An approximate method for nonlinear ordinary differential equations
Author:
Affiliation:
1. The Boeing Company, Seattle, Wash.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.6335
Reference12 articles.
1. Free Vibrations of a Pin-Ended Column With Constant Distance Between Pin Ends
2. NON-LINEAR DEFORMATION OF A FLEXIBLE RING
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