Tip vortex core measurements on a hovering model rotor
- 24 March 1987
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Velocity measurements in the near field of a rotor blade in hoverPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Experimental results for Reynolds number effects on trailing vorticesJournal of Aircraft, 1985