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Pisma v Zhurnal Tekhnicheskoi Fiziki, 2015, Volume 41, Issue 19, Pages 29–37
(Mi pjtf7848)
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This article is cited in 21 scientific papers (total in 21 papers)
The influence of the laminar–turbulent transition on the interaction between the shock wave and boundary layer at a low supersonic Mach number
P. A. Polivanov, A. A. Sidorenko, A. A. Maslov Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch of the Russian Academy of Sciences, Novosibirsk
Abstract:
An experimental study is devoted to the problem of the interaction between the shock wave and boundary layer. The influence of the approaching boundary layer state on parameters of the interaction region is studied by use of measurements of velocity fields. It is shown that the case in which the interaction occurs near the zone of the laminar–turbulent transition in the boundary layer is optimum. The possibility of controlling for the interaction by means of turbulizers is studied.
Received: 10.12.2014
Citation:
P. A. Polivanov, A. A. Sidorenko, A. A. Maslov, “The influence of the laminar–turbulent transition on the interaction between the shock wave and boundary layer at a low supersonic Mach number”, Pisma v Zhurnal Tekhnicheskoi Fiziki, 41:19 (2015), 29–37; Tech. Phys. Lett., 41:10 (2015), 933–937
Linking options:
https://www.mathnet.ru/eng/pjtf7848 https://www.mathnet.ru/eng/pjtf/v41/i19/p29
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