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quailbird
May 18, 2004, 01:12 PM
Up till now I have been flying delta wings, but I am going to make a straight winged airplane. On the chart I have, that I got off the internet on CG, it shows a swept back wing. How do you find the CG on a stright winged airplane?

Marion
May 18, 2004, 01:46 PM
If it is a straight wing with constant cord, then the c.g. should be set at 25% of the wing cord - 25% of the way back from the leading edge.

If it is not a constant cord wing, then it gets a little more complicated.

Sparky Paul
May 18, 2004, 07:16 PM
Put "0" where the computation asks for leading edge sweep.