Open Access

ARTICLE

Computational Modelling of Control of Laminar Separation Bubble over an Airfoil Using an Integrated Tubercle and Vortex Generator

Mustafa Özden^1,2,3, Sinem Keskin^1,4, Eren Anıl Sezer^1,4,5, Muhammed Hatem^1,4, Mustafa Serdar Genç^1,5,*, Halil Hakan Açıkel¹

1 Wind Engineering and Aerodynamic Research Laboratory, Department of Energy Systems Engineering, Erciyes University, Kayseri, Turkey
2 Scientific Research Projects Unit of Erciyes University, Erciyes University, Kayseri, Turkey
3 Dominion Energy Innovation Center, Clemson University, North Charleston, SC, USA
4 Graduate School of Natural and Applied Science, Erciyes University, Kayseri, Türkiye
5 MSG Teknoloji Ltd. Şti, Erciyes Teknopark Tekno-1 Binası, 61/20, Kayseri, Türkiye

* Corresponding Author: Mustafa Serdar Genç. Email:

(This article belongs to the Special Issue: Modeling and Applications of Bubble and Droplet in Engineering and Sciences)

Computer Modeling in Engineering & Sciences 2026, 146(2), 13 https://doi.org/10.32604/cmes.2026.074675

Received 15 October 2025; Accepted 26 January 2026; Issue published 26 February 2026

Abstract

This paper examines a model that combines vortex generators and leading-edge tubercles for controlling the laminar separation bubble (LSB) over an airfoil at low Reynolds numbers (Re). This new concept of passive flow control technique utilizing a tubercle and vortex generator (VG) close to the leading edge was analyzed numerically for a NACA0015 airfoil. In this study, the Shear Stress Transport (SST) turbulence model was employed in the numerical modelling. Numerical modelling was completed using the ANSYS-Fluent 18.2 solver. Analyses were conducted to investigate the flow pattern and understand the underlying LSB control phenomena that enabled the new passive flow control method to provide this significant performance benefit. The findings indicated that the new concept of passive flow control technique suppressed the formation of an LSB at the suction surface of the NACA0015 airfoil, resulting in a higher lift coefficient and improved aerodynamic performance. Improvements in LSB dynamics and aerodynamic performance through the passive flow control method lead to increased energy output and enhanced stability.

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