Hi:

I need to know the upper and lower coordinates of the NACA airfoils, say 0012 and 2412. That is to make some benchmarking on them. I wonder if you know where I can find such an info please let me know.

Thanks. Mohammad

"Theory of Wing Sections" by Abbott and Von Doenhoff (ISBN 486-60586-8) has profiles for many NACA airfoils in it. It's an old book, but you may be able to find a copy at your local large college library.

Alton

Check the "Resources/References/Airfoils" section of this web-site. There are several links there to airfoil-sites with coordinate databases etc.

Hello Mohammad, I think I have the coordinates of 0012 (I don´t remember if 2412 also) in my computer, if you are still interested send me an e-mail

hanngal@yahoo.com

I can not remember which was the site where i found them, but as soon as I remember it I´ll let you know.

[dnsantosh]

Can anybody tell me how to get naca 66012 airfoil coordinates database ,which should have more than 50 points

[rwryne]

Originally Posted by dnsantosh

Can anybody tell me how to get naca 66012 airfoil coordinates database ,which should have more than 50 points

I think it is safe to make your own thread when this one is 11+ years old!

Anyways:

http://www.mh-aerotools.de/airfoils/javafoil.htm

1) go to that site above

2) click "The Applet"

3) Change the pulldown menu to NACA 6-digit

4) change "thickness location" to 60 and hit Create Airfoil

5) might want to use the "Modify NACA section to have a closed trailing edge"

[dnsantosh]

To : rwryne
thank you very much

[dnsantosh]

hi
am trying to generate prism on bwb with 10mm thick prism. geometry has V shape in trailing edge with 73degree angle and side lengths ( 80mm, 65mm) ,wen i generate the prisms using icem cfd ,it generating penetrating elements in between V,, any solution to avoid this problem

thanks

[mb.pejvak]

I uploaded all airfoil coordinates that I have in my PC and everyone can download it in this site:

http://www.4shared.com/rar/-nPRSVWM/coord.html

[saikrishna12]

Originally Posted by Mohammad
;9326

Hi:

I need to know the upper and lower coordinates of the NACA airfoils, say 0012 and 2412. That is to make some benchmarking on them. I wonder if you know where I can find such an info please let me know.

Thanks. Mohammad

@mohammad

hope these attachments will give u the coordinates