Aeroelastic flutter and divergence of stiffness coupled, graphite/epoxy cantilevered plates
- 1 January 1984
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 21 (1) , 69-76
- https://doi.org/10.2514/3.48224
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Vibration of Cantilevered Graphite/Epoxy Plates With Bending-Torsion CouplingJournal of Reinforced Plastics and Composites, 1982
- Aeroelastic flutter and divergence of stiffness coupled, graphite/epoxy, cantilevered platesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Flutter of forward swept wings, analyses and testsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
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- Aeroelastic Tailoring of Forward Swept Composite WingsJournal of Aircraft, 1981
- Frequency determination and non-dimensionalization for composite cantilever platesJournal of Sound and Vibration, 1980
- The Two-Dimensional Incompressible Aerodynamic Coefficients for Oscillatory Changes in Airfoil CamberJournal of the Aeronautical Sciences, 1953