My point of contention here is not whether it'll work or not work and in 
Barry's case for the last 8 inches of the wing spar I'm sure the loads are 
slight  towards the tips and Larry using it in his canopy  bows is in a non 
critical area of the airplane. There are a lot of people looking in at this 
site to learn how to do composite work and we got complimented as being a very 
informative source of information. I personally don't think it's a good 
practice to do in the critical areas of the primary structure and would like 
point out my views to the builders that are just getting started as we don't 
want any mishaps happening because of misinformationLarry&Sallie Flesner 
<[email protected]> wrote:  At 09:44 PM 8/24/2006, you wrote:
>I'll express an apprehension here about using a layer of
>fibereglass cloth in a glue joint. It has been my experience
>with a cloth and resin layup that it is strong in tension and
>has some compressive strength but has no peel strength
Don Chisholm
++++++++++++++++++++++++++++++++++++++++++++++++++++++

I don't expect my canopy or turtledeck bows to ever have any "peel"
loads applied. Also, what changes in a glue joint from a single
layer of glass to wood (wing skins to spar) and multiple layers
of glass to wood ( wood-glass-wood-glass-wood-glass,etc.) ?
I think I left enough epoxy in the glass layers to get a good bond
to the wood, through the glass, and to the next layer of wood.
I really don't expect my "bows" to fail in any kind of incident that
would be otherwise survivable. I'm not concerned enough to
test my installed bows to failure or build a test bow to test.
However, do not view my installation as a "commonly accepted
building practice". I have no personal knowledge of this type of
component being tested, other than by my flight time.

Larry Flesner



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