Design, development, and testing of an active flutter margin augmentation system for a commercial transport airplane
20th Structures, Structural Dynamics, and Materials Conference ; 1979 ; St. Louis , MO , U.S.A.
1979-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Flutter Margin Augmentation Synthesis Using Normalized Coprime Factors Approach
Online Contents | 1995
|Airplane Vibrations and Flutter Controllable by Design
SAE Technical Papers | 1933
|