|
[Sponsors] |
June 25, 2000, 17:58 |
Coordinates of NACA airfoils
|
#1 |
Guest
Posts: n/a
|
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 |
|
June 26, 2000, 09:58 |
Re: Coordinates of NACA airfoils
|
#2 |
Guest
Posts: n/a
|
"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 |
|
June 27, 2000, 02:38 |
Re: Coordinates of NACA airfoils
|
#3 |
Guest
Posts: n/a
|
Check the "Resources/References/Airfoils" section of this web-site. There are several links there to airfoil-sites with coordinate databases etc.
|
|
June 30, 2000, 11:43 |
Re: Coordinates of NACA airfoils
|
#4 |
Guest
Posts: n/a
|
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. |
|
January 16, 2012, 02:08 |
Naca 66012 airfoil cordinates
|
#5 |
New Member
SANTOSH
Join Date: Jan 2012
Posts: 10
Rep Power: 14 |
Can anybody tell me how to get naca 66012 airfoil coordinates database ,which should have more than 50 points
|
|
January 16, 2012, 08:54 |
|
#6 | |
Senior Member
Ryne Whitehill
Join Date: Aug 2009
Posts: 312
Rep Power: 18 |
Quote:
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" |
||
January 16, 2012, 09:14 |
thanks a lot
|
#7 |
New Member
SANTOSH
Join Date: Jan 2012
Posts: 10
Rep Power: 14 |
To : rwryne
thank you very much |
|
April 18, 2012, 07:38 |
problem in prism layer
|
#8 |
New Member
SANTOSH
Join Date: Jan 2012
Posts: 10
Rep Power: 14 |
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 |
|
April 19, 2012, 01:21 |
|
#9 |
Senior Member
Mehdi Baba Mehdi
Join Date: Jan 2011
Posts: 158
Rep Power: 15 |
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 |
|
April 19, 2012, 03:47 |
|
#10 | |
New Member
Saikrishna
Join Date: Feb 2011
Location: India
Posts: 5
Rep Power: 15 |
Quote:
hope these attachments will give u the coordinates |
||
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
NACA profile coordinates | ken87 | FloEFD, FloWorks & FloTHERM | 1 | March 9, 2011 18:38 |
MOdelling a 3-D structure of a fan blade using NACA airfoils | ashu.feb28 | Main CFD Forum | 0 | February 2, 2010 10:19 |
Drag coefficient of NACA airfoils | L3munoz | Main CFD Forum | 3 | April 23, 2009 11:52 |
Where to find airfoils with more coordinates pts? | KB | Main CFD Forum | 2 | March 23, 2008 23:18 |
NACA Airfoils | Igor | Main CFD Forum | 3 | December 5, 2001 01:35 |