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Numerical modeling of supersonic flow over wings with varying aspect ratio on a broad range of angles of attack using the law of plane sections - MaRDI portal

Numerical modeling of supersonic flow over wings with varying aspect ratio on a broad range of angles of attack using the law of plane sections (Q1317696)

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scientific article; zbMATH DE number 536725
Language Label Description Also known as
English
Numerical modeling of supersonic flow over wings with varying aspect ratio on a broad range of angles of attack using the law of plane sections
scientific article; zbMATH DE number 536725

    Statements

    Numerical modeling of supersonic flow over wings with varying aspect ratio on a broad range of angles of attack using the law of plane sections (English)
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    12 April 1994
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    Godunov's method
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    Sychev's theory
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