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NACA profile coordinates

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Old   March 9, 2011, 13:24
Default NACA profile coordinates
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koay kheng kean
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Hi, anyone know where to get a correct NACA 0012 coordinates? i have generate the coordinates by using JavaFoil software but when i run the simulation by using cosmofloworks i cannot get the same result (lift and drag coefficient against AOA) as the software provided....pls help...thanks..
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Old   March 9, 2011, 19:38
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Travis Carrigan
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The best option would be to write your own code. For symmetric NACA 4-series airfoils it's pretty straightforward. See the Wikipedia article below for the equations.

http://en.wikipedia.org/wiki/NACA_airfoil

Or you could always visit the UIUC airfoil database. There are tons of airfoil coordinates available.

http://www.ae.illinois.edu/m-selig/a..._database.html
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