Coupled Helicopter Rotor/Flexible Fuselage Aeroelastic Model for Control of Structural Response
- 1 October 2000
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 38 (10), 1777-1788
- https://doi.org/10.2514/2.838
Abstract
No abstract availableThis publication has 13 references indexed in Scilit:
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