Accurate closed-form eigensolutions of three-dimensional panel flutter with arbitrary homogeneous boundary conditions
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Mechanical Engineering,Aerospace Engineering
Reference48 articles.
1. Review of nonlinear panel flutter at supersonic and hypersonic speeds;Mei;Appl Mech Rev,1999
2. A parametric study on supersonic/hypersonic flutter behavior of aero-thermo-elastic geometrically imperfect curved skin panel;Abbas;Acta Mech,2011
3. Supersonic/hypersonic flutter and postflutter of geometrically imperfect circular cylindrical panels;Librescu;J Spacecr Rockets,2002
4. Hypersonic aeroelastic response of elastic boundary panel based on a modified Fourier series method;Zhou;Int J Aerosp Eng,2019
5. A modern course in aeroelasticity;Dowell,2015
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3. Aerodynamic and structural characteristics of helicopter rotor in circling flight;Chinese Journal of Aeronautics;2023-12
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