Dynamic-stall prediction on a helicopter retreating blade (NACA 0012) using UNISTALL — a reduced-order Unified Indicial–Beddoes State-Space (UIBS) solver — calibrated to a published static polar and validated against held-out NASA dynamic-stall experiments. Full geometry→mesh→solve→validate pipeline with plots, drawings, and technical report.
python helicopter scientific-computing computational-fluid-dynamics aerodynamics airfoil aerospace-engineering aeroelasticity rotor-blade rotorcraft unsteady-aerodynamics dynamic-stall naca0012 reduced-order-model beddoes-leishman stall-flutter
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Updated
Sep 9, 2026 - Python