Abstract
Classical investigations on the aeroelasticity of wings used for the analysis of flutter stability are often carried out based on simplifying model configurations given by elastically mounted rigid wings.
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The project is financially supported by the German Research Foundation (Deutsche Forschungsgemeinschaft) under the contract number BR 1847/17-1.
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Boulbrachene, K., Breuer, M. (2024). Wind Gust-Induced Flutter of an Elastically Mounted Airfoil: A Fluid-Structure Interaction Study Based on LES. In: Marchioli, C., Salvetti, M.V., Garcia-Villalba, M., Schlatter, P. (eds) Direct and Large Eddy Simulation XIII. DLES 2023. ERCOFTAC Series, vol 31. Springer, Cham. https://doi.org/10.1007/978-3-031-47028-8_13
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