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The
Palos
R/C
Flying
Club
The M.A.C. Calculator
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The form shown below
will calculate the percentage of the Mean Aerodynamic Cord (%MAC) of a model
airplane wing for a given position of the CG. If you would like to know the
position of the Center of Gravity(CG) as measured from the leading edge of
the Root Cord, you should use the form on The Center of
Gravity Page.
The Equations
| C |
= (S(A+2B)) /
(3(A+B)) |
| MAC |
= A-(2(A-B)(0.5A+B) /
(3(A+B))) |
| d |
= (2Y(0.5A+B)) /
(3(A+B)) |
|
%MAC
B.P.
|
= ((CG-C) /
MAC)*100 |
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Al
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The Palos R/C Flying Club. All Rights Reserved.
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