Vibration analysis of composite turbopropellers using a nonlinear beam-type finite-element approach
- 1 November 1989
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 27 (11), 1606-1614
- https://doi.org/10.2514/3.10308
Abstract
No abstract availableThis publication has 12 references indexed in Scilit:
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