Structural eigenvalue problems - elimination of unwanted variables
Author:
Affiliation:
1. Rolls Royce Ltd., Derby, England
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.3027
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1. Measurements of test time in the galcit 17-inch shock tube
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4. BASIS FOR DERIVATION OF MATRICES FOR THE DIRECT STIFFNESS METHOD
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