Articles | Volume 7, issue 3
https://doi.org/10.5194/wes-7-967-2022
https://doi.org/10.5194/wes-7-967-2022
Research article
 | 
10 May 2022
Research article |  | 10 May 2022

Investigation into boundary layer transition using wall-resolved large-eddy simulations and modeled inflow turbulence

Brandon Arthur Lobo, Alois Peter Schaffarczyk, and Michael Breuer

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Cited articles

Abu-Ghannam, B. J. and Shaw, R.: Natural transition of boundary layers – The effects of turbulence, pressure gradient, and flow history, J. Mech. Eng. Sci., 22, 213–228, https://doi.org/10.1243/JMES_JOUR_1980_022_043_02, 1980. a
Andersson, P., Brandt, L., Bottaro, A., and Henningson, D. S.: On the breakdown of boundary layer streaks, J. Fluid Mech., 428, 29–60, https://doi.org/10.1017/s0022112000002421, 2001. a, b, c, d
Asada, K. and Kawai, S.: Large-eddy simulation of airfoil flow near stall condition at Reynolds number 2.1×106, Phys. Fluids, 30, 1139–1145, 2018. a, b
Asai, M., Minagawa, M., and Nishioka, M.: The instability and breakdown of a near-wall low-speed streak, J. Fluid Mech., 455, 289–314, https://doi.org/10.1017/S0022112001007431, 2002. a
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Short summary
This research involves studying the flow around the section of a wind turbine blade, albeit at a lower Reynolds number or flow speed, using wall-resolved large-eddy simulations, a form of computer simulation that resolves the important scales of the flow. Among the many interesting results, it is shown that the energy entering the boundary layer around the airfoil or section of the blade is proportional to the square of the incoming flow turbulence intensity.
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