It may help
HI all,
I designed the RV-10 airfoil specifically to use the -3 degree flap setting at cruise. The two main benefits are that you keep the fuselage a bit more level, less nose down, and you create a pressure distribution that is a bit more favorable to laminar flow on the lower surface.
We don't get much laminar flow on our riveted aluminum wings with skin seams at the spar, but we do get some.
The more-level fuselage attitude also reduces the trim drag slightly, as well as a slight reduction in fuselage drag.
Evaluating the Roncz airfoil on the RV-9, it would achieve a lot of laminar flow on the bottom if the wing were smooth enough, and I think it has enough reflex designed into it that it already essentially has the effect of slight negative flap built right into it. But that doesn't mean that its incidence on the fuselage is also correct to capture that benefit -- I don't know.
So, I would suggest giving it a try. See if you can rig both the flaps and ailerons to about -2 or -3. Report back what you find. The difference may be very small, so try to use some consistent test procedure if you can -- lots of threads here on the forum about that.
You may want to do the take-off with a small amount of positive flap, although I doubt you would notice any adverse affect of the slight negative flap -- just a slightly longer ground roll and slightly more nose high in climb.