Open AccessExperimental investigation of natural disturbances of a supersonic boundary layer on a swept-wing model with periodic roughness at Mach 2.5
Author(s) -
A. A. Yatskikh,
А. В. Панина,
Yu. G. Ermolaev,
V. L. Kocharin,
Н. В. Семёнов,
А. Д. Косинов
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 - 10.1063/5.0051999
Subject(s) - anemometer , mach number , boundary layer , supersonic speed , swept wing , leading edge , mechanics , aerodynamics , boundary (topology) , choked flow , surface roughness , surface finish , boundary layer thickness , wing , optics , acoustics , materials science , physics , structural engineering , engineering , mathematics , mathematical analysis , turbulence , composite material
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