Those who know
My test pilot has calculated MAC
(mean aerodynamic chord) in my case
(Europa XS Mono w standard wings)
to be 1123 mm (=44,2").
He would like to know its (front points)
distance to the reference point (fuselage datum).
Any idea of that?
He would like to compare MACs position
to the C of G position in per cent, beause it tolds
him aerodynamically more than arms only.
XRTs C of G arm is 1496 mm (=58,9").
Thanks, Raimo
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Raimo M W Toivio
OH-XRT Europa XS Mono #417, FCAA cleared for test flights.
OH-CVK C172 Skyhawk, reinterioring completed
OH-BLL Beechcraft C45, w radial engines (grounded)
37500 Lempaala
Finland
tel + 358 3 3753 777
fax + 358 3 3753 100
gsm + 358 40 590 1450
raimo.toivio@rwm.fi
www.rwm.fi
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