Open AccessAn experimental study of the vortex wake at Mach number of 3
Author(s) -
A. S. Shmakov,
A. M. Shevchenko
Publication year - 2017
Publication title -
aip conference proceedings
Language(s) - English
Resource type - Conference proceedings
eISSN - 1551-7616
pISSN - 0094-243X
DOI - 10.1063/1.5007547
Subject(s) - mach number , wake , anemometer , vortex , mechanics , supersonic speed , physics , flow visualization , trailing edge , chord (peer to peer) , wake turbulence , leading edge , mach wave , wind tunnel , drag divergence mach number , aerodynamics , flow (mathematics) , transonic , turbulence , computer science , distributed computing
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