Good to hear that's a none issue for the KR2 safety! Even if it is not the
strongest section on the airframe, I too, don't see much of the torsional
stresses potentially harmful to the skin of the stub wings, except when we
step on it with a hard bottom shoes....

Also, assuming we use tapes to cover up the opening at the KR2 wing joints,
would it be a big safety hazard if the type gets blown off somehow during a
cruise speed beyond 150mph, perhaps? I don't think anyone had done any wind
tunnel test concerning flight dynamics of KR2...

Dr. Hsu

On Mon, Apr 6, 2020, 1:54 PM Mark Langford via KRnet <krnet@list.krnet.org>
wrote:

> I wrote:
>
>  > Call me skeptical of this....very skeptical.  Torsional failure of the
>  > SKIN between front and aft spars in the stub wing area?  Really? So
>  > what?
>
> And the whole premise of the KR is that the load bearing structure of
> the KR is the spruce and plywood....the fiberglass skins are just there
> for the aerodynamic loads, and so far that seems to be working just fine
> for every flying KR on the planet.
>
> I refuse to get wrapped around the axle on this....it's a non-issue that
> somebody is using to justify their job, or like I said, maybe there's a
> loss in the translation somewhere.  Either way, a non-issue.....
>
> Mark Langford
> m...@n56ml.com
> http://www.n56ml.com
>
>
>
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