Looks like I'll leave the thrust angle alone then.

I am all for matching the incidences so now I am thinking it through. The wing is designed to have 1.5 degrees of incidence and the stabilizer has zero. If I repositioned the stab to 1.5, would this mean that the fuseage would tend to travel through the air in kind of a pitch oriented skid? I see an easy way to cleanly and permanently reposition the stab but wouldn't want to if there is a penalty in performance that I would notice in which case I'll change the wing. What do you all think?

Greg