Hey Guys,
I have a simple question here. I have built the Dynam C-188 and I noticed several threads that said the CG as posted in the instructions was off, (90-100mm), and instead recommended a CG of 65mm from the leading edge. Now I know that generally, you take the leading edge at the fuselage, and measure back from there. Well, the C-188 has a pretty sharp triangular sweep starting at the fuselage and tapering back to what I will call the main leading edge of the wing. If I measure 65mm from the fuselage, the CG is only about an inch from the main leading edge. This looks kind of forward to me, but I would certainly rather have it nose heavy than tail heavy. The instruction have a picture showing CG about in line with where the Flap and Aileron wires come down the wing.
Have any of you guys run into this, and can you let me know where you balanced your plane?
Thanks!
I have a simple question here. I have built the Dynam C-188 and I noticed several threads that said the CG as posted in the instructions was off, (90-100mm), and instead recommended a CG of 65mm from the leading edge. Now I know that generally, you take the leading edge at the fuselage, and measure back from there. Well, the C-188 has a pretty sharp triangular sweep starting at the fuselage and tapering back to what I will call the main leading edge of the wing. If I measure 65mm from the fuselage, the CG is only about an inch from the main leading edge. This looks kind of forward to me, but I would certainly rather have it nose heavy than tail heavy. The instruction have a picture showing CG about in line with where the Flap and Aileron wires come down the wing.
Have any of you guys run into this, and can you let me know where you balanced your plane?
Thanks!

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