Enhancing flutter stability in nanocomposite thin panels by harnessing CNT/polymer dissipation
Author:
Funder
AFOSR
Publisher
Elsevier BV
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science,Civil and Structural Engineering
Reference31 articles.
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3. Theoretical and experimental panel flutter studies in the mach number range 1.0 to 5.0;Dowell;AIAA J.,1965
4. Piston theory a new aerodynamic tool for the aeroelastician;Ashley;J. Aeronaut. Sci.,1956
5. Nonconservative Problems of the Theory of Elastic Stability;Bolotin,1963
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