Frequency Determination Techniques for Cantilevered Plates with Bending-Torsion Coupling.
- 1 March 1984
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 22 (3) , 415-420
- https://doi.org/10.2514/3.48463
Abstract
No abstract availableThis publication has 6 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
- Wind Tunnel Demonstration of Aeroelastic Tailoring Applied to Forward Swept WingsJournal of Aircraft, 1981
- Frequency determination and non-dimensionalization for composite cantilever platesJournal of Sound and Vibration, 1980
- The Natural Modes of Graphite/Epoxy Cantilever Plates and ShellsJournal of Composite Materials, 1979
- Improvement of Plate and Shell Finite Elements by Mixed FormulationsAIAA Journal, 1978