I would consider that insignificant, a bit unsightly, but should have little
affect.  However, please note that my closest encounter with being an
aeronautical engineer was the night that I stayed at a Holiday Inn Express. 

See N64KR at http://KRBuilder.org - Then click on the pics 
See you at the 2007 - KR Gathering
There is a time for building and a time for FLYING and the time for Flying
has begun.
Daniel R. Heath - Lexington, SC
-------Original Message-------

From: bobby burington
List-Post: [email protected]
Date: 04/23/07 01:45:34
To: KRnet
Subject: Re: KR> wing airfoil shape

Sory about that, this is my first time web building,  but here is another
link to the pictures and I think this one will work. I hope.

  http://bobskr.white.prohosting.com/wing.htm

  thanks
  Bob

Darren Crompton <[email protected]> wrote:
  The link takes me to the freeprohosting page and not to your photo.


On 4/23/07, bobby burington wrote:
>
> Hello Mark,
>
> thanks for the input ,
>
> I have posted some pictures of the wing. its kind of hard to see how bad
> the distortion is from the pictures but I tried.
> the wing already has a thin skin of fiberglass over it so if I do as you
> suggest I will have to sand down to the spar, then glue in a new piece of
> wood over the spar cap then re-glass the wing skin. ?. Then will it hurt
to
> make the new Spar cap a little wider so the old skn will lay over it when
> re-glasing ?.
>
> Thanks
> Robert
>
> bobby burington wrote:
>
> > I have discovered a small problem with one of the wings on this plane
> > project I have sort of inherited , the rear spar is about 3/16 shy of
> what
> > is called for in the plans and the airfoil is slightly misshapen because
> > of this.
>
> If you are saying that the spar is not tall enough, you need to use T-88
> or
> some other suitable epoxy to glue some more wood on top of the spars,
> rather
> than use foam to make up the difference to get to the airfoil profile. The
> skin's connection to the rest of the plane is done through the spar cap,
> and
> foam cannot support the load (it is structurally "useless").


---------------------------------
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