Oh, and one more thing is that during the bending process, the verticals end
up "twisted" a little, so that gap tightens up, and you'll probably have to
shave a little off of the vertical member that mates up to the front main
spar, and also the vertical that faces the aft face of the aft spar.
Erik Kline wrote:
> the two should be 21.625", not 21.56" right. Upon further inspection
> there
> should be a 1/32" gap between the main spar and the vertical member behind
> it. Adding that to the total gives me 21.65625". I know its splitting
> hairs, but it will change how much material co
In the drawing for the AS5048 root airfoil, it shows a distance of 21.56"
between the main and aft center spars. Looking at my plans, there is a
10.75" bay behind the main spar, followed by another 10.25" bay before the
forward vertical member of the aft spar. Now that's 21" for the bays and
the
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