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An efficient finite differences method for the computation of compressible, subsonic, unsteady flows past airfoils and panels - MaRDI portal

An efficient finite differences method for the computation of compressible, subsonic, unsteady flows past airfoils and panels (Q1692049)

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scientific article; zbMATH DE number 6829824
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English
An efficient finite differences method for the computation of compressible, subsonic, unsteady flows past airfoils and panels
scientific article; zbMATH DE number 6829824

    Statements

    An efficient finite differences method for the computation of compressible, subsonic, unsteady flows past airfoils and panels (English)
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    26 January 2018
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    airfoil-fluid interaction
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    compressible subsonic flow
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    convected wave equation
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    flutter
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    linearized potential flow
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    unsteady aerodynamics
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