|August 20, 2002, 09:41||
ONERA M6 Wing DATA
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
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