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Pisma v Zhurnal Tekhnicheskoi Fiziki, 2012, Volume 38, Issue 17, Pages 39–44
(Mi pjtf8943)
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This article is cited in 1 scientific paper (total in 1 paper)
Control of the flow over wing airfoils in transonic regimes by means of force action of surface elements on the flow
S. M. Aul'chenkoab, V. P. Zamuraevab a Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch of the Russian Academy of Sciences, Novosibirsk
b Novosibirsk State University
Abstract:
Mathematical modeling of the effect of force oscillations of surface elements of a wing airfoil on the shock-wave structure of the transonic flow over it is implemented. The qualitative and quantitative effect of the oscillation parameters on the airfoil wave drag is investigated.
Received: 26.03.2012
Citation:
S. M. Aul'chenko, V. P. Zamuraev, “Control of the flow over wing airfoils in transonic regimes by means of force action of surface elements on the flow”, Pisma v Zhurnal Tekhnicheskoi Fiziki, 38:17 (2012), 39–44; Tech. Phys. Lett., 38:9 (2012), 797–799
Linking options:
https://www.mathnet.ru/eng/pjtf8943 https://www.mathnet.ru/eng/pjtf/v38/i17/p39
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