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SAL P51 Mustang Airfoil

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Avio

Member
Joined
Sep 28, 2011
Messages
10
Location
Bologna
Hello everybody,
I would realize my dream "SAL P-51 Mustang" and I decided to start to build the horizzontal stabilizer.
I would drawing by AUTOCAD each airfoil but I have a problem.

On the drawing there is write that the airfoil is 63(2)-015 MOD that is NACA MODIFIED!

I understand from the drawing that maximum thickness is 13.4% at 30% of the chord but the naca 63(2)-015 have maximum thickness is 15% at 35%!!

Someone could help me to found this Airfoil or understand How to realize this?

Thanks a lot to all

Alberto
 
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