI) Juin 1988.
Ryan J., Lê T.H., Morchoisne Y.: “Panels code solvers”. 7th GAMM, Louvain (Belgique), 9–11 Septembre 1987.
Batchelor G.K.: “Axial flow in trailing line vortices”. J.Fluid Mech., Vol 20 p. 645, 1964.
Nakamura Y., Leonard A., Spalart P.R.: “Vortex breakdown simulation”. AIAA Paper 85–1581, Cincinnati, Ohio. Juillet 1985.
Uchida S., Nakamura Y., Ohsawa M.: “Experiments on the axisymetric vortex breakdown in a swirling air flow”. Transaction of the Japan society for aeronautical and space sciences.Vol 27 1985.
Pagan D., Solignac J.L.:“Etude expérimentale de l’éclatement d’un tourbillon engendré par une aile delta”. La Recherche Aérospatiale n°1986–3 (English and French edition).
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© 1991 Springer Science+Business Media Dordrecht
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Mege, P., Le, T.H., Morchoisne, Y. (1991). Numerical simulation of vortex breakdown via 3-D Euler equations. In: Metais, O., Lesieur, M. (eds) Turbulence and Coherent Structures. Fluid Mechanics and Its Applications, vol 2. Springer, Dordrecht. https://doi.org/10.1007/978-94-015-7904-9_19
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DOI: https://doi.org/10.1007/978-94-015-7904-9_19
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