Frequency domain system identification of helicopter blades with trailing edge flaps
Adaptive Structures Forum ; 1996 ; Salt Lake City , UT , U.S.A.
1996-01-01
Conference paper
Electronic Resource
English
Stabilization of Helicopter Blades with Severed Pitch Links Using Trailing-Edge Flaps
Online Contents | 2003
|Swashplateless Helicopter Rotor with Trailing-Edge Flaps
AIAA | 2004
|Helicopter Vibration Reduction with Trailing Edge Flaps
British Library Conference Proceedings | 1995
|Helicopter Vibration Reduction with Trailing Edge Flaps
British Library Conference Proceedings | 1995
|