Численное исследование взаимодействия сверхзвукового потока вязкого газа с поперечной струёй, вдуваемой под углом через щель в пластине
Published in Computational Continuum Mechanics • Jun 1, 2026
Authors:,
Елена Викторовна Бабич
Колесник Елизавета Владимировна
Abstract
This paper presents the results of a comprehensive numerical study of the interaction between a supersonic air flow with a Mach number of 3.5 and a stationary jet injected through a slot in a streamlined plate. The mathematical model is based on the Reynolds-averaged Navier–Stokes equations, which a...
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