Swashplateless Helicopter Rotor System with Trailing-Edge Flaps for Flight and Vibration Controls
Author:
Affiliation:
1. National Institute of Aerospace, Hampton, Virginia 23666
2. Northwestern Polytechnical University, Xi’an 710072, People’s Republic of China
3. 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/10.2514/1.14634
Reference24 articles.
1. Status of Application of Smart Structures Technology to Rotorcraft Systems
2. Vibration reduction in rotorcraft using active control - A comparison of various approaches
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