THE NUMERICAL SIMULATION OF THE BUFFETING'S APPEARANCE FOR ONERA M6 WING
Abstract
Introduction to the results of a numerical study buffeting on Onera M6 wing. The determination of condition to appear buffeting of the modes of oscillation of a shock when interacting with in the boundary layer at Mach numbers and angles of attack.
References
1. Woodgate M.A. and Barakos G.N. (2012) Implicit computational fluid dynamics methods for fast analysis of rotor flows. AIAA Journal vol 50 issue 6 pp 1217-1244.
2. Smagorinsky J. 1971: Numerical simulation of climate modification. In, Proceedings of the 12th Interagency Conference on Climate Modification, Virginia Beach, VA, 221-2263 [Электронный ресурс]. URL: http://www.aero.polimi.it/freecase/ ONERA-M6-wing.
Review
For citations:
Lipatov I.I., Vinh P.T. THE NUMERICAL SIMULATION OF THE BUFFETING'S APPEARANCE FOR ONERA M6 WING. Civil Aviation High Technologies. 2014;(200):133-140. (In Russ.)
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