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Coordinates of NACA airfoils

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Old   June 25, 2000, 17:58
Default Coordinates of NACA airfoils
  #1
Mohammad
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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
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Old   June 26, 2000, 09:58
Default Re: Coordinates of NACA airfoils
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Alton Reich, PE
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"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
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Old   June 27, 2000, 02:38
Default Re: Coordinates of NACA airfoils
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Jonas Larsson
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Check the "Resources/References/Airfoils" section of this web-site. There are several links there to airfoil-sites with coordinate databases etc.
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Old   June 30, 2000, 11:43
Default Re: Coordinates of NACA airfoils
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Carlos Hannover
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Hello Mohammad, I think I have the coordinates of 0012 (I donŽt 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 IŽll let you know.

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Old   January 16, 2012, 03:08
Default Naca 66012 airfoil cordinates
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Can anybody tell me how to get naca 66012 airfoil coordinates database ,which should have more than 50 points
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Old   January 16, 2012, 09:54
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Ryne Whitehill
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Quote:
Originally Posted by dnsantosh View Post
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"
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Old   January 16, 2012, 10:14
Default thanks a lot
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To : rwryne
thank you very much
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Old   April 18, 2012, 07:38
Default problem in prism layer
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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
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Old   April 19, 2012, 01:21
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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
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E-mail: mb.pejvak[at]Gmail[dot]com
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Old   April 19, 2012, 03:47
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YSV Saikrishna
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Quote:
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
Attached Files
File Type: zip n0012.zip (931 Bytes, 28 views)
File Type: zip naca2412.zip (323 Bytes, 22 views)
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