Flutter analysis of an articulated high aspect ratio wing in subsonic airflow

DOI10.1016/j.jfranklin.2014.04.010zbMath1294.93058OpenAlexW2019365157MaRDI QIDQ402030

Iylene Patino, Amjad M. Tuffaha, A. V. Balakrishnan, O. V. Mel'nikov

Publication date: 27 August 2014

Published in: Journal of the Franklin Institute (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.jfranklin.2014.04.010

zbMATH Keywords

flutter speedshighly flexible wing configurationinviscid air flowunmanned aerial vehicle (UAV) type aircraft

Mathematics Subject Classification ID

Application models in control theory (93C95) Automated systems (robots, etc.) in control theory (93C85)

Related Items (2)

Static stability analysis of a thin plate with a fixed trailing edge in axial subsonic flow: Possio integral equation approach ⋮ Aeroelastic stability analysis of a pyrotechnic separation plate in subsonic airflow

Cites Work

• Aeroelasticity
• Dynamics and Control of Distributed Systems
• Unnamed Item

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