Computational And Experimental Study of Spanwise Synthetic Jet Flow Control
Fluid Dynamics
2024-12-11 v1
Abstract
This study investigates the reattachment of flow on a stalled NACA 0025 airfoil with an array of circular synthetic jet actuators. Experimental flow visualizations are used to assess the spanwise control authority of the array and the three-dimensionality of the flow. Numerical simulations provide insights into the flow structures created by the actuation, and how they evolve with different parameters.
Keywords
Cite
@article{arxiv.2412.07726,
title = {Computational And Experimental Study of Spanwise Synthetic Jet Flow Control},
author = {Howard Ho and Adnan Machado and Pierre Sullivan},
journal= {arXiv preprint arXiv:2412.07726},
year = {2024}
}
Comments
5 pages, 7 figures, conference