Aeroelastic stability of hingeless rotor blade in hover using large deflection theory
- 1 July 1994
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 32 (7) , 1472-1477
- https://doi.org/10.2514/3.12217
Abstract
No abstract availableThis publication has 20 references indexed in Scilit:
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