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Boundary Layer Thickness Extraction

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Old   July 25, 2019, 12:07
Default Boundary Layer Thickness Extraction
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Shubham jhamb
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Hey!
I am using SU2 as a tool to analyze flow over an airfoil in supersonic regime. I wanted to compute the boundary layer thickness over the airfoil. I presume it changes over the entire blade surface due to the contouring of the airfoil.

Is there any way I can calculate the boundary layer thickness over the airfoil using TecPlot and flow.dat from the simulation?

Any insight will be helpful.

Thanks!
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