ONERA M6 Wing DATA
 

Hello,

Does anyone have electronic data of C_p at various cross-sections for the ONERA M6 Wing under the following condition.

M_infinity = .837, Re_c_infinity = 11.7 million Alpha = 6.06 degrees.

I have already completed the test case with alpha 3.06 and would now like to do the seperated flow.

Thank You, Kevin