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Old June 5th 11, 09:53 AM posted to rec.aviation.homebuilt
Philippe[_4_]
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Posts: 26
Default Filament wound airfoils. (again)

le dimanche 5 juin 2011 01:17, s'est penché sur son écritoire numérique:

I imagine a simmilar technique might be servicable for experimental
aircraft. paper fiber honeycomb is used as packing material and can
probably be had quite cheap. I was thinking, cut it to form, attach it
to the spar, drown the whole lot in epoxy. Then after it cures
filament wind it to make the skin.

More difficult than layout carbon fabric and require more tools.

I prefer the basic
1 layer bid 0°/90°,
1 layer biaxial ±45°,
1 layer bid 0°-90° in a simple wood mold

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http://www.youtube.com/watch?v=1ODCf7J8L0o
Philippe Vessaire Ò¿Ó¬