Active suppression of aeroelastic instabilities on a forward-swept wing
- 1 March 1984
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 21 (3) , 202-208
- https://doi.org/10.2514/3.48246
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
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- Rigid body-structural mode coupling on a forward swept wing aircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Active control of forward swept wings with divergence and flutter aeroelastic instabilitiesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- 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 tailoring of a forward swept wing and comparisons with three equivalent aft swept wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- On the use of Pade approximants to represent unsteady aerodynamic loads for arbitrarily small motions of wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976