General formulation for the aeroelastic divergence of composite swept-forward wing structures
- 1 April 1988
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 25 (4) , 364-371
- https://doi.org/10.2514/3.45572
Abstract
No abstract availableKeywords
This publication has 15 references indexed in Scilit:
- Flutter and divergence aeroelastic characteristics for composite forward swept cantilevered wingJournal 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
- Aeroelastic Tailoring of Forward Swept Composite WingsJournal of Aircraft, 1981
- of Forward Swept Composite Wings DivergenceJournal of Aircraft, 1980
- Forward Swept Wing Static AeroelasticityPublished by Defense Technical Information Center (DTIC) ,1979
- Aeroelastic Stability and Performance Characteristics of Aircraft with Advanced Composite Sweptforward Wing StructuresPublished by Defense Technical Information Center (DTIC) ,1978
- A Formulation of the Aeroelastic Problem for a Swept WingJournal of the Aeronautical Sciences, 1949