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Explore CFD studies structured around the question, inputs, method, metrics, results, and recommendation behind an engineering decision.

Spanwise-vorticity visualization showing the separated shear layer, near-wake vortices, and downstream vortex street around the pitching NACA 0012 airfoil.
Unsteady AerodynamicsPlanned internal demonstration case

NACA 0012 Pitching-Oscillation CFD Study

An unsteady CFD demonstration for resolving aerodynamic hysteresis, phase lag, and dynamic-stall development on a harmonically pitching airfoil.

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