Articles | Volume 11, issue 1
https://doi.org/10.5194/wes-11-127-2026
https://doi.org/10.5194/wes-11-127-2026
Research article
 | 
15 Jan 2026
Research article |  | 15 Jan 2026

Modelling vortex generator effects on turbulent boundary layers with integral boundary layer equations

Abhratej Sahoo, Akshay Koodly Ravishankara, Wei Yu, Daniele Ragni, and Carlos Simao Ferreira

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Vortex generator design for unsteady flow separation control and dynamic stall suppression on pitching thick airfoils
Abhratej Sahoo, Wei Yu, and Daniele Ragni
Wind Energ. Sci. Discuss., https://doi.org/10.5194/wes-2026-7,https://doi.org/10.5194/wes-2026-7, 2026
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Cited articles

Aparicio, M., Martín, R., Muñoz, A., and González, A.: Results of a parametric study of flow devices, guidelines for design, AVATAR project: WP3, 2015. a
Bak, C., Skrzypiński, W., Gaunaa, M., Villanueva, H., Brønnum, N. F., and Kruse, E. K.: Full scale wind turbine test of vortex generators mounted on the entire blade, Journal of Physics: Conference Series, 753, 022001, https://doi.org/10.1088/1742-6596/753/2/022001, 2016. a
Baldacchino, D., Ragni, D., Simao Ferreira, C., and van Bussel, G.: Towards integral boundary layer modelling of vane-type vortex generators, in: 45th AIAA Fluid Dynamics Conference, American Institute of Aeronautics and Astronautics, Reston, Virginia, p. 3345, ISBN 978-1-62410-362-9, https://doi.org/10.2514/6.2015-3345, 2015. a, b
Baldacchino, D., Ferreira, C., Tavernier, D. D., Timmer, W., and van Bussel, G. J. W.: Experimental parameter study for passive vortex generators on a 30 % thick airfoil, Wind Energy, 21, 745–765, https://doi.org/10.1002/we.2191, 2018. a, b, c, d, e, f, g, h, i, j
Bardina, J., Huang, P., Coakley, T., Bardina, J., Huang, P., and Coakley, T.: Turbulence modeling validation, in: 28th Fluid Dynamics Conference, p. 2121, American Institute of Aeronautics and Astronautics, Reston, Virigina, https://doi.org/10.2514/6.1997-2121, 1997. a
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Short summary
A new model incorporates vortex generator (VG) effects into fast aerodynamic tools like XFOIL and RFOIL. It modifies boundary layer equations and uses empirical functions scaled with VG geometry and Reynolds numbers to implement the modified integral boundary layer equations in RFOIL. The model improves accuracy across airfoils and predicts separation delay, stall delay, lift increase, and added drag, enabling VG effects to be included in wind turbine blade design.
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