Experimental study of influence of heavy gas injection into boundary layer on perforated model surface at Mach number 2 on its stability to controlled disturbances
Author(s) -
В. И. Лысенко,
B. V. Smorodsky,
Yu. G. Ermolaev,
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 - 10.1063/5.0051747
Subject(s) - mach number , boundary layer , supersonic speed , mechanics , reynolds number , perturbation (astronomy) , sulfur hexafluoride , choked flow , physics , boundary layer thickness , materials science , quantum mechanics , turbulence
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