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
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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
Publisher Name: Springer, Dordrecht
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