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Now the MAC is calculated for each wing section and then is combinded to a MAC for the wing and CG is expressed relativly to this overall MAC. | Now the MAC is calculated for each wing section and then is combinded to a MAC for the wing and CG is expressed relativly to this overall MAC. | ||
[[File:Yasim-forces-with-sections.jpg|thumb|Canvas showing yasim internals. CG green, correct MAC calculation using wing sections.]] | [[File:Yasim-forces-with-sections.jpg|thumb|Canvas showing yasim internals. CG green, correct MAC calculation using wing sections.]] | ||