2020
DOI: 10.5194/wes-5-1487-2020
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Laminar-turbulent transition characteristics of a 3-D wind turbine rotor blade based on experiments and computations

Abstract: Abstract. Laminar-turbulent transition behavior of a wind turbine blade section is investigated in this study by means of field experiments and 3-D computational fluid dynamics (CFD) rotor simulations. The power spectral density (PSD) integrals of the pressure fluctuations obtained from the high-frequency microphones mounted on a blade section are analyzed to detect laminar-turbulent transition locations from the experiments. The atmospheric boundary layer (ABL) velocities and the turbulence intensities (T.I.)… Show more

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Cited by 9 publications
(5 citation statements)
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“…Wind turbine blade airfoils operate at large Reynolds numbers in highly unsteady conditions (Leishman, 2002), often in a degraded surface state because of soiling and erosion (Sareen et al, 2013). Even over one single rotor revolution, the local turbulent inflow to a blade section can undergo significant changes (Schaffarczyk et al, 2016;Özçakmak et al, 2020;Madsen et al, 2019a). The resulting large disturbances can cause abrupt transitions in otherwise smoothly developing boundary layers, with not yet fully understood consequences (Morkovin, 1985).…”
Section: Physics Unknownsmentioning
confidence: 99%
“…Wind turbine blade airfoils operate at large Reynolds numbers in highly unsteady conditions (Leishman, 2002), often in a degraded surface state because of soiling and erosion (Sareen et al, 2013). Even over one single rotor revolution, the local turbulent inflow to a blade section can undergo significant changes (Schaffarczyk et al, 2016;Özçakmak et al, 2020;Madsen et al, 2019a). The resulting large disturbances can cause abrupt transitions in otherwise smoothly developing boundary layers, with not yet fully understood consequences (Morkovin, 1985).…”
Section: Physics Unknownsmentioning
confidence: 99%
“…The details of the instrumentation and the sampling frequencies are described by Özçakmak et al (2020). Detailed boundary layer transition analyses were performed in subsequent studies (Madsen et al, 2019;Özçakmak et al, 2019, 2020 by analyzing the DAN-AERO data further and conducting CFD simulations for the 2D and the full rotor flow.…”
Section: Dan-aeromentioning
confidence: 99%
“…The effective angle of attack in the simulations is calculated by the annular averaging of the axial velocity method in order to compare the results with the field experiments. The details of this method and how it is implemented can be found in previous studies (Hansen et al, 1997;Özçakmak, 2020).…”
Section: Urans Full Rotor Simulations For Dan-aero Experimentsmentioning
confidence: 99%
“…There are several transition models available (for a review see, e.g., Saric et al, 2003;Langtry et al, 2006;Pasquale et al, 2009;Colonia et al, 2017). Some of these are based on the transport equations, such as the γ (Colonia et al, 2017) and γ −Re equation models (Menter et al, 2006;Langtry et al, 2006;Sørensen, 2009;Menter et al, 2015;Langtry et al, 2015); other ones rely on stability analysis, such as the e N method (Smith and Gamberoni, 1956;van Ingen, 1956).…”
Section: Introductionmentioning
confidence: 99%
“…is the rotation speed, u the mean-flow velocity vector projected in the x 1 -x 2 plane, k = (α, β, 0) the wave vector, and the perturbation propagation angle relative to the outer streamline. Giles, 1987;Özçakmak et al, 2020). This transition model does not account for effects of the blade rotation or the threedimensional flow.…”
Section: Introductionmentioning
confidence: 99%