A CFD-Based Reduced Order Aerodynamic Model for On-Blade Active Control in Rotorcraft
A Computational Study of Microflaps with Application to Vibration Reduction in Helicopter Rotors
A Surrogate Based Approach to Reduced-Order Dynamic Stall Modeling
Numerical Evaluation of Microflaps for On Blade Control of Noise and Vibration
AIAA-2004-1948 The HHC Algorithm for Helicopter Vibration Reduction Revisited
Unsteady Aerodynamics of Flapped Airfoils and Rotors Using CFD and Approximate Methods
Efficient Global Optimization of Helicopter Rotor Blades for Vibration Reduction in Forward Flight
Helicopter Noise Reduction By Actively Controlled Flaps AIAA Paper 2005-2904
Rotorcraft Vibration and Noise Prediction Using a Unified Aeroelastic Analysis
Comparison of Experiments on Bio-inspired Hover Kinematics with the Unsteady Vortex Model and CFD