Hi All
First another photo to give you an idea of size verses the Morris Dancer, big ain't it

Kev me old fruit; Bruce is right about the forces involved and the carbon strips are cleaned and epoxied straight to the balsa with weights on top to get a good bond, you need to step back from the FAI thing as the panel sizes are small (see plan) and Kevlar would be an overkill. The bottom carbon spar is locked in place by being the meat in the sandwich, it goes nowhere

And there is no Dee box, it's a solid leading edge.
Rey; what I did was took a stick of spruce about 1/4" wide, 1/2 rounded one end then with a steel ruler as a guide, indented the balsa and scored a line the length of the panel light enough for the carbon strip to sit in.
The moment arm dimension is now fixed at 20" and the dihedral on the stab is 1.5" per side. The boom will be a GForce SUL (I have a few of them) as they appear to have adequate stiffness for a modest weight.
With no experience with DLG's other than the short time spent with Len I stuck the finger pin as indicated on the photo and I found no appreciable increase in pressure on the top part, if any thing it equals out once you get twirling.
As of this posting I can now report that the wing is finished ready for gluing to the yet to be made fuselage. It came in at 56.8 grams which is 1/2 gram lighter than the Morris Dancer wing BUT is 36% larger in area which I calculate as being about 20 grams less than equivalent all balsa wing

Ployd