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JOURNALS // Prikladnaya Mekhanika i Tekhnicheskaya Fizika // Archive

Prikl. Mekh. Tekh. Fiz., 2020 Volume 61, Issue 2, Pages 109–116 (Mi pmtf343)

This article is cited in 9 papers

Method of the qualitative description of the laminar-turbulent transition position on a swept wing in the flow with an elevated degree of free-stream turbulence

A. V. Ivanov, D. A. Mishchenko, A. V. Boiko

Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch of the Russian Academy of Sciences, Novosibirsk, 630090, Russia

Abstract: A new experimental method for panoramic contactless determination of the laminar-turbulent transition position in a three-dimensional boundary layer is described. It is demonstrated that this method allows accurate determination of the transition region boundaries at both reduced and elevated degrees of free-stream turbulence.

Keywords: boundary layer, laminar-turbulent transition, panoramic methods of measurements, swept wing, crossflow vortices, hydrodynamic instability.

UDC: 532.526

Received: 19.08.2019
Revised: 19.08.2019
Accepted: 26.08.2019

DOI: 10.15372/PMTF20200210


 English version:
Journal of Applied Mechanics and Technical Physics, 2020, 61:2, 250–255

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© Steklov Math. Inst. of RAS, 2026