|July 17, 2016, 13:01||
Transition position evaluation
Join Date: Apr 2013
Posts: 9Rep Power: 5
Hi dear colleagues,
I was searching an open source code that allows laminar to turbulent transition prediction on NACA airfoils. Specifically, I would like to be able to perform Tollmienn Schlichting N factor computations from the CPs over the airfoil.
Does anyone know such an open source code?
Thanks in advance!
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