Original Research Articles
Parametric Optimisation of the SG6042 Airfoil for Improved Lift-to-Drag Performance of Small Horizontal Axis Wind Turbines at Low Reynolds Numbers
Received 5 Aug 2026, Published online: 5 Aug 2026
Published in Volume 6, Issue 2, 2026, pages 1-8
Muhammad Ramzan Luhur , M. R. L., Sher Muhammad Ghoto, S. M. G., Aijaz Abbasi, A. A., Muhammad Kashif Abbasi, M. K. A., Azhar Hussain Shah, A. H. S., Sajjad Bhangwar, S. B., & Arif Ali Rind, A. A. R. (2026). Parametric Optimisation of the SG6042 Airfoil for Improved Lift-to-Drag Performance of Small Horizontal Axis Wind Turbines at Low Reynolds Numbers. Journal of Magnetism and Its Applications, 6(2), 1-8.
Open access
Abstract
Small horizontal axis wind turbines (HAWTs) operate at chord Reynolds numbers well below those of utility-scale machines, typically between 1×10⁵ and 6×10⁵, where laminar separation raises profile drag and lowers the lift-to-drag ratio of conventional airfoils. This study presents a numerical optimisation of the SG6042 airfoil, a section developed for small wind turbines, with the objective of raising its maximum lift-to-drag ratio (CL/CD) under low Reynolds number conditions. The baseline SG6042 geometry, with 10 percent thickness and 3.75 percent camber, was analysed in QBlade, which couples the XFOIL panel method with blade design routines, and the computed performance was compared with published wind tunnel data. Eighteen modified profiles were then generated by varying maximum thickness from 5 to 9 percent of chord and maximum camber from 5 to 9 percent of chord, and each profile was analysed at Reynolds numbers from 1×10⁵ to 6×10⁵ over an incremental sweep of angle of attack. All modified profiles outperformed the baseline. Peak efficiency moved to lower angles of attack as Reynolds number increased, from 5.5 to 6 degrees at Re = 1×10⁵ to 3 to 3.5 degrees at Re = 5×10⁵ and 6×10⁵. The best three sections, SG6042M5-7, SG6042M5-8 and SG6042M5-9, combine 5 percent thickness with 7 to 9 percent camber and reached maximum CL/CD values of 178.25, 182.41 and 182.40 respectively at 3.5 degrees and Re = 5×10⁵, against 124.10 for the baseline under identical computational settings, an improvement of about 47 percent. The results confirm that reduced thickness combined with raised camber is an effective route to high aerodynamic efficiency for small HAWT blades, subject to structural verification and experimental validation.
Keywords
- low Reynolds number airfoil
- SG6042
- small horizontal axis wind turbine
- lift-to-drag ratio
- QBlade
- thickness-to-camber ratio
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© 2026 Journal of Magnetism and Its Applications. This article is published under CC BY 4.0.
How to cite
Muhammad Ramzan Luhur , M. R. L., Sher Muhammad Ghoto, S. M. G., Aijaz Abbasi, A. A., Muhammad Kashif Abbasi, M. K. A., Azhar Hussain Shah, A. H. S., Sajjad Bhangwar, S. B., & Arif Ali Rind, A. A. R. (2026). Parametric Optimisation of the SG6042 Airfoil for Improved Lift-to-Drag Performance of Small Horizontal Axis Wind Turbines at Low Reynolds Numbers. Journal of Magnetism and Its Applications, 6(2), 1-8.