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Rotor Design Options for Improving V-22 Whirl-Mode Stability
Range and Endurance Tradeoffs on Personal Rotorcraft Design
Range and Endurance Tradeoffs on Personal Rotorcraft Design
Preliminary report on in-flight measurement of rotor hub drag and lift using the RSRA
Personal Rotorcraft Design and Performance with Electric Hybridization
Performance of Advanced Heavy-Lift, High-Speed Rotorcraft Configurations
Integration of Rotor Aerodynamic Optimization with the Conceptual Design of a Large Civil Tiltrotor
Influence of Alternative Engine Concepts on LCTR2 Sizing and Mission Profile
In-flight measurement of rotor hub drag using the RSRA - A feasibility demonstration
High-Speed Wind Tunnel Tests of a Full-Scale Proprotor on the Tiltrotor Test Rig
Exploring Propulsion System Requirements for More and All-Electric Helicopters
Exploring Propulsion System Requirements for More and All-Electric Helicopters
Effects of Rotor Design Variations on Tiltrotor Whirl-Mode Stability
Effects of Rotor Design Variations on Tiltrotor Whirl-Mode Stability
Effects of Blade Sweep on V-22 Whirl Flutter and Loads
Development and Initial Testing of the Tiltrotor Test Rig
Design Study of Propulsion and Drive Systems for the Large Civil TiltRotor (LCTR2) Rotorcraft
Defining Gas Turbine Engine Performance Requirements for the Large Civil TiltRotor (LCTR2)
Analytical Performance, Loads, and Aeroelastic Stability of a Full-Scale Isolated Proprotor