Aeroelasticity of joined-wing airplane configurations - Past work and future challenges - a survey
- 11 June 2001
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 36 references indexed in Scilit:
- Aerodynamic investigation of twist and cant angles for joined wing transport aircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1997
- Structural optimization for joined-wing synthesisJournal of Aircraft, 1996
- Preliminary weight estimation of conventional and joined wings usingequivalent beam modelsJournal of Aircraft, 1988
- Studies in Nonlinear AeroelasticityPublished by Springer Nature ,1988
- The design of a joined wing flight demonstrator aircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- The joined wing - An overviewJournal of Aircraft, 1986
- Control of a forward-swept-wing configuration dominated by flight dynamic/aeroelastic interactionsJournal of Guidance, Control, and Dynamics, 1986
- Dynamic stability of flexible forward swept wing aircraftJournal of Aircraft, 1983
- Aeroelastic considerations for continuous patrol/high altitude surveillance platformsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Structural Weight Comparison of a Joined Wing and a Conventional WingJournal of Aircraft, 1982