Advanced Rotorcraft Aeromechanic Studies in the French-German SHANEL Project
Simulation of Complete Helicopter Noise in Maneuver Flight Using Aeroacoustic Flight Test Data
Effect of Wake Structure on Blade-Vortex Interaction Phenomena: Acoustic Prediction and Validation
Effect of Wake Structure on Blade-Vortex Interaction Phenomena: Acoustic Prediction and Validation
Aerodynamics and Acoustics of Rotor Blade-Vortex Interactions