Evaluation of innovative concepts for semi-active and active rotorcraft control
Lead-lag dampers are present in most rotor systems to provide the desired level of damping for all flight conditions. These dampers are critical components of the rotor system, and the performance of semi-active Coulomb-friction-based lead-lag dampers is examined for the UH-60 aircraft. The concept...
Main Author: | Van Weddingen, Yannick |
---|---|
Published: |
Georgia Institute of Technology
2012
|
Subjects: | |
Online Access: | http://hdl.handle.net/1853/42893 |
Similar Items
-
Higher harmonic blade pitch control : a system for helicopter vibration reduction
by: Shaw, John
Published: (2005) -
Response, Loads And Stabillity Of Helicopters With Interconnected Rotor Blades
by: Suresh, J K
Published: (2012) -
Aeromechanical Stability Augmentation Using Semi-Active Friction-Based Lead-Lag Damper
by: Agarwal, Sandeep
Published: (2006) -
Design strategies for rotorcraft blades and HALE aircraft wings applied to damage tolerant wind turbine blade design
by: Richards, Phillip W.
Published: (2015) -
A multi-fidelity framework for physics based rotor blade simulation and optimization
by: Collins, Kyle Brian
Published: (2009)