Stiffness matrix adjustment using mode data
Author:
Affiliation:
1. The Aerospace Corporation, El Segundo, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.9103
Reference17 articles.
1. A method for deriving structural influence coefficients from ground vibration tests.
2. LINEAR ESTIMATION OF STRUCTURAL PARAMETERS FROM DYNAMIC TEST DATA
3. Theory of Incomplete Models of Dynamic Structures
4. Discrete Model Improvement by Eigenvector Updating
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