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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
Similarly Configured Public Use Vertical Airports for VSTOL Commuter Aircraft
Concept Selection of a New Design to Meet the Medium Lift Replacement (MLR) Helicopter Requirements
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
Sikorsky Design Concepts for NASA Heavy Lift Rotorcraft Systems Investigation
Full Scale Flight Acoustics Results for the UH-60A Airloads Aircraft
Integrated Product and Process Development (IPPD) for Dual-Use VTOL Aircraft
S-92 - Design for Minimum Operating Costs
Performance, Load and Stability of Heavy Lift Tiltrotors
STOVL Propulsion System Selections Effect on Aircraft Design
Designs and Technology Requirements for Civil Heavy Lift Rotorcraft
The Impact of Integrated Product Development on the Helicopter Design Process