Feb 20, 2013, 02:07 AM
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Port Fairy, Australia
Joined Jun 2005
1,972 Posts
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Thanks for the reply. I will shoot you an email as well.
FAI rules actually count the fuselage area under the wing and the tails by some quirk of ancient free flight history.
I remember seeing a pantograph being used during processing for an Electric W/C years ago and weights being checked to then see a few embarrassed pilots super gluing bits of balsa to tailplanes to make the loading
Based on your numbers and the fairly slim fuz I guess safe area is going to be 26dm for a max wt of 1950+g or 69oz'ish. So based on Ezza's recent build (2080) not much to lose at all. Lose an Oz at the tail and 4 in the nose to match and it would be a close thing
The only other minor one might be the nose Radius as per below but some sandpaper if I ever take it toward record attempts will do the job.
That 59oz version looked good in the air too but I reckon the 300g of materials would be well worth it for taking some more G's.
Sorry Geek Stuff
1.4.1. Surface Area
The surface area includes the total surface of the wings and that of the horizontal or oblique stabilising
surface or surfaces. The surfaces taken for calculation are the orthogonal projection on to a horizontal
plane of the surfaces in question with each surface at zero incidences.
When wings or stabilising surfaces are built into the fuselage of the model aircraft the surface taken into
account shall include that area contained within the normal contours of the flight surfaces extended so as
to meet at the plane of symmetry of the model.
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Last edited by tim_mellor; Feb 20, 2013 at 02:19 AM.
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