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Experimental study of the influence of parameters of a passive porous coating on the development of disturbances in a hypersonic boundary layer

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Abstract

The influence of the thickness and porosity of a passive porous coating on the development of natural disturbances in a hypersonic boundary layer has been studied for the sharp cone model at a Mach number of M ∞ = 6, zero angle of attack, and Reynolds numbers Re1∞. It is established that there exists an optimum thickness of the passive porous coating that corresponds to the maximum stabilization of second-mode disturbances.

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Authors and Affiliations

  1. Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch, Russian Academy of Sciences, Novosibirsk, 630090, Russia

    S. V. Lukashevich, S. O. Morozov & A. N. Shiplyuk

Authors
  1. S. V. Lukashevich
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  2. S. O. Morozov
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  3. A. N. Shiplyuk
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Correspondence to S. O. Morozov.

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Original Russian Text © S.V. Lukashevich, S.O Morozov, A.N. Shiplyuk, 2012, published in Pis’ma v Zhurnal Tekhnicheskoi Fiziki, 2012, Vol. 38, No. 23, pp. 83–88.

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Lukashevich, S.V., Morozov, S.O. & Shiplyuk, A.N. Experimental study of the influence of parameters of a passive porous coating on the development of disturbances in a hypersonic boundary layer. Tech. Phys. Lett. 38, 1077–1079 (2012). https://doi.org/10.1134/S1063785012120073

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  • DOI: https://doi.org/10.1134/S1063785012120073

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