|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
|Thread||Thread Starter||Forum||Replies||Last Post|
|M6 ONERA Wing profile||Cyril A.||Main CFD Forum||17||June 30, 2013 09:47|
|Looking for data of ONERA M6 wing||Chih-Hao Chang||Main CFD Forum||2||May 29, 2009 11:49|
|Postprocessing Pressure data spanwise over a wing||Rick||FLUENT||1||February 3, 2006 10:28|
|How to update polyPatchbs localPoints||liu||OpenFOAM Running, Solving & CFD||6||December 30, 2005 18:27|
|Onera Wing Wall function?||Dianhong||Main CFD Forum||0||November 21, 2003 21:19|