Mark,
   So if I'm reading this correctly,  since i am building a standard kr-2, 
but using the new airfoil, I need to use waf's for a kr-2s.  Is that 
correct? Also, if I already have kr-2 waf's, can you have the other aft 
waf's bent to 3 degrees without any problems?  Thanks for any help.   Jim



>From: "Mark Langford" <n5...@hiwaay.net>
>Reply-To: KRnet <kr...@mylist.net>
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>Subject: Re: KR> AS504x wing sections
>Date: Fri, 10 Dec 2004 14:39:20 -0600
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>Steve Jacobs wrote:
>
> > The Ashok sections generated and made available by your kind self and
> > others offer the 48" section, but offer a shorter section for the tip -
> > closer to 30".
> > No doubt a good reason, but I am missing it.
> > If you have a moment, maybe talk about the differences in the selection
> > of airfoils included in the pdf file.
>
>Ashok designed that airfoil specifically for the KR2S, but the set of 
>points
>he generated was for a standard "unity" profile, based on the chord length
>being 1.000.  Not that it won't work just fine on a KR2, but at the time, I
>couldn't imagine anybody wanting to build a KR2 wing if they were starting
>from scratch, so the templates are also designed for the KR2S, rather than
>the KR2, hence the lack of a 36" chord tip template.  The S wing planform 
>is
>different, by virtue of the fact that the aft WAFs (wing attach fittings)
>are ALL bent 3 degrees, rather than just half, so the aft spar rakes 
>forward
>6 degrees.  That makes the template at the end of the spar smaller (33"),
>and answers your question.  The wing area is compensated for by adding a
>hoaky foam extension.  The drawings that I made allow for the
>forward-thinking builder to make his spars longer, and include a template
>(30-11/16") for a tip located way out at 132.75" from the centerline.
>There's a dotted  outline of a spar and the mention of this option printed
>on the template itself.  There are a lot of details on these templates that
>I put in just to make building them easy and more foolproof.
>
>Mark Langford, Huntsville, AL
>N56ML at hiwaay.net
>see KR2S project N56ML at http://home.hiwaay.net/~langford
>
>
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