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#1 |
New Member
Shubham jhamb
Join Date: Jan 2018
Posts: 3
Rep Power: 8 ![]() |
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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