Effect of the surface roughness of blunt cone forebody on the position of laminar-turbulent transition


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In the present paper, data on the effect of the surface roughness of blunt cone forebody on the position of laminar-turbulent transition are reported. The study was carried out under freestream Mach 5.95. It was found that the roughness position plays a substantial role in the transition process. Critical Reynolds numbers at which the laminar-turbulent transition occurs on the nose-tip of the model were identified. For the first time, hysteresis in transition position was observed.

Sobre autores

D. Bountin

Khristianovich Institute of Theoretical and Applied Mechanics SB RAS

Autor responsável pela correspondência
Email: bountin@itam.nsc.ru
Rússia, Novosibirsk

Yu. Gromyko

Khristianovich Institute of Theoretical and Applied Mechanics SB RAS

Email: bountin@itam.nsc.ru
Rússia, Novosibirsk

A. Maslov

Khristianovich Institute of Theoretical and Applied Mechanics SB RAS

Email: bountin@itam.nsc.ru
Rússia, Novosibirsk

P. Polivanov

Khristianovich Institute of Theoretical and Applied Mechanics SB RAS

Email: bountin@itam.nsc.ru
Rússia, Novosibirsk

A. Sidorenko

Khristianovich Institute of Theoretical and Applied Mechanics SB RAS

Email: bountin@itam.nsc.ru
Rússia, Novosibirsk

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