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

Copy For Citation

Uluocak S., Hazaveh H. A. , PERÇİN M. , Akpolat M. T. , UZOL O.

44th European Rotorcraft Forum, 18 - 21 September 2018

Publication Type: Conference Paper / Full Text