Evolving vortex dynamics around a pitching wing for dynamic stall at a transitional Reynolds number
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
Published online on May 30, 2026
Abstract
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Ahead of Print.
This study investigates the dynamic-stall process over a pitching NACA 0018 wing at a Reynolds number of 160,000 using the detached-eddy simulation (DES) technique and proper orthogonal decomposition (POD). The aim is to employ POD as an energy-ranked ...
This study investigates the dynamic-stall process over a pitching NACA 0018 wing at a Reynolds number of 160,000 using the detached-eddy simulation (DES) technique and proper orthogonal decomposition (POD). The aim is to employ POD as an energy-ranked ...