The Prediction of Helicopter Rotor Hover Performance using a ...
The Prediction of Helicopter Rotor Hover Performance using a ...
The Prediction of Helicopter Rotor Hover Performance using a ...
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Relative<br />
induced<br />
torq,ue<br />
Relative<br />
pr<strong>of</strong>ile<br />
torque<br />
hi<br />
1-0<br />
12<br />
U<br />
t 0-2<br />
1<br />
0-2 0-4 0-6 0-8 1-0<br />
0-4 p 0-6 0-8 1-0<br />
Fig. 17 Relative torque distributions for Wessex main rotor
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