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 low and enhanced levels of free-stream turbulence.
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Original Russian Text © A.V. Ivanov, D.A. Mischenko, A.V. Boiko.
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Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, Vol. 61, No. 2, pp. 109–116, March–April, 2020.
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Ivanov, A.V., Mischenko, D.A. & Boiko, A.V. Method of the Description of the Laminar-Turbulent Transition Position on a Swept Wing in the Flow with an Enhanced Level of Free-Stream Turbulence. J Appl Mech Tech Phy 61, 250–255 (2020). https://doi.org/10.1134/S0021894420020108
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DOI: https://doi.org/10.1134/S0021894420020108