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Re: Carbon Dragon structural limits 10 Dec 2013 22:44 #548

--- In This email address is being protected from spambots. You need JavaScript enabled to view it., russell wilson wrote:
>
> hi kenny
Hi all,
For what it is worth the actual load tests were done on the full wing.
I have an article from Kitplane Magazine May of 1993. There is a photo of them loading the wing. The caption stated load tested to 5g's. I'll scan the article and upload it within a few days if any one would like to see it.

And Steve's post of the CD video's contained a video of the ULF-1. No big deal but I am the author of that video. I was going to build an ULF-1. Still may one day but not out of wood. Still pondering building the carbon dragon also.

Sincerely,
Schnka Or Schneider, Karl

> im not knocking the rods or any ones work.....im simply pointing out that
> no matter what caps or strenth any of us have......the weak point is were
> the holes are drilled at the root where the highest load is and that any
> thing stronger/out board of this point is for nort.......actually it
> becomes a weight penalty......
>
> were the calculations done on one or two pice wings?
>
> russ.

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