Ground Vibrations of Helicopters
Author:
Affiliation:
1. Air Materiel Command,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.11359
Reference10 articles.
1. Design gross and landing weight = 40,000 Ibs. Limit landing load factor = 3.0g Tires = 17.00-20 L.P. Shock strut = 6-in. diameter piston-13-in. stroke
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3. Lead-Lag Damper Robustness Analysis for Helicopter Ground Resonance;Journal of Guidance, Control, and Dynamics;2013-07
4. Milestones in Rotorcraft Aeromechanics Alexander A. Nikolsky Honorary Lecture;Journal of the American Helicopter Society;2011-07-01
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