Open AccessExperimental study of vortex wake behind of a wing at Mach number range of M=2–4
Author(s) -
A. M. Shevchenko,
A. S. Shmakov
Publication year - 2018
Publication title -
aip conference proceedings
Language(s) - English
Resource type - Conference proceedings
eISSN - 1551-7616
pISSN - 0094-243X
DOI - 10.1063/1.5065197
Subject(s) - anemometer , wake , mach number , vortex , mechanics , wind tunnel , supersonic speed , wing , physics , angle of attack , range (aeronautics) , wake turbulence , choked flow , supersonic wind tunnel , aerospace engineering , aerodynamics , engineering , turbulence , 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