2012
DOI: 10.1080/19942060.2012.11015401
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Numerical Study of Flow Around Iced Wind Turbine Airfoil

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Cited by 31 publications
(24 citation statements)
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“…Villalpando et al [8] evaluated the e ciency of four turbulence models, i.e., Spalart Allmaras, SST k !, RNG k !, and RSM models, to estimate the aerodynamic coe cients. Among these turbulence models, SST k !…”
Section: Governing Equations and Air Ow Simulationsmentioning
confidence: 99%
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“…Villalpando et al [8] evaluated the e ciency of four turbulence models, i.e., Spalart Allmaras, SST k !, RNG k !, and RSM models, to estimate the aerodynamic coe cients. Among these turbulence models, SST k !…”
Section: Governing Equations and Air Ow Simulationsmentioning
confidence: 99%
“…The numerical simulation over a clean and ice-accreted NACA 63-415 airfoil using commercial package FLUENT and SST k ! turbulence model was conducted by Villalpando et al [8]. Li et al [6,17] also investigated the characteristics of surface icing on the wind turbine blades with the NACA0018 and NACA 7715 airfoils.…”
Section: Introductionmentioning
confidence: 99%
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“…Accumulation of ice on the leading edge surfaces of aircraft and wind turbine blades will result in disruption of smooth flow, reduction of lift and increase of drag, stall at much higher speeds than normal, vibrations due to mass imbalance, and damage of aircraft or wind turbine components due to ice shedding [8][9][10].…”
Section: Introductionmentioning
confidence: 99%
“…Dynamic overset grid technology for CFD simulation was presented in Li et al 15 for computation of bodies with relative motions, including elastic deformation. In Villalpando et al, 16 the streamlines around the clean and iced airfoil were analyzed to evaluate the ice impact on lift and drag with the SST k2v model. The performance of a turbine blade with a large leading edge diameter and wedge angle was investigated in Sun et al 17 Yelmule and EswaraRao Anjuri 18 is a case study in which the capability of CFD in predicting complex 3D wind turbine aerodynamics was demonstrated with NREL Phase VI data.…”
Section: Introductionmentioning
confidence: 99%