SU2 V3.2 questions

hedley · June 19, 2014, 10:57

1. If I download from Github for Linux the compiler says Ver 3.1 not Ver 3.2 ??
2. Running the x64 Bit binaries on windows I do not know if these were built for single or multi core . ??

hlk · August 10, 2014, 00:49

1. the version number was a typo
2. For parallel operation, please follow the installation instructions for installing from source with parallel.

hedley · August 10, 2014, 01:35

Thanks HLK . I have put this on the backburner for a while after realizing the importance of meshing and also no end to end tutorials from mesh creating to generation and interpretation of results in paraview . Most importantly it seems as if CFD is not yet there when it comes to analyzing turbulent flow at or near the stall . My original mission was to visualise the onset of tip stalling so I could modify the wing to reduce this behavior so perhaps in a few years the tech will improve . For now I will have to tuft and flight test on each iteration . So " back to the future "

June 19, 2014, 10:57	SU2 V3.2 questions	#1
hedley Member Hedley Join Date: May 2014 Posts: 52 Rep Power: 12	1. If I download from Github for Linux the compiler says Ver 3.1 not Ver 3.2 ?? 2. Running the x64 Bit binaries on windows I do not know if these were built for single or multi core . ??

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August 10, 2014, 00:49		#2
hlk Senior Member Heather Kline Join Date: Jun 2013 Posts: 309 Rep Power: 14	1. the version number was a typo 2. For parallel operation, please follow the installation instructions for installing from source with parallel.

August 10, 2014, 01:35		#3
hedley Member Hedley Join Date: May 2014 Posts: 52 Rep Power: 12	Thanks HLK . I have put this on the backburner for a while after realizing the importance of meshing and also no end to end tutorials from mesh creating to generation and interpretation of results in paraview . Most importantly it seems as if CFD is not yet there when it comes to analyzing turbulent flow at or near the stall . My original mission was to visualise the onset of tip stalling so I could modify the wing to reduce this behavior so perhaps in a few years the tech will improve . For now I will have to tuft and flight test on each iteration . So " back to the future "