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NASA Heavy Lift Rotorcraft Systems Investigation
Designs and Technology Requirements for Civil Heavy Lift Rotorcraft
Conceptual Design of Vertical Lift Aircraft with Future Propulsion System Architectures
Coaxial Compound Helicopter for Confined Urban Operations
Performance Optimization of Plate Airfoils for Martian Rotor Applications Using a Genetic Algorithm
Airloads and Wake Geometry Calculations for an Isolated Tiltrotor Model in a Wind Tunnel
NDARC NASA Design and Analysis of Rotorcraft - Input, Appendix 4
Handling Qualities Optimization for Rotorcraft Conceptual Design
NDARC NASA Design and Analysis of Rotorcraft Theory Appendix 1
NDARC NASA Design and Analysis of Rotorcraft - Theory, Appendix 7
NDARC NASA Design and Analysis of Rotorcraft - Input, Appendix 8
Influence of Wake Models on Calculated Tiltrotor Aerodynamics
Analysis of Advanced Rotorcraft Configurations
NDARC NASA Design and Analysis of Rotorcraft - Input, Appendix 2
Calculation of the Aerodynamic Behavior of the Tilt Rotor Aeroacoustic Model (TRAM) in the DNW
Observations from Exploration of VTOL Urban Air Mobility Designs
VTOL Urban Air Mobility Concept Vehicles for Technology Development
Application of the joined wing to tiltrotor aircraft
The effect of nonlinear elastomeric lag damper characteristics on helicopter rotor dynamics
Calculated performance, stability and maneuverability of high-speed tilting-prop-rotor aircraft