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Pisma v Zhurnal Tekhnicheskoi Fiziki, 2012 Volume 38, Issue 17, Pages 39–44 (Mi pjtf8943)

This article is cited 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


 English version:
Technical Physics Letters, 2012, 38:9, 797–799

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