Stability of Rotor Blade Flapping Motion When the Hinges Are Tilted. Generalization of the "Rectangular Ripple" Method of Solution
- 1 October 1947
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 14 (10) , 583-593
- https://doi.org/10.2514/8.1459
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Rotor blade flapping motionQuarterly of Applied Mathematics, 1947