Nonlinear Perturbation Theory for Structural Dynamic Systems
Author:
Affiliation:
1. University of Glasgow, Glasgow, Scotland G12 8LT, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.15207
Reference16 articles.
1. Rates of change of eigenvalues and eigenvectors.
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