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Experimental study of the evolution of periodic controlled disturbances in a hypersonic viscous shock layer on a flat plate

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Thermophysics and Aeromechanics Aims and scope

Abstract

Characteristics of the fields of mean density and density fluctuations measured with introduction of periodic disturbances into a hypersonic viscous boundary layer on a flat plate are presented. The experiments are performed for a flow Mach number M∞ = 21, Reynolds number per meter Re1∞ = 6·105 m−1, and temperature factor of the surface T w /T 0 = 0.26. The disturbances are introduced into the shock layer by an oblique gasdynamic whistle.

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Authors and Affiliations

  1. Khristianovich Institute of Theoretical and Applied Mechanics SB RAS, Novosibirsk, Russia

    S. G. Mironov & I. S. Tsyryul’nikov

Authors
  1. S. G. Mironov
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  2. I. S. Tsyryul’nikov
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The work was financially supported by the Russian Foundation for Basic Research (Grants Nos. 04-01-00474 and 05-08-33436).

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Mironov, S.G., Tsyryul’nikov, I.S. Experimental study of the evolution of periodic controlled disturbances in a hypersonic viscous shock layer on a flat plate. Thermophys. Aeromech. 13, 327–333 (2006). https://doi.org/10.1134/S0869864306030024

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  • DOI: https://doi.org/10.1134/S0869864306030024

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