Optimal placement of tuning masses for vibration reduction in helicopter rotor blades
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.10390
Reference21 articles.
1. 3Taylor, R. B. "Helicopter Rotor Blade Design for Minimum Vibration," NASA CR-3825, Oct.1984.
2. Blade Design for Reduced Helicopter Vibration
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