Aeroelastic stability analysis of aircraft wings with high aspect ratios by transfer function method

DOI10.1142/S021945541850150XWikidataQ129768864 ScholiaQ129768864MaRDI QIDQ6493140

Jingbo Duan, Zhong-Yuan Zhang

Publication date: 26 April 2024

Published in: International Journal of Structural Stability and Dynamics (Search for Journal in Brave)

zbMATH Keywords

flutteraeroelastic stabilityhigh aspect ratiotransfer function methodaircraft wingtorsional divergence

Mathematics Subject Classification ID

Stability of dynamical problems in solid mechanics (74H55)

Cites Work

• Nonlinear Thermal Flutter Analysis of Supersonic Composite Laminated Panels Using Differential Quadrature Method
• Transfer functions of constrained/combined one-dimensional continuous dynamic systems
• Distributed transfer function method for analysis of cylindrical shells
• A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows.

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