Experimental investigation of the effects of different helicopter rotor tip geometries on aerodynamic performance and tip vortex characteristics | AVESİS

Middle East Technical University Research Information System

Experimental investigation of the effects of different helicopter rotor tip geometries on aerodynamic performance and tip vortex characteristics

Copy For Citation

Uluocak S., Hazaveh H., Perçin M., Akpolat M., Uzol O.

44th European Rotorcraft Forum 2018, ERF 2018, Rotterdam, Netherlands, 18 - 21 September 2018, vol.1, pp.199-207

Publication Type: Conference Paper / Full Text
Volume: 1
City: Rotterdam
Country: Netherlands
Page Numbers: pp.199-207
Middle East Technical University Affiliated: Yes