Acoustic Flight Tests of Rotorcraft Noise-Abatement Approaches Using Local Differential GPS Guidance
Adaptive Rotor Blade Concepts -Direct Twist and Camber Variation-
Advancing Blade Concept (ABC) Technology Demonstrator
Analysis and Correlation of Test Data from an Advanced Technology Rotor System
Calculation of the Aerodynamic Flow Field in the Vicinity of a Sea King Helicopter
Center for Excellence for Rotary Wing Aircraft Technology
Correlation of Puma Airloads-Lifting-Line and Wake Calculation
Design and Performance Analysis of a Prototype Circulation Control Helicopter Rotor
Directionality of Helicopter Noise and Its Exploitation
Dynamic Stall on Advanced Airfoil Sections
Effect of Rotor Blade Root Cutout on Vertical Drag
Future Directions in Rotorcraft Technology at Ames Research Center