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Experimental data for NACA 0012

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Old   February 26, 2014, 08:58
Default Experimental data for NACA 0012
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Manuel
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Hi,
does anyone know where to find experimental data (i.e. cp) for the NACA 0012 airfoil at following conditions:

M=0.65
Re=500,000
AOA=2

These are really unusual conditions and therefore it is really hard to find anything. I would be very grateful, if someone has some data, that is nearly at these conditions!

Best regards
Manuel
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