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-   -   Coordinates of NACA airfoils (http://www.cfd-online.com/Forums/main/2286-coordinates-naca-airfoils.html)

Mohammad June 25, 2000 17:58

Coordinates of NACA airfoils
 
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

Alton Reich, PE June 26, 2000 09:58

Re: Coordinates of NACA airfoils
 
"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

Jonas Larsson June 27, 2000 02:38

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

Carlos Hannover June 30, 2000 11:43

Re: Coordinates of NACA airfoils
 
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.


dnsantosh January 16, 2012 03:08

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

rwryne January 16, 2012 09:54

Quote:

Originally Posted by dnsantosh (Post 339466)
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 January 16, 2012 10:14

thanks a lot
 
To : rwryne
thank you very much

dnsantosh April 18, 2012 07:38

problem in prism layer
 
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 April 19, 2012 01:21

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 April 19, 2012 03:47

2 Attachment(s)
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 :)


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