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Hammam March 24, 2007 09:18
analyzing NACA 0012 airfoil
 
Hi everybody! i would like to analyze the NACA 0012 airfoil to determine the lift and drag coefficients at different angle of attack by using cfx. can you please tell me the steps required to achieve that.

thanks M.Hammam.

nor May 2, 2007 05:19
Re: analyzing NACA 0012 airfoil
 
Hello I am an aerospace engeneering and want to NACA 0012 airfoil codes to determine the pressure,lift and drag coefficients at different angle of attack by using cfx. thanks N.Tohidi

Santiago Orrego May 3, 2007 12:07
Re: analyzing NACA 0012 airfoil
 
What do you mean with "codes" ??

The (x,y) coordinates that define the contour of the airfoil?

Santiago.

Gert-Jan May 3, 2007 12:17
Re: analyzing NACA 0012 airfoil
 
This is really breaking news.

Good luck, Gert-Jan

Dr. FLow Squad May 7, 2007 04:47
Re: analyzing NACA 0012 airfoil
 
Choose "The Applet" on http://www.mh-aerotools.de/airfoils/javafoil.htm to run JAVAFOIL. Why bother with CFD...

tohidi May 14, 2007 10:30
Re: analyzing NACA 0012 airfoil
 
Hello I require analyzing NACA 0012 airfoil. Thanks


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