Vibration Analysis of Structures by Component Mode Substitution
Author:
Affiliation:
1. Martin Marietta Corporation, Denver, Colo.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.49936
Reference10 articles.
1. A METHOD OF CALCULATING THE NORMAL MODES OF AN AIRCRAFT
2. Branch mode analysis of vibrating systems
3. Dynamic analysis of structural systems using component modes
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