Static aeroelastic analysis of a high-aspect-ratio wing based on wind-tunnel experimental aerodynamic forces

DOI10.1007/s11431-011-4446-5zbMath1239.74024OpenAlexW2264234174MaRDI QIDQ424981

J. Herrera, H. S. Yoon

Publication date: 7 June 2012

Published in: Science China. Technological Sciences (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s11431-011-4446-5

zbMATH Keywords

aeroelasticityaileron efficiencyaileron reversalexperimental aerodynamic forcesflight loadshigh-aspect-ratio wing

Mathematics Subject Classification ID

Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10)

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

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