NACA 63-520M airfoil

laltenburg · March 3, 2016, 13:01

Dear all,

I want to investigate the NACA 63-520M airfoil in Ansys Fluent (chord length = 5 cm). For this investigation I obviously need the coordinates of the airfoil, so I can import them into Ansys. Does anyone know, how to obtain these coordinates?

luna125 · March 30, 2016, 12:31

Quote:

Originally Posted by laltenburg

Dear all,

I want to investigate the NACA 63-520M airfoil in Ansys Fluent (chord length = 5 cm). For this investigation I obviously need the coordinates of the airfoil, so I can import them into Ansys. Does anyone know, how to obtain these coordinates?

i have all of them: luna125@foxmail.com

March 3, 2016, 13:01	NACA 63-520M airfoil	#1
laltenburg New Member Join Date: Jan 2016 Posts: 2 Rep Power: 0	Dear all, I want to investigate the NACA 63-520M airfoil in Ansys Fluent (chord length = 5 cm). For this investigation I obviously need the coordinates of the airfoil, so I can import them into Ansys. Does anyone know, how to obtain these coordinates?

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