TonyHallo
150cc
It is my understanding that using the graphical method locates the mean aerodynamic chord, from there you need to determine at what percentage of the chord you want to fly at. 15% to 33% is the range that I can remember where the low side would be used for high lift flat bottom type wings and the high end would be used for aerobatic aircraft. Anything above approximately 33% becomes unstable, tail heavy. I built a Hurley Extra 300 many years ago, on the test flight I rolled inverted and it climbed at a 45 degree angle, landing was fun but not really uncontrollable, using down to land is just not normal.
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