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Assessment of numerical uncertainty around shocks and corners on blunt trailing-edge supercritical airfoils - MaRDI portal

Assessment of numerical uncertainty around shocks and corners on blunt trailing-edge supercritical airfoils (Q5948593)

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scientific article; zbMATH DE number 1670017
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Assessment of numerical uncertainty around shocks and corners on blunt trailing-edge supercritical airfoils
scientific article; zbMATH DE number 1670017

    Statements

    Assessment of numerical uncertainty around shocks and corners on blunt trailing-edge supercritical airfoils (English)
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    10 February 2002
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    blunt trailing-edge supercritical airfoils
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    grid refinement
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    grid convergence index
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    compressible Reynolds-averaged Navier Stokes equations
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    shock
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    corners
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    pressure
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    aerodynamic drag
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    lift
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