Experimental Investigation ofthe Hovering Performance of aTwin-Rotor Test Model

Farid Shahmiri

Volume 10, Issue 2 , September 2013

  Hover performance of a twin-rotor test model in terms of rotor overlap sweep, blade collective pitch, and blade tip speedwasexaminedexperimentally.The experimental setup consisted of two three-bladed rotors (tandem rotor configuration) with a diameter of1,220 mm and constant chord of 38 mm, giving a ...  Read More