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