Experimental data for NACA 0012
 

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