Experimental aeroelastic behavior of unswept and forward-swept cantilever graphite/epoxy wings
- 1 August 1985
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 22 (8) , 679-686
- https://doi.org/10.2514/3.45186
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- Active suppression of aeroelastic instabilities on a forward-swept wingJournal of Aircraft, 1984
- Aeroelastic flutter and divergence of stiffness coupled, graphite/epoxy cantilevered platesJournal of Aircraft, 1984
- Rigid-body structural mode coupling on a forward swept wing aircraftJournal of Aircraft, 1983
- Vibration and flutter of advanced composite lifting surfacesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Swept composite wing aeroelastic divergence experimentsJournal of Aircraft, 1982
- Vibration of Cantilevered Graphite/Epoxy Plates With Bending-Torsion CouplingJournal of Reinforced Plastics and Composites, 1982
- Wind Tunnel Demonstration of Aeroelastic Tailoring Applied to Forward Swept WingsJournal of Aircraft, 1981
- The Two-Dimensional Incompressible Aerodynamic Coefficients for Oscillatory Changes in Airfoil CamberJournal of the Aeronautical Sciences, 1953