Year: 2024
Type: article
Abstract: Dynamic stall at low Reynolds numbers, $Re \sim O(10^4)$ , exhibits complex flow physics with co-existing laminar, transitional and turbulent flow regions. Current state-of-the-art stall onset criteria use parameters that rely on flow properties integrated around the leading edge. These include the leading edge suction parameter or $LESP$ (Ramesh et al. , J. Fluid Mech. , vol. 751, 2014, pp. 500–538) and boundary enstrophy flux or $BEF$ (Sudharsan et al. , J. Fluid Mech. , vol. 935, 2022, A10), which have been found to be effective for predicting stall onset at moderate to high $Re$ . However, low- $Re$ flows feature strong vortex-shedding events occurring across the entire airfoil surface, including regions away from the leading edge, altering the flow field and influencing the onset of stall. In the present work, the ability of these stall criteria to effectively capture and localize these vortex shedding events in space and time is investigated. High-resolution large-eddy simulations for an SD7003 airfoil undergoing a constant-rate, pitch-up motion at two $Re$ (10 000 and 60 000) and two pitch rates reveal a rich variety of unsteady flow phenomena, including instabilities, transition, vortex formation, merging and shedding, which are described in detail. While stall onset is reflected in both $LESP$ and $BEF$ , local vortex-shedding events are identified only by the $BEF$ . Therefore, $BEF$ can be used to identify both dynamic stall onset and local vortex-shedding events in space and time.
Source: Journal of Fluid Mechanics
DOI: 10.1017/jfm.2024.753
Authors: Sarasija Sudharsan, Anupam Sharma
Institution: Iowa State University
Language: English
Subfield: Computational Mechanics
Field: Engineering
Domain: Physical Sciences
Open Access status: hybrid
Estimated APC paid: $3,450
OpenAlex ID: W4402876160