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February 26, 2014, 09:58 |
Experimental data for NACA 0012
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New Member
Manuel
Join Date: Feb 2014
Posts: 2
Rep Power: 0 |
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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