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October 27, 2021, 07:43 |
Cp and x/c for Turbulent NACA 0012
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#1 |
New Member
robert landis
Join Date: Oct 2021
Posts: 1
Rep Power: 0 |
Hi everyone,
I am trying to replicate the results seen here https://su2code.github.io/tutorials/...lent_NACA0012/ I have SU2 version 7.0.2. Installed, ran fine. I was able to view the pressure map on Paraview. How do I get the Cp vs x/c plot though? I read the output format here https://su2code.github.io/docs_v7/Custom-Output/ to say OUTPUT_FILES= (RESTART, TECPLOT_ASCII, SURFACE_TECPLOT_ASCII) Then reran the simulation, and now I have surface_flow.dat, and flow.dat, I can read the Pressure_Coefficient from this file, but what is it plotted against? Thanks, |
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October 28, 2021, 14:21 |
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#2 |
Senior Member
bigfoot
Join Date: Dec 2011
Location: Netherlands
Posts: 676
Rep Power: 21 |
I always use PARAVIEW_MULTIBLOCK, which gives the boundaries as separate entities. You can then do an Extract Block to select only the naca profile wall boundary. You can then select the Plot Data filter to visualize only the data on the surface as a function of x-coordinate.
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tutorials |
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