Research efforts aim at flutter suppression are discussed. The application of active controls technology to reduce the aeroelastic response of aircraft structures is discussed. Feedback control, control law design processes and synthesis, wind tunnel studies, and delta-wing wind tunnel models are discussed.
Experiences with the design and implementation of flutter suppression systems
1984-03-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Aeroservoelastic design for flutter suppression
AIAA | 1997
|DESIGN AND IMPLEMENTATION OF A FLUTTER SUPPRESSION EXPERIMENT (AlAA 2017-4357)
British Library Conference Proceedings | 2017
|AIAA | 1976
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