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title: Vertical lift aircraft design conference
X-Wing: A Low Disc-Loading V/STOL for the Navy
V/STOL Conference, Palo Alto, Calif., June 6-8, 1977, Technical Papers
Volantor* - A Powered Lift Aircraft for Personal Use
Vertical Lift - Not Just For Terrestrial Flight
Type 'A' V/STOL - One aircraft for all support missions
Trust Control of VTOL Aircraft Part Deux
Trajectory computation Infrastructure based on BADA Aircraft Performance Model
The selection of convertible engines with current gas generator technology for high speed rotorcraft
The selection of convertible engines with current gas generator technology for high speed rotorcraft
Theoretical and Experimental Studies on Unsteady Rotor-Fuselage Interactional Aerodynamics
The MDA/BAe/GEAE/RR ASTOVL/CTOL Technology Demonstrator Team
The Impact of Integrated Product Development on the Helicopter Design Process
The Direct Lift ASTOVL Aircraft
The Design, Development and Testing of a Turbine Powered Simulator for Hot Gas Ingestion Testing
The Autonomous Scout Rotorcraft Testbed (ASRT), A US Army IPPD Pilot Project
Technology Needs for Future US Navy/Marine Corps Heavy Lift VTOL Aircraft
Takeoff Predictions for Powered-Lift Aircraft
Supplement to Conference Proceedings No. 22 Pre-Print