Hi Guys,
Robert, you are correct vertical CG is about wing alignment on the "roll axis", that is, is the outboard wingtip up or down in relationship to the lines. Joe was measuring the CG on the "yaw axis" , in other words is the nose located inboard or outboard when looked at from the "top-view". This CG location also directly impacts the planes ability to turn on the "pitch-axis", because as you change one CG you also change the other CG.
Over on SSW Al Rabe in his Mustunt IV building series had a photo of the plane hanging by the leadouts , next to a wall that is checked to be plumb and true. The wheels are only an inch or so away from the wall. You measure the distance from the wall to the "front -view" centerline of the leading edge of the wing, on both the inboard and outboard sides, of the wing, measured at an equal span from the "top-view" root chord centerline of the wing. This will work with straight wings or wings with dihedral.
I like this idea much better than messing with plumb bobs , strings ,and etc. The wall gives you an easy, instant and repeatable reference point to check the vertical CG of your airplane. It was one of those "Why didn't I think of that " moments , the instant I saw Al's picture.
One idea that I haven't heard anyone mention they have tried yet is to use a laser level projected vertically onto the"front-view" centerline of the leading edge of the wing right next to where a centerline is drawn. Check if the laser line and the ink line are parallel to each other to find out if the vertical CG is correct. This obviously would not work with dihedral wings but might be do-able with straight wings.
I make no claims at expertise but I think what I said was accurate.
I am also getting ready to replace the bellcrank with a Tom Morris system in a TF Score and would like to see photos of the best way to accomplish that particular job.
PS -I just saw Joe's last post .
Joe moving the leadouts front to back only changes the "yaw-axis" CG. Let me give you an example of vertical CG.
You may have seen pictures of biplane stunters and the leadouts are usually mounted on an inboard strut and not coming out of a wing. The reason they are on the strut is that is where the vertical CG is located that would let wings fly level with the lines. If the leadouts came out of the bottom wing, the plane would fly with the outboard wing tips flying way down in relation to your lines.
Someone gave me a low-wing plane that was imbalanced like this once, and there is not enough flap bending or trim tabs available to fix that mess. Forget stunting, when you get inverted you lose all line tension and it comes in on you big time.
Back, in the 70's Tom Dixon was the first guy I ever read bring up vertical CG issues in his Stephens Akro article.
Most stunt designs account for the vertical CG ,just fine, unless you change something. If a plane is designed for an inverted engine and you change it to a side mounted engine you will change the vertical CG, and so you may have to use heavier wheels or add wheel pants in order to restore the vertical CG.
Some people do make vertically adjustable leadout guides or they may use temporary guides during final construction to locate vertical CG location and then glue in the permanent adjustable leadout guides at that determined height.
Pat Robinson