DESIGN OF A SUBSONIC VACUUM AERODYNAMIC FACILITY
D.A. Vnuchkov, V.I. Zvegintsev, D.G. Nalivaichenko
Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch of the Russian Academy of Sciences (ITAM SB RAS), Novosibirsk, Russia
Keywords: vacuum wind tunnel, subsonic flow, aerodynamic experiment
Abstract
Results of the conceptual development of a vacuum aerodynamic facility based on the vacuum system of the AT-303 wind tunnel at the ITAM SB RAS are presented. The layout, geometry, design features, and advantages of the proposed facility are described. Its operating parameters and performance characteristics are evaluated.
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