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February 12, 1999, 11:46
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NACA 6A-series airfoil data
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Guest
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I'am trying to test a 2D potential flow code over NACA airfoils, but I don't have analytical solutions nor any experimental data of the airfoil ordinates and the corresponding pressure distribution, if anyone can provide me with these data or knows where I can find them I'll be very gratful.
Thanks. |
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February 12, 1999, 13:35
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Re: NACA 6A-series airfoil data
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Guest
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Start at http://amber.aae.uiuc.edu/~m-selig/ads.html and good luck. Note NVFoil there, it might be useful.
If all you need is to check a potential flow solver, why NACA airfoils? Joukowskii will do just as well. |
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February 15, 1999, 05:25
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Re: NACA 6A-series airfoil data
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hi Shereef, I've done some simulation on 3D-code upon the NACA65 ... Profile. If you can use my results please let me know.
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