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Characteristics of the AT-303 hypersonic wind tunnel. Part 1. Velocity Fields

Authors
  • Kharitonov, A. M.1
  • Zvegintsev, V. I.1
  • Vasenev, L. G.1
  • Kuraeva, A. D.1
  • Nalivaichenko, D. G.1
  • Novikov, A. V.1
  • Paikova, M. A.1
  • Chirkashenko, V. F.1
  • Shakhmatova, N. V.1
  • Shpak, S. I.1
  • 1 Khristianovich Institute of Theoretical and Applied Mechanics SB RAS, Novosibirsk, Russia , Novosibirsk (Russia)
Type
Published Article
Journal
Thermophysics and Aeromechanics
Publisher
Nauka/Interperiodica
Publication Date
Jan 01, 2006
Volume
13
Issue
1
Pages
1–16
Identifiers
DOI: 10.1134/S1531869906010011
Source
Springer Nature
Keywords
License
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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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