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Afanasyev L.V., Yermolaev Yu.G., Kosinov A.D., Semionov N.V., Shmakova A.V., Yatskikh A.A. Experimental Study of the Influence of Weak Shock Waves on the Laminar-Turbulent Transition in the Swept Wing Boundary Layer at Mach Number 2.5. SIBERIAN JOURNAL OF PHYSICS. 2024;19(4):41-54. (In Russ.) https://doi.org/10.25205/2541-9447-2024-19-4-41-54



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ISSN 2541-9447 (Print)