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title: Vertical lift aircraft design conference
A Qualitative Flight Evaluation of a Sidestick Controller in the XV-15 Tiltrotor Research Aircraft
Trust Control of VTOL Aircraft Part Deux
Integrated Helicopter Design Tools (IHDT): Improving Rotorcraft Affordability and Quality
Analytical model and control solutions for unmanned aerial vehicle maneuvers in a vertical plane
A New Technique for Estimating Ground Footprint Acoustics for Rotorcraft Using Measured Sound Fields
Flight Testing the Eagle Eye Tiltrotor Unmanned Air Vehicle
Civil Helicopter Market in Russia - CANCELLED
Dual-Use Rotorcraft Technology: Market Factors and Technology Development
ARPA X-32 STOVL/CTOL Affordable Lightweight Fighter Program
Control of BVI Noise Using an Active Trailing Edge Flap
Helicopter Rotor Blade Flutter - CANCELLED
Theoretical and Experimental Studies on Unsteady Rotor-Fuselage Interactional Aerodynamics
Development and Utilization of a Knowledge-Based (KB) Environment on a Production Helicopter Program
Damage Tolerant Thermoplastic Composite Helicopter Tailboom Structures
Development and Testing of a Main Rotor Designed for Reduced Vibratory Hub Loads
MODUS A High Speed VTOL System Configuration