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analyzing NACA 0012 airfoil

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Old   March 24, 2007, 11:18
Default analyzing NACA 0012 airfoil
  #1
Hammam
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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.
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Old   May 2, 2007, 06:19
Default Re: analyzing NACA 0012 airfoil
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nor
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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
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Old   May 3, 2007, 13:07
Default Re: analyzing NACA 0012 airfoil
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Santiago Orrego
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What do you mean with "codes" ??

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

Santiago.
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Old   May 3, 2007, 13:17
Default Re: analyzing NACA 0012 airfoil
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Gert-Jan
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This is really breaking news.

Good luck, Gert-Jan
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Old   May 7, 2007, 05:47
Default Re: analyzing NACA 0012 airfoil
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Dr. FLow Squad
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Choose "The Applet" on http://www.mh-aerotools.de/airfoils/javafoil.htm to run JAVAFOIL. Why bother with CFD...

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Old   May 14, 2007, 11:30
Default Re: analyzing NACA 0012 airfoil
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tohidi
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Hello I require analyzing NACA 0012 airfoil. Thanks
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