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
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