Transient Loads Control of a Variable Speed Rotor During Lagwise Resonance Crossing
Author:
Affiliation:
1. Aerospace Engineering, Pennsylvania State University, University Park, Pennsylvania 16802
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J050598
Reference15 articles.
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2. JohnsonW.YamauchiG. K. “NASA Heavy Lift Rotorcraft Systems Investigations,” NASA TP-2005-213467, Dec. 2005.
3. Broadband vibration damping in beams using distributed viscoelastic tuned mass absorbers
4. Rotorcraft blade lag damping using highly distributed tuned vibration absorbers
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