Flutter and divergence aeroelastic characteristics for composite forward swept cantilevered wing
- 1 November 1985
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 22 (11) , 1001-1007
- https://doi.org/10.2514/3.45238
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Control of aeroelastic instabilities through elastic cross-couplingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Generic Approach to Determine Optimum Aeroelastic Characteristics for Composite Forward-Swept-Wing AircraftAIAA Journal, 1984
- Aeroelastic flutter and divergence of stiffness coupled, graphite/epoxy cantilevered platesJournal of Aircraft, 1984
- Wind Tunnel Demonstration of Aeroelastic Tailoring Applied to Forward Swept WingsJournal of Aircraft, 1981
- Aeroelastic Tailoring of Forward Swept Composite WingsJournal of Aircraft, 1981
- Aeroelastic Stability and Performance Characteristics of Aircraft with Advanced Composite Sweptforward Wing StructuresPublished by Defense Technical Information Center (DTIC) ,1978
- A Study of the Bending-Torsion Aeroelastic Modes for Aircraft WingsJournal of the Aeronautical Sciences, 1949
- The Flutter of a Uniform Wing With Tip WeightsJournal of Applied Mechanics, 1948
- The Flutter of a Uniform Cantilever WingJournal of Applied Mechanics, 1945