Optimal Placement of Piezoelectric Actuated Trailing-Edge Flaps for Helicopter Vibration Control
49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 16th AIAA/ASME/AHS Adaptive Structures Conference,10th AIAA Non-Deterministic Approaches Conference, 9th AIAA Gossamer Spacecraft Forum, 4th AIAA Multidisciplinary Design Optimization Specialists Conference ; 2008 ; Schaumburg , IL
2008-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Optimal Placement of Piezoelectric Actuated Trailing-Edge Flaps for Helicopter Vibration Control
British Library Conference Proceedings | 2008
|Optimal Placement of Piezoelectric Actuated Trailing-Edge Flaps for Helicopter Vibration Control
Online Contents | 2009
|Helicopter vibration reduction with trailing edge flaps
Tema Archiv | 1995
|Helicopter Vibration Reduction with Trailing Edge Flaps
British Library Conference Proceedings | 1995
|Helicopter Vibration Reduction with Trailing Edge Flaps
British Library Conference Proceedings | 1995
|