Spectral-error based implicit large-eddy simulation (SE-ILES) of Dassault Aviation's V2C laminar-flow wing section (unswept, aspect ratio = 1) at Re=500,000 and M=0.7 under buffet conditions. Animation shows contours of the streamwise pressure gradient and the green sonic line (M=1). Details about this simulation can be found in our corresponding paper: Wide domain simulations of flow over an unswept laminar wing section undergoing transonic buffet M. Zauner and N.D. Sandham Submitted to Physical Review Fluids, 2020
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