Unsteady Aero at High AoA in Subsonic Flow Jens Nitzsche
NACA0012 Unsteady lift w.r.t. pitch (2-d RANS)
NACA0012 α =17.00 ° Re=10 6
Normalized vorticity integrated in wall- normal direction γ TE =0 still holds in separated flow
Quasi- steady
Quasi- steady
Quasi- steady
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