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title: Vertical lift aircraft design conference
The Direct Lift ASTOVL Aircraft
AIAA-2019-3478: Lift Fan Assessment for Conceptual Design of Aircraft Forebody
Aircraft Conceptual Design Trim Matrix Selection
Design of the Atlas Maritime Heavy Lift Helicopter
Design Opportunities and Challenges in the Development of Vertical Lift Planetary Aerial Vehicles
Technology Needs for Future US Navy/Marine Corps Heavy Lift VTOL Aircraft
Shaft Driven Lift Fan for Common Affordable Lightweight Fighter
Vertical Lift - Not Just For Terrestrial Flight
Sikorsky Design Concepts for NASA Heavy Lift Rotorcraft Systems Investigation
Design and Performance of Lift-Offset Rotorcraft for Short-Haul Missions
Full Scale Flight Acoustics Results for the UH-60A Airloads Aircraft
Integrated Product and Process Development (IPPD) for Dual-Use VTOL Aircraft
Preliminary design of a supersonic Short-Takeoff and Vertical-Landing (STOVL) fighter aircraft
S-92 - Design for Minimum Operating Costs
Performance, Load and Stability of Heavy Lift Tiltrotors
Impact of Airfoils on Aerodynamic Optimization of Heavy Lift Rotorcraft
Impact of Airfoils on Aerodynamic Optimization of Heavy Lift Rotorcraft
Aeromechanic Analysis of a Heavy Lift Slowed-Rotor Compound Helicopter