User:Eas4200c.f08.wiki.d/HW3

{| class="toccolours collapsible collapsed" style="width:100%" ! MATLAB Code

NACA 2415 Airfoil in MATLAB command window
EDU>> Airfoil(2,4,15,.5,[0 0 0])

A_bar =

0.0253

EDU>> Airfoil(2,4,15,.5,[0 0.19 0.01])

A_bar =

0.0255

EDU>> Airfoil(2,4,15,.5,[0 0.25 -1])

A_bar =

0.0256


 * }