Induced flow variation of the helicopter rotor operating in the vortex ring state.
- 1 July 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 5 (4) , 381-386
- https://doi.org/10.2514/3.43954
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Experiments on a model helicopter rotor operating in the vortex ringstate.Journal of Aircraft, 1966
- Flight Testing of HelicoptersJournal of the Royal Aeronautical Society, 1948