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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
Rotorcraft Conceptual Design Environment
Rotorcraft Conceptual Design Environment
Prediction of SA 349/2 GV blade loads in high speed flight using several rotor analyses
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
Overview of the Testing of a Small-Scale Proprotor
Optimum Design of a Compound Helicopter
NDARC - NASA Design and Analysis of Rotorcraft Validation and Demonstration
NDARC-NASA Design and Analysis of Rotorcraft Theoretical Basis and Architecture
Mars Helicopter Technology Demonstrator
Influence of Lift Offset on Rotorcraft Performance
Improved Mars Helicopter Aerodynamic Rotor Model for Comprehensive Analyses
Full-scale investigation of aerodynamic interactions between a rotor and fuselage
Exploration of Configuration Options for a Large Civil Compound Helicopter
Designs and Technology Requirements for Civil Heavy Lift Rotorcraft
Design and Performance of Lift-Offset Rotorcraft for Short-Haul Missions
Correlation of SA349/2 helicopter flight-test data with a comprehensive rotorcraft model
Correlation of SA349/2 helicopter flight-test data with a comprehensive rotorcraft model
Conceptual Design and Performance Analysis for a Large Civil Compound Helicopter