Definition of the NACA 65 on the bladegen
I 'm generating the blade geometry through BLADEGEN software, and in particular I'm studying a compressor fan where the profile of its rotor and stator are NACA 65. Then I want to implement that information on the BLADEGEN, but by using the NACA thickness dialog window I can specify some other parameters. However I can't define the designation on the same window.
Please, let me know as soon as possible.
P.s. You can have look on the attached file
Domenico di Cugno
Although Im sorry i cant answer your question. I'm hoping you can help me. Im still new to ANSYS and I cant seem to find the dialog thickness window. Could you help?
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