Helicopter Sizing by Statistics - Faculty of Aerospace Engineering
Helicopter Sizing by Statistics - Faculty of Aerospace Engineering
Helicopter Sizing by Statistics - Faculty of Aerospace Engineering
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Tail Rotor Blade Chord (m)<br />
0.5<br />
0.4<br />
0.3<br />
0.2<br />
0.1<br />
0<br />
AHS Forum 58, June 2002<br />
Tail Rotor Blade Chord & Solidity<br />
Database configurations<br />
(without FENESTRON)<br />
0 0.1 0.2 0.3 0.4 0.5<br />
Tail Rotor Blade Chord Estimation (m)<br />
c = . W N ,<br />
TR<br />
/ 0<br />
b TR<br />
0058 0506 . . 720<br />
0<br />
c W<br />
ε ε<br />
where TR is in [ m] and 0 is in [ kg]<br />
( AVER = 10%, MAX = 30%, R = . 9437).<br />
<strong>Faculty</strong> <strong>of</strong> <strong>Aerospace</strong> Eng., Technion - I.I.T.<br />
18
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