Aeroservoelastic wind-tunnel investigations using the active flexible wing model - Status and recent accomplishments
- 3 April 1989
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- All optimal Hankel-norm approximations of linear multivariable systems and theirL,∞-error bounds†International Journal of Control, 1984
- Decoupler Pylon: A Simple, Effective Wing/Store Flutter SuppressorJournal of Aircraft, 1980