Basic Development of Hybrid Finite Element Method for Midfrequency Structural Vibrations
- 1 November 1999
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 37 (11) , 1495-1505
- https://doi.org/10.2514/2.629
Abstract
No abstract availableKeywords
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