Carmen published a paper on her doctoral research on wall-modeling in the AIAA Journal. Unlike typical wall models, Carmen’s approach avoids the need to query the interior solution by utilizing solution information solely at the boundary, making it well-suited for unstructured grids and mesh adaptation. Furthermore, it is formulated to lessen the near-wall grid resolution requirements by, below the log layer, making the eddy viscosity approach a constant, nonzero value and the velocity varying approximately linearly with distance from the wall. The image shows the lift vs angle of attack for a Joukowski airfoil comparing the WMRANS to RANS showing excellent ability to match RANS even at stall. This past summer, Carmen presented the model at the AIAA Aviation conference. And, here’s a link to her dissertation which also includes results for WMLES and DES.