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Search: Posts Made By: klausb
Forum: OpenFOAM Running, Solving & CFD March 6, 2015, 10:06
Replies: 0
Views: 752
Posted By klausb
komegaSST underprecitcting lift/cl

Hello,

I try to reproduce an airfoil simulation at Re = 1.000.000 which has originally also been done using OpenFoam komegaSST.

Expected vs. achieved cl/cd results are:

expected cl: 1.1401...
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