| Issue |
EPJ Web Conf.
Volume 355, 2026
4th International Conference on Sustainable Technologies and Advances in Automation, Aerospace and Robotics (STAAAR 2025)
|
|
|---|---|---|
| Article Number | 04003 | |
| Number of page(s) | 13 | |
| Section | Thermofluids, Aerodynamics and CFD Simulation | |
| DOI | https://doi.org/10.1051/epjconf/202635504003 | |
| Published online | 03 March 2026 | |
https://doi.org/10.1051/epjconf/202635504003
Numerical Study of the Flow Around the S818-NR Aerodynamic Profile Based on Modern Turbulence Models
1 Institute of Mechanics and Seismic Stability of Structures named after M.T. Urazbaev, Tashkent, Uzbekistan
2 Bukhara State University, Bukhara, Uzbekistan
3 Oriental University, Tashkent, Uzbekistan
* Corresponding author: This email address is being protected from spambots. You need JavaScript enabled to view it.
Published online: 3 March 2026
Abstract
This study examines the subsonic airflow around a S818-NR air foil at angles of attack from 0° to 20° through numerical simulation. The calculations were done in COMSOL Multiphysics using the finite element method. The Shear Stress Transport (SST) model was used to accurately capture the complicated nature of turbulence. We got numerical results for important aerodynamic parameters like lift coefficient, pressure distribution, and velocity components. A comparative analysis of various Reynolds numbers was performed to assess their impact on the flow structure. The simulation results were very similar to the experimental data, which showed that the chosen turbulence model and numerical method were reliable. The data collected help us better understand how turbulent flow works around aerodynamic profiles, and they can be used to design and improve wind turbines.
© The Authors, published by EDP Sciences, 2026
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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