Performance Analysis of a Micro-scale Model Helicopter Rotor in Hover Flight

2015-09-12
This experimental study contains the design, production, test and evaluation of the test processes of a Micro-Scale Rotor Test-Rig. For the study, NACA 0012 airfoil section is selected as a rotor blade without a twist and a taper ratio. The tests cover the thrust and the torque relation with different blade pitch angles and RPM values.
8 th ANKARA INTERNATIONAL AEROSPACE CONFERENCE ,10-12 September 2015

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Citation Formats
M. Şahin and D. F. Kurtuluş, “Performance Analysis of a Micro-scale Model Helicopter Rotor in Hover Flight,” presented at the 8 th ANKARA INTERNATIONAL AEROSPACE CONFERENCE ,10-12 September 2015, METU, Ankara TURKEY, 2015, Accessed: 00, 2021. [Online]. Available: http://aiac.ae.metu.edu.tr/paper.php?No=AIAC-2015-044.