Energy addition to a gas in a turbulent supersonic boundary layer (Q2746945)

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scientific article; zbMATH DE number 1656880
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Energy addition to a gas in a turbulent supersonic boundary layer
scientific article; zbMATH DE number 1656880

    Statements

    11 October 2001
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    friction reduction
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    heat transfer
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    turbulent supersonic boundary-layer flow
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    finite difference method
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    friction force
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    isothermal surface
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    thermal source
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    Energy addition to a gas in a turbulent supersonic boundary layer (English)
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    The effect of thermal action on a turbulent supersonic boundary-layer flow is studied numerically. It is shown that the friction force on an isothermal surface decreases significantly, and the effectiveness of using a thermal source for reducing friction is evaluated.
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