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Oleg Vishnyakov, Pavel Polivanov and Andrey Sidorenko
The paper focuses on the investigation of unsteady effects in shock wave/boundary layer interaction. The study was carried out using a flat plate model subjected to a free stream Mach number of 1.43 and a unit Reynolds number (Re1) of 11.5 × 106 1/m. To ...
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Pavel Polivanov, Oleg Vishnyakov and Andrey Sidorenko
The problem of flow control under conditions of a turbulent boundary layer at transonic and supersonic free-stream velocities is considered. Such flows are integral components of the flight process and exert significant effects on the flow around both th...
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Carlos Medina, Vladimir Sidorenko (Autor/a)
Pág. 17 - 26
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Sidorenko, I. Rhodes, M. J.
Pág. 137 - 154
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Sidorenko, I; Martin, I; Honary, B
Pág. 720 - 724
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Breitbach, M; Bossert, M; Zyablov, V; Sidorenko, V
Pág. 2025 - 2031
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Sidorenko, V; Markarian, G; Honary, B
Pág. 2048 - 2052
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