A wind tunnel demonstration of the principle of aeroelastic tailoring applied to forward swept wings
- 12 May 1980
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- A wind tunnel demonstration of the principle of aeroelastic tailoring applied to forward swept wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Forward Swept Wing Static AeroelasticityPublished by Defense Technical Information Center (DTIC) ,1979
- An aeroelastic optimization procedure for composite high aspect ratio wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Aeroelastic tailoring studies in fighter aircraft designPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Aeroelastic Stability and Performance Characteristics of Aircraft with Advanced Composite Sweptforward Wing StructuresPublished by Defense Technical Information Center (DTIC) ,1978
- An efficient structural resizing procedure for meeting static aeroelastic design objectivesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- AEROELASTIC TAILORING OF ADVANCED COMPOSITE LIFTING SURFACES IN PRELIMINARY DESIGNPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Divergence elimination with advanced compositesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Subsonic unsteady aerodynamics for general configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972