Open AccessOn the oblique breakdown mechanism in a supersonic boundary layer on a swept wing at Mach 2
Author(s) -
А. В. Панина,
А. Д. Косинов,
Н. В. Семёнов,
Yu. G. Yermolaev
Publication year - 2017
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 - 10.1063/1.5007538
Subject(s) - mach number , boundary layer , swept wing , boundary layer thickness , mechanics , wing , reynolds number , supersonic speed , flow separation , airfoil , oblique case , optics , physics , aerodynamics , angle of attack , stall (fluid mechanics) , turbulence , linguistics , philosophy , thermodynamics
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