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C r below is the core chord of the wing.<br />
A.C.<br />
tail<br />
control-fixed<br />
static margin<br />
apex of<br />
wing<br />
wing<br />
A.C.<br />
mac<br />
c.g<br />
positive for<br />
static<br />
stability<br />
wing_4_generic.vsdx<br />
Nasser M. Abbasi<br />
020914<br />
This is a diagram to use to generate equations of longitudinal equilibrium.<br />
This distance is called the stick-fixed static margin k m = (h n − h) ¯c Must be positive for static stability<br />
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