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A fully-coupled CFD/CSD computational approach for aeroelastic studies of helicopter blade-vortex interaction - MaRDI portal

A fully-coupled CFD/CSD computational approach for aeroelastic studies of helicopter blade-vortex interaction (Q2008495)

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scientific article; zbMATH DE number 7136516
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English
A fully-coupled CFD/CSD computational approach for aeroelastic studies of helicopter blade-vortex interaction
scientific article; zbMATH DE number 7136516

    Statements

    A fully-coupled CFD/CSD computational approach for aeroelastic studies of helicopter blade-vortex interaction (English)
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    26 November 2019
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    helicopter aerodynamics
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    blade-vortex interaction
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    fully-coupled aerolastic model
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    two-spring model
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    large-eddy simulation
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    Identifiers