Analysis of a Multi-Flap Rotor System for Swashplateless Rotor Control
Influence of Controlled Blade Lead-Lag Motions on Helicopter Vibration
The Effect of Non-Harmonic Active Twist Actuation on BVI Noise
Initial Whirl-Flutter Characterization of the TiltRotor Aeroelastic Stability Testbed
Helicopter Horizontal Tail Incidence Control to Reduce Rotor Cyclic Pitch and Blade Flapping
Coupled CFD/CSD Analysis of Rotor Blade Structural Loads with Experimental Validation