NACA 63-520M airfoil

laltenburg · March 3, 2016, 12:01

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, 11:31

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, 12:01	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?

Thread Tools	Search this Thread
Show Printable Version Email this Page	Search this Thread: Advanced Search
Display Modes
Linear Mode Switch to Hybrid Mode Switch to Threaded Mode

Similar Threads
Thread	Thread Starter	Forum	Replies	Last Post
SU2 AOA optimization	454514566@qq.com	SU2	9	March 7, 2022 16:17
Ffd_control_point_2d	feiyi	SU2	4	September 30, 2019 12:42
High drag for airfoil compared to XFOIL and wind tunnel data	Ry10	SU2	15	October 30, 2016 17:27
2D FFD Optimization	RLangtry	SU2	2	August 5, 2014 09:48
Problem with restart solution in shape_optimization.py	robyTKD	SU2 Shape Design	21	May 29, 2013 09:26