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Structural Deformation-Based Computational Method for Static Aeroelasticity of High-Aspect-Ratio Wing Model in Pressurized Wind Tunnel - MaRDI portal

Structural Deformation-Based Computational Method for Static Aeroelasticity of High-Aspect-Ratio Wing Model in Pressurized Wind Tunnel (Q5156611)

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scientific article; zbMATH DE number 7408330
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English
Structural Deformation-Based Computational Method for Static Aeroelasticity of High-Aspect-Ratio Wing Model in Pressurized Wind Tunnel
scientific article; zbMATH DE number 7408330

    Statements

    Structural Deformation-Based Computational Method for Static Aeroelasticity of High-Aspect-Ratio Wing Model in Pressurized Wind Tunnel (English)
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    11 October 2021
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    static aeroelastic computation
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    high-aspect-ratio wing
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    pressurized wind tunnel
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    CFD-CSD
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    structural stiffness
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