This site gives a good way to calculate your c.g. range based on taper and
sweep...figure 15 to 35 % mac

http://www.nasascale.org/howtos/mac-calculator.htm

https://sites.google.com/site/mykr2stretch/
https://sites.google.com/site/mykr2stretch/parts-for-sale
On Mar 30, 2016 8:14 PM, "Pete Klapp via KRnet" <krnet at list.krnet.org>
wrote:

> KRNetters
> I am in the process of determining the cg on my project. In comparing cg
> location, RR plans show the 8" cg range with the fwd edge of the range
> starting 8" aft of the leading edge of the wing. Based on the profile of
> the 48" rib, the leading edge of the cg range is 2" fwd of the front face
> of the main spar. I have Diehl RAF - 48 skins along with inboard skins that
> Jeannette Rand also produced. With those, the leading edge of the wing is
> 11.5" fwd of the front spar face, an 1.5" fwd of RR plans. Should I move
> the cg envelope fwd by that 1.5" or use the cg range set by RR.
> Next question: Preliminary calculations show my empty cg is approx. an 1"
> fwd of the RR cg location. Knowing that any weight added, passengers, fuel,
> baggage, etc will fall push the flying cg aft, should I fabricate my engine
> mount using this calculated engine position?
> I have done calculations with pilot plus 1/2 fuel and it falls at 2" into
> the RR cg range, and pilot & passenger plus 3/4 fuel and cg falls within 6"
> preferred cg range, the later coming in right at the aft edge of the
> preferred range. I'm thinking that I would like set the engine such that
> with me and 1/2 fuel that the cg falls right at the fwd cg limit.
>
> Next question: The horizontal engine centerline with the temporary engine
> mount is 2.5" below the top of the upper longerons. I'd like to drop the
> centerline a little more, 1/2 to 3/4", for better clearance for engine
> cowling and cooling plenum. Anyone see a problem with that.
> All advise cheerfully accepted,
> Thanks in advance for any and all assistance.
> Pete Klapp
>
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