Boundary Layer Thickness Extraction -- CFD Online Discussion Forums

July 25, 2019, 12:07	Boundary Layer Thickness Extraction	#1
Shubham_J 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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