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VTOL Urban Air Mobility Concept Vehicles for Technology Development
The effect of nonlinear elastomeric lag damper characteristics on helicopter rotor dynamics
Rotor Design Options for Improving V-22 Whirl-Mode Stability
Preliminary report on in-flight measurement of rotor hub drag and lift using the RSRA
Performance Optimization of Plate Airfoils for Martian Rotor Applications Using a Genetic Algorithm
Performance of Advanced Heavy-Lift, High-Speed Rotorcraft Configurations
Performance and Design Investigation of Heavy Lift Tiltrotor with Aerodynamic Interference Effects
Optimum Design of a Compound Helicopter
Observations from Exploration of VTOL Urban Air Mobility Designs
NDARC - NASA Design and Analysis of Rotorcraft Validation and Demonstration
NDARC NASA Design and Analysis of Rotorcraft- User Training
NDARC NASA Design and Analysis of Rotorcraft - Theory, Appendix 7
NDARC NASA Design and Analysis of Rotorcraft Theory Appendix 1
NDARC-NASA Design and Analysis of Rotorcraft Theoretical Basis and Architecture
NDARC NASA Design and Analysis of Rotorcraft - Input, Appendix 10
NDARC NASA Design and Analysis of Rotorcraft - Input, Appendix 8
NDARC NASA Design and Analysis of Rotorcraft - Input, Appendix 4
NDARC NASA Design and Analysis of Rotorcraft - Input, Appendix 2
NDARC: NASA Design and Analysis of Rotorcraft
NDARC - NASA Design and Analysis of Rotorcraft
NDARC NASA Design and Analysis of Rotorcraft
NDARC NASA Design and Analysis of Rotorcraft
NASA Heavy Lift Rotorcraft Systems Investigation
Model for Vortex Ring State Influence on Rotorcraft Flight Dynamics
Mars Helicopter Technology Demonstrator
Integration of Rotor Aerodynamic Optimization with the Conceptual Design of a Large Civil Tiltrotor
Influence of Wake Models on Calculated Tiltrotor Aerodynamics
Influence of Lift Offset on Rotorcraft Performance
Influence of Alternative Engine Concepts on LCTR2 Sizing and Mission Profile
In-flight measurement of rotor hub drag using the RSRA - A feasibility demonstration
Improved Mars Helicopter Aerodynamic Rotor Model for Comprehensive Analyses
High-Speed Wind Tunnel Tests of a Full-Scale Proprotor on the Tiltrotor Test Rig
Handling Qualities Optimization for Rotorcraft Conceptual Design
Exploration of Configuration Options for a Large Civil Compound Helicopter
Effects of Rotor Design Variations on Tiltrotor Whirl-Mode Stability
Effects of Rotor Design Variations on Tiltrotor Whirl-Mode Stability
Effects of Blade Sweep on V-22 Whirl Flutter and Loads
Development and Initial Testing of the Tiltrotor Test Rig
Designs and Technology Requirements for Civil Heavy Lift Rotorcraft
Design and Performance of Lift-Offset Rotorcraft for Short-Haul Missions
Conceptual Design of Vertical Lift Aircraft with Future Propulsion System Architectures
Conceptual Design and Performance Analysis for a Large Civil Compound Helicopter
Coaxial Compound Helicopter for Confined Urban Operations
Calculation of the Aerodynamic Behavior of the Tilt Rotor Aeroacoustic Model (TRAM) in the DNW
Calculated performance, stability and maneuverability of high-speed tilting-prop-rotor aircraft
Calculated performance, stability, and maneuverability of high-speed tilting-prop-rotor aircraft
A Quiet Helicopter for Air Taxi Operations
An Assessment of the State-of-the-art in Multidisciplinary Aeromechanical Analyses