Performance Improvement with Variable Rotor Span and RPM
On Power and Actuation Requirement in Swashplateless Primary Control using Trailing-Edge Flaps
Optimally Actuated Spanwise-Segmented Aerodynamic Effectors for Rotorcraft Power Reduction
Rotor Vibration Reduction using an Embedded Spanwise Absorber
Energy Absorption of Sandwiched Honeycombs with Facesheets in In-plane Crushing
Rotorcraft Operating Envelope Expansion Using Extendable Chord Sections
Dynamic Blade Shape for Improved Helicopter Rotor Performance
Optimally Scheduled Deployments of Miniature Trailing Edge Effectors for Rotorcraft Power Reduction