Effect of Modified Aerodynamic Strip Theories on Rotor Blade Aeroelastic Stability
- 1 July 1977
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 15 (7), 932-940
- https://doi.org/10.2514/3.60735
Abstract
No abstract availableKeywords
This publication has 12 references indexed in Scilit:
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