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Numerical study of the hydrodynamic stability of a wind-turbine airfoil with a laminar separation bubble under free-stream turbulence

Coelho Leite Fava, Thales (författare)
KTH,Strömningsfysik,SeRC - Swedish e-Science Research Centre
Lobo, B. A. (författare)
Mechanical Engineering Department, Kiel University of Applied Sciences 2 , D-24149 Kiel, Germany
Nogueira, P. A. S. (författare)
Aerospace Engineering, Monash University 3 , 3800 Clayton, Australia
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Schaffarczyk, A. P. (författare)
Mechanical Engineering Department, Kiel University of Applied Sciences 2 , D-24149 Kiel, Germany
Breuer, M. (författare)
Professur für Strömungsmechanik, Helmut-Schmidt-Universität Hamburg 4 , D-22043 Hamburg, Germany
Henningson, Dan S. (författare)
KTH,SeRC - Swedish e-Science Research Centre,Strömningsmekanik och Teknisk Akustik
Hanifi, Ardeshir, Docent, 1963- (författare)
KTH,Linné Flow Center, FLOW,SeRC - Swedish e-Science Research Centre,Strömningsmekanik och Teknisk Akustik
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 (creator_code:org_t)
AIP Publishing, 2023
2023
Engelska.
Ingår i: Physics of fluids. - : AIP Publishing. - 1070-6631 .- 1089-7666. ; 35:8
  • Tidskriftsartikel (refereegranskat)
Abstract Ämnesord
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  • The interaction of several instabilities and the influence of free-stream turbulence on laminar-turbulent transition on a 20% thick wind-turbine blade section with a laminar separation bubble (LSB) are investigated with wall-resolved large-eddy simulations (LES). Turbulence intensities (TI) of 0%, 2.2%, 4.5%, 8.6%, and 15.6% at chord Reynolds number 100,000 are considered. Linear receptivity occurs for the most energetic disturbances; high-frequency perturbations are excited via non-linear mechanisms for  TI≥8.6%⁠. Unstable Tollmien–Schlichting (TS) waves appear in the inflectional flow region for  TI≤4.5%⁠, shifting to inviscid Kelvin–Helmholtz (KH) modes upon separation and forming spanwise rolls. Sub-harmonic secondary instability occurs for  TI=0%⁠, with rolls intertwining before transition. Streaks spanwise modulate the rolls and increase their growth rates with TI for  TI≤4.5%⁠, reducing separation and shifting transition upstream. The  TI=4.5% case presents the highest perturbations, leading to the smallest LSB and most upstream transition. Earlier inception of TS/KH modes occurs on low-speed streaks, inducing premature transition. However, for  TI=8.6%⁠, the effect of the streaks is to stabilize the attached mean flow and front part of the LSB. This occurs due to the near-wall momentum deficit alleviation, leading to the transition delay and larger LSB than  TI=4.5%⁠. This also suppresses separation and completely stabilizes TS/KH modes for  TI=15.6%⁠. Linear stability theory predicts well the modal evolution for  TI≤8.6%⁠. Optimal perturbation analysis accurately computes the streak development upstream of the inflectional flow region but indicates higher amplification than LES downstream due to the capture of low-frequency, oblique modal instabilities from the LSB. Only low-amplitude [ O(1%)] streaks displayed exponential growth in the LES since non-linearity precludes the appearance of these modes.

Ämnesord

TEKNIK OCH TEKNOLOGIER  -- Maskinteknik -- Strömningsmekanik och akustik (hsv//swe)
ENGINEERING AND TECHNOLOGY  -- Mechanical Engineering -- Fluid Mechanics and Acoustics (hsv//eng)

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