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keywords:(Vertical lift aircraft)
ARPA X-32 STOVL/CTOL Affordable Lightweight Fighter Program
Development of a Tiltrotor Autopilot System
Rotor Blade Deicing Using Advanced Blade Control
Aeroelastic Tailoring of a Civil Tiltrotor Configuration
Government Facilities Supporting the ASTOVL/CTOL Common Affordable Lightweight Fighter Project
The MDA/BAe/GEAE/RR ASTOVL/CTOL Technology Demonstrator Team
Incorporating Genetic Algorithms and Sizing Codes for Conceptual Design of Rotorcraft
The Autonomous Scout Rotorcraft Testbed (ASRT), A US Army IPPD Pilot Project
Damage Tolerant Thermoplastic Composite Helicopter Tailboom Structures
Development and Testing of a Main Rotor Designed for Reduced Vibratory Hub Loads
The Impact of Integrated Product Development on the Helicopter Design Process
A New Technique for Estimating Ground Footprint Acoustics for Rotorcraft Using Measured Sound Fields
Shaft Driven Lift Fan for Common Affordable Lightweight Fighter
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
S-92 - Design for Minimum Operating Costs
Civil Helicopter Market in Russia - CANCELLED