Open AccessAn effect of unit Reynolds number on the laminar-turbulent transition on 3D swept wing with χ = 72° at M = 2
Author(s) -
Н. В. Семёнов,
А. Д. Косинов,
V. L. Kocharin,
S. A. Shipul,
A. A. Yatskikh
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 - 10.1063/5.0051717
Subject(s) - leading edge , supersonic speed , laminar flow , reynolds number , turbulence , swept wing , mechanics , wing , laminar turbulent transition , mach number , physics , anemometer , boundary layer , wind tunnel , angle of attack , geometry , aerodynamics , mathematics , thermodynamics
Accelerating Research
Robert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom
Address
John Eccles HouseRobert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom