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Comprehensive mesh study for a direct numerical simulation of the transonic flow at \(\mathrm{Re}_{c} = 500,000\) around a NACA 0012 airfoil - MaRDI portal

Comprehensive mesh study for a direct numerical simulation of the transonic flow at \(\mathrm{Re}_{c} = 500,000\) around a NACA 0012 airfoil (Q1646023)

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scientific article; zbMATH DE number 6893570
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English
Comprehensive mesh study for a direct numerical simulation of the transonic flow at \(\mathrm{Re}_{c} = 500,000\) around a NACA 0012 airfoil
scientific article; zbMATH DE number 6893570

    Statements

    Comprehensive mesh study for a direct numerical simulation of the transonic flow at \(\mathrm{Re}_{c} = 500,000\) around a NACA 0012 airfoil (English)
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    22 June 2018
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    WENO
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    direct numerical simulation (DNS)
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    mesh study
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    aeroacoustics
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    compressible
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    transonic flow
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