Investigation of the Effect of Blade Sweep on Rotor Vibratory Loads
Loads and Stability Analysis of an Unmanned Tilt Rotor
Design and Performance Analysis of a Prototype Circulation Control Helicopter Rotor
Hot Cycle Rotor System. Volume II. Rotor Blade Structural Analysis
Use of a Portable Programmable Guidance Display in Support of Helicopter Noise Testing
Helicopter Rotor Blade Computation in Unsteady Flows Using Moving Overset Grids
Military Potential Test of the Model 135M Blade Tracker
Center for Excellence for Rotary Wing Aircraft Technology
Adaptive Rotor Blade Concepts -Direct Twist and Camber Variation-
Advancing Blade Concept (ABC) Technology Demonstrator
Future Directions in Rotorcraft Technology at Ames Research Center
Time Domain Analysis of a Rigid Two-Bladed Fully Gimballed Helicopter Rotor with Circulation Control