For citations:
Kocharin V.L., Semionov N.L., Kosinov A.D., Yatskikh A.A., Shipul S.A., Yermolaev Yu.G. Experimental Study of the Influence of Unit Reynolds Number on the Laminar-Turbulent Transition on the Model Swept Wing with a Subsonic Leading Edge at M = 2. SIBERIAN JOURNAL OF PHYSICS. 2021;16(1):44-52. (In Russ.) https://doi.org/10.25205/2541-9447-2021-16-1-44-52
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