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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

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