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Pisma v Zhurnal Tekhnicheskoi Fiziki, 2011 Volume 37, Issue 22, Pages 61–68 (Mi pjtf9335)

This article is cited in 3 papers

Effect of dielectric barrier discharge on wing-tip vortex formation

S. A. Agibalovaab, V. V. Golubab, I. A. Moralevab, A. S. Savel'evab

a Joint Institute for High Temperatures, Russian Academy of Sciences, Moscow
b Moscow Institute of Physics and Technology, Dolgoprudny, Moscow Region

Abstract: The formation of vortex trace behind a finite-span model airfoil has been studied by the method of stereoscopic particle image velocimetry. It is established that a dielectric barrier discharge initiated at the airfoil tip surface influences the wing-tip vortex formation.

Received: 14.06.2011


 English version:
Technical Physics Letters, 2011, 37:11, 1070–1073

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© Steklov Math. Inst. of RAS, 2026