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unsteady-aerodynamics

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aero-dynamic-stall-sam

Dynamic-stall prediction on a helicopter retreating blade (NACA 0012) using UNISTALL — a reduced-order Unified Indicial–Beddoes State-Space (UIBS) solver — validated against NASA static and dynamic-stall experiments. Full geometry→mesh→solve→validate pipeline with plots, drawings, and technical report.

  • Updated Sep 1, 2026
  • Python

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