The design report
The design report
The design report
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Appendix D – Control surface sizing<br />
AILERONS<br />
wingspan<br />
(mm) 2300<br />
wing chord<br />
(mm) 260<br />
aileron chord<br />
(% of wing<br />
chord)<br />
aileron<br />
chord<br />
(mm)<br />
span (min)<br />
(% of wing<br />
span)<br />
span (max)<br />
(% of wing<br />
span)<br />
span<br />
(min)<br />
(mm)<br />
span<br />
(max)<br />
(mm)<br />
each<br />
aileron<br />
(min)<br />
(mm)<br />
each<br />
aileron<br />
(max)<br />
(mm)<br />
30 78 35 40 805 920 402.5 460<br />
35 91 35 40 805 920 402.5 460<br />
ELEVATOR<br />
h tail chord<br />
(mm) 180<br />
h tail span<br />
(mm) 763<br />
chord (% of<br />
elevator<br />
chord<br />
tail chord) (mm)<br />
30 54<br />
35 63<br />
RUDDER<br />
v tail base<br />
length (mm) 240<br />
v tail height<br />
(mm) 188<br />
chord (% of<br />
rudder<br />
chord<br />
tail chord) (mm)<br />
30 72<br />
35 84<br />
FINAL<br />
SIZING<br />
chord<br />
(mm)<br />
span/height<br />
(mm)<br />
elevator<br />
span % of<br />
tail span<br />
elevator<br />
span<br />
mm<br />
90 686.7<br />
95 724.85<br />
rudder<br />
rudder<br />
height<br />
height % mm<br />
90 169.2<br />
95 178.6<br />
Aileron (each) 91 460 90 440<br />
Rudder<br />
(each) 84 178.6 84 178<br />
Elevator 63 724.85 63 743