Characteristics of the at-303 hypersonic wind tunnel. Part 1. Velocity fields
A.M. Kharitonov, V.I. Zvegintsev, L.G. Vasenev, A.D. Kuraeva, D.G. Nalivaichenko, A.V. Novikov, M.A. Paikova, V.F. Chirkashenko, N.V. Shakhmatova, and S.I. Shpak
Khristianovich Institute of Theoretical and Applied Mechanics SB RAS, Novosibirsk, Russia
Pages: 1-16
Abstract
The structure and principle of operation of a new wind tunnel AT-303 with adiabatic compression are described. Results of systematic investigations are presented in terms of velocity distributions both at the nozzle exit and in the region where the models are located. The velocity fields are obtained with the use of total pressure probes in the ranges of Mach numbers from 7.6 to 19.7 and Reynolds numbers per meter Re1 = (0.25–3.64).107.
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