Experimental investigation of the weak shock wave influence on the boundary layer of a flat blunt plate at the Mach number 2.5

DOI10.1134/S0015462819020058zbMath1416.76005OpenAlexW2948221884WikidataQ127757736 ScholiaQ127757736MaRDI QIDQ2314589

V. L. Kocharin, N. V. Semenov, A. D. Kosinov, A. A. Yatskikh, Yu. G. Ermolaev

Publication date: 29 July 2019

Published in: Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s0015462819020058

zbMATH Keywords

experimentturbulencesupersonic flowboundary layer\(N\)-wavehot-wire anemometry

Mathematics Subject Classification ID

Experimental work for problems pertaining to fluid mechanics (76-05) Shock waves and blast waves in fluid mechanics (76L05) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Cites Work

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