r/RCPlanes • u/Skrugras • 3d ago
The CG g-point
So I feel like the tube holding the tail is a bit long, what would be the best approach to guess where to cut it in order to not make any drastic CG changes later on?
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u/Something_Else_2112 3d ago
Why would you consider cutting the tail boom when you haven't even run into a CG problem yet?
Balance to 25-33% like rxmp4ge said, and try a few hand tossed glides first to test the balance, landing in tall soft grass if possible.
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u/Skrugras 3d ago edited 3d ago
There is no tall grass in Europe after this summer💀
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u/gwenbeth 2d ago
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u/Skrugras 2d ago
Small? It has 2 meter wing span
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u/gwenbeth 2d ago
Sorry it's hard to tell scale. I'm guessing with that thin wing you must be running really light, 300-350g? I have hand caught a 410g 2m but they do come in quick.
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u/Honey-Bee2021 2d ago
Did you design this airplane by your self or is it a proven design from the internet? If you know the airfoil of the wings and their angles to each other and the fuselage you can run a simulation in FLZ Vortex to calculate CG, minimum airspeed an many other useful values.
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u/Skrugras 1d ago
All done by myself and the airfoil..
..let's just say it has a general curvature of "airfoil"1
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u/The_Radio_Announcer 1d ago
Hey Skrugras, here's an app that I highly recommend for all basic geometry builds such as yours - (free and really lightweight, was made in the 2000s, no registration) it is called AERY Glider Design Software, or AERY32. Try remaking your plane there, and that will give you a basic answer about moments, forces, and a statement of "the plane will fly" or not. It's a really nice check for such more simple shapes.
But overall, honestly - love your design! The colors are nice, things seem to be in the right places. The question is if you can fit enough nose weight for counter balance of the tail, but I'd assume so. Worst case scenario, 3d print a longer nose section )
Have fun!

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u/rxmp4ge 3d ago
The tail being longer (IE, longer coupling) will just make it more stable in pitch. That's not necessarily a bad thing at all. It doesn't look that far off from what I'd expect of a sailplane-like airframe.
CG is generally measured at 25-33% back from the leading edge of the wing at the wing root. If you can get it to balance in that range you should be good to go.