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Old Feb 01, 2013, 07:04 AM
charlespereira is offline
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Brazil, SC, Florianopolis
Joined May 2008
127 Posts
Thank you Adam and Tim!

I will follow your advice! It will be fiberglass, balsa and fiberglass again, maybe a 26g/mē on the internal layer.

Between these layers, the carbon, that will be acting as a spar.

Now I ask: is it necessary to make a spar that goes trough the center of the fuselage?

Or using only carbon along the shape of the fuselage is enough.

I don't know if I made myself clear.

Thanks!

Charles
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Last edited by charlespereira; Feb 01, 2013 at 02:52 PM.
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