Effect of Piezoelectric Hysterisis Nonlinearity on Helicopter Vibration Control Using Trailing Edge Flaps
46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
01.01.2005
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Effect of Piezoelectric Hysteresis on Helicopter Vibration Control Using Trailing-Edge Flaps
Online Contents | 2006
|Helicopter vibration reduction with trailing edge flaps
Tema Archiv | 1995
|Helicopter vibration reduction with trailing edge flaps
AIAA | 1995
|Helicopter Vibration Reduction with Trailing Edge Flaps
British Library Conference Proceedings | 1995
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