Analysis and Testing of Mach-Scaled Rotor with Trailing-Edge Flaps
Author:
Affiliation:
1. University of Maryland, College Park, Maryland 20742
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1086
Reference24 articles.
1. Application of Higher Harmonic Control to Rotors Operating at High Speed and Thrust
2. Higher Harmonic Control: Wind Tunnel Demonstration of Fully Effective Vibratory Hub Force Suppression
3. On Developing and Flight Testing a Higher Harmonic Control System
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