Have a look at the Bushby Mustang 2 folding wing set up. Search 
http://www.mustangaero.com
The Mustang 2 has leading edge wing tanks and folding  wing for transport   
Phil. 

Sent from my iPhone

> On 15 Dec 2020, at 17:08, Michael via KRnet <krnet@list.krnet.org> wrote:
> 
> Greetings
> 
>  This discussion throws my idea of stub tanks right out the window and
> with good reason as I am a complete novice (onlly just started finishing
> this project) and did not adequately consider CG.  Rather learn on the
> ground than in the air!  As a skydiver I have a good understanding of how
> weight affects flight :)
> 
>  Next question if I may; wing leading edge tank (infront of main spar),
> Wing chord tanks (behind main spar) or wing tip tanks?  Considering that I
> am wanting to make the main wing foldable (fold up then sideways aft) for
> trailer storage & transport; which would be the better option and how to
> ensure the piping etc will work with folding wings?
> 
> Regards
> שָׁלוֹם עֲלֵיכֶם (Shalom aleichem)
> 
> Michael L Griffin
> mileg...@gmail.com
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> Cel : +27 83 462 0462
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> 
> He who play in root,
>                     eventually kill tree.
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> 
>> On Tue, 15 Dec 2020 at 04:31, Flesner via KRnet <krnet@list.krnet.org>
>> wrote:
>> 
>>> On 12/14/2020 7:44 PM, Mark Wegmet via KRnet wrote:
>>> The CG issue would (I would think) depend on
>>> placement of the tanks - wing or tip - relative to the "normal" CG
>>> calculations for the airframe.
>> 
>> +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
>> 
>> That is correct as with anything with weight attached to the aircraft.
>> The closer to the desired CG location the better.  My tanks are in the
>> area 10" behind the main spar with most of the weight in the CG
>> envelope.  Other than the weight I can't really tell what my fuel load
>> is from how how the aircraft handles. Pitch forces remain almost
>> constant from full to empty tanks.
>> 
>> Larry
>> 
>> 
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