Pitch damping of helicopter rotor with nonuniform inflow
- 1 October 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 11 (10), 639-646
- https://doi.org/10.2514/3.44396
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Dynamic analysis of the rigid rotor system.Journal of Aircraft, 1967
- Rotor blade harmonic air loadingAIAA Journal, 1964