Unsteady aerodynamic and stall effects on helicopter rotor blade airfoil sections.
- 1 January 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 6 (1) , 46-51
- https://doi.org/10.2514/3.44000
Abstract
No abstract availableKeywords
This publication has 0 references indexed in Scilit: