Aeroelastic divergence of swept-forward composite wings including warping restraint effect
- 1 November 1988
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 26 (11) , 1373-1377
- https://doi.org/10.2514/3.10050
Abstract
No abstract availableThis publication has 14 references indexed in Scilit:
- Aeroelastic tailoring - Theory, practice, and promiseJournal of Aircraft, 1986
- Flutter and divergence aeroelastic characteristics for composite forward swept cantilevered wingJournal of Aircraft, 1985
- Experimental aeroelastic behavior of unswept and forward-swept cantilever graphite/epoxy wingsJournal of Aircraft, 1985
- Generic Approach to Determine Optimum Aeroelastic Characteristics for Composite Forward-Swept-Wing AircraftAIAA Journal, 1984
- A Hybrid State Vector Approach to Aeroelastic AnalysisAIAA Journal, 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
- of Forward Swept Composite Wings DivergenceJournal of Aircraft, 1980
- Aeroelastic Stability and Performance Characteristics of Aircraft with Advanced Composite Sweptforward Wing StructuresPublished by Defense Technical Information Center (DTIC) ,1978
- Elastostatics and Kinetics of Anisotropic and Heterogeneous Shell-Type StructuresJournal of Applied Mechanics, 1976