Swept composite wing aeroelastic divergence experiments
- 1 November 1982
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 19 (11) , 1019-1024
- https://doi.org/10.2514/3.44806
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- of Forward Swept Composite Wings DivergenceJournal of Aircraft, 1980
- A wind tunnel demonstration of the principle of aeroelastic tailoring applied to forward swept wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Aeroelastic Stability and Performance Characteristics of Aircraft with Advanced Composite Sweptforward Wing StructuresPublished by Defense Technical Information Center (DTIC) ,1978
- Divergence elimination with advanced compositesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- The Influence of Structural Deformation on Airplane CharacteristicsJournal of the Aeronautical Sciences, 1945
- On the analysis of experimental observations in problems of elastic stabilityProceedings of the Royal Society of London. Series A, Containing Papers of a Mathematical and Physical Character, 1932