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On the theory of separation of a laminar boundary layer in a supersonic flow - MaRDI portal

On the theory of separation of a laminar boundary layer in a supersonic flow (Q1057734)

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scientific article; zbMATH DE number 3898470
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On the theory of separation of a laminar boundary layer in a supersonic flow
scientific article; zbMATH DE number 3898470

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    On the theory of separation of a laminar boundary layer in a supersonic flow (English)
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    1984
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    In the present paper, we propose a flow model that permits elimination of the singularity at the point of separation of the laminar boundary layer in a supersonic flow in the case of a given adverse pressure gradient.
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    viscous gas
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    elimination of the singularity
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    laminar boundary layer
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    adverse pressure gradient
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