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Investigation of the effect of heavy gas injection into a supersonic boundary layer on laminar-turbulent transition - MaRDI portal

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Investigation of the effect of heavy gas injection into a supersonic boundary layer on laminar-turbulent transition (Q1742456)

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scientific article; zbMATH DE number 6858590
Language Label Description Also known as
English
Investigation of the effect of heavy gas injection into a supersonic boundary layer on laminar-turbulent transition
scientific article; zbMATH DE number 6858590

    Statements

    title
    Investigation of the effect of heavy gas injection into a supersonic boundary layer on laminar-turbulent transition (English)
    0 references
    author
    S. A. Gaponov
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    Yu. G. Ermolaev
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    N. N. Zubkov
    0 references
    A. D. Kosinov
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    V. I. Lysenko
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    A. A. Yatskikh
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    Boris V. Smorodsky
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    publication date
    11 April 2018
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    zbMATH Keywords
    compressible boundary layer
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    hydrodynamic stability
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    laminar-turbulent transition
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    permeable surface
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    injection
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    Identifiers

    Mathematics Subject Classification ID
    76N20
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    76F06
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    76J20
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    76M20
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    76-05
    0 references
    zbMATH DE Number
    6858590
    0 references
    OpenAlex ID
    W2784546273
    0 references
     
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