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Rotor Design Options for Improving V-22 Whirl-Mode Stability
Preliminary report on in-flight measurement of rotor hub drag and lift using the RSRA
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
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
Analytical Performance, Loads, and Aeroelastic Stability of a Full-Scale Isolated Proprotor