xollat
Aerospace
- Aug 11, 2011
- 5
I have a old drawing with he following nomenclature for an NACA airfoil
NACA 64(9.5)8
Can some one tee]ll me how to interprete the number in parantheses?
In additio the the NACA airfoild I have the leading and traling edge raduis, the corde lenght the setting angle and a sketch of the profile showing the location of maximum camber (x,y location for the leading edge)
Noone in the company know how to recreate the profile
Tank you
NACA 64(9.5)8
Can some one tee]ll me how to interprete the number in parantheses?
In additio the the NACA airfoild I have the leading and traling edge raduis, the corde lenght the setting angle and a sketch of the profile showing the location of maximum camber (x,y location for the leading edge)
Noone in the company know how to recreate the profile
Tank you