Open AccessExperimental study of the laminar-turbulent transition in the boundary layer of the wing with a sweep angle of the leading edge of 72 degrees at Mach 4
Author(s) -
V. L. Kocharin,
A. A. Yatskikh,
Н. В. Семёнов,
S. N. Tagaev,
А. Д. Косинов,
Yu. G. Yermolaev
Publication year - 2021
Publication title -
aip conference proceedings
Language(s) - English
Resource type - Conference proceedings
SCImago Journal Rank - 0.177
H-Index - 75
eISSN - 1551-7616
pISSN - 0094-243X
DOI - 10.1063/5.0051932
Subject(s) - laminar flow , mach number , boundary layer , anemometer , swept wing , turbulence , leading edge , laminar turbulent transition , wind tunnel , supersonic speed , physics , mechanics , mach wave , optics , aerodynamics
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