Influence of nonlinear blade damping on helicopter ground resonance instability
Author:
Affiliation:
1. Duke University, Durham, North Carolina
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45275
Reference7 articles.
1. 2Tongue, B.H. 'Two Studies in Nonlinear Dynamical Systems," Ph.D. Thesis,Princeton University, Princeton, NJ, June 1983; also, "Limit Cycle Oscillations of a Nonlinear Rotorcraft Model," AIAA Journal,Vo\. 22, July 1984, pp. 967-974.
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