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Jens Nitzsche NACA0012 Unsteady lift w.r.t. pitch (2-d RANS) - PowerPoint PPT Presentation

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


  1. Unsteady Aero at High AoA in Subsonic Flow Jens Nitzsche

  2. NACA0012 Unsteady lift w.r.t. pitch (2-d RANS)

  3. NACA0012 α =17.00 ° Re=10 6

  4. Normalized vorticity integrated in wall- normal direction γ TE =0 still holds in separated flow

  5. Quasi- steady

  6. Quasi- steady

  7. Quasi- steady

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