A finite element for vibration analysis of twisted blades based on beam theory
- 1 November 1984
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 22 (11) , 1646-1651
- https://doi.org/10.2514/3.8831
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
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