What do you see in flight that makes you feel the CG needs to be "more back" than the plans suggest? My complete WAG is if it is not flying correct with the plans specified CG (within reason) the wing or tail angles/ decalage is likely wrong? Now if we could do the dive test the RC guys do that might help decide its neutral,negative, or positive longitudinal stability.
Not sayin' your wrong, just looking to learn something new regarding CG placement.
The amount of "up elevator warp" I had to put into the H. stab to get it to *not* nose-dive, which was alleviated by removal of noseweight. (granted this is in calm air ... in rough air, I'd plan on adding both noseweight (clay) and elevator trim).
To your point, there are several things of which I am not aware:
> I do not know if my fuselage stick has the correct decalage built in ... it could be really incorrect (1 or 2 degrees is, unfortunately, 3/5ths of not much)
> I do not know if my airfoils are "correct" which affects dynamic stability
>> My wing "airfoil" is really a triangle with a Phillips Entry LE
>> My stab airfoils ... hard to say ... rounded LE and "thinned aft section," but probably not "airfoils" in the truest sense
#2 Zweibox is still in yet-to-be-finished-or-assembled-pieces after my move. Work has been insanity lately, am trying to break free one day and grind on it a bit.
-Dave