Two-dimensional (2D) flow past airfoils
These benchmark cases employ a RANS modeling framework and serve as validation and verification of the 1-eq Gamma Transition Model. They include the following airfoils and flow parameters:
NASA NLF(1)-0416 airfoil at M=0.1, Re=4M, Tu=0.15%
TU Delft DU00-W-212 airfoil at M=0.1, Re=3M, Tu=0.0864%
A paper is currently in draft containing these results.