2016
DOI: 10.1155/2016/6059741
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Investigation of the Unsteady Flow Behaviour on a Wind Turbine Using a BEM and a RANSE Method

Abstract: Analyses of the unsteady flow behaviour of a 5 MW horizontal-axis wind turbine (HAWT) rotor (Case I) and a rotor with tower (Case II) are carried out using a panel method and a RANSE method. The panel method calculations are obtained by applying the in-house boundary element method (BEM) panMARE code, which is based on the potential flow theory. The BEM is a three-dimensional first-order panel method which can be used for investigating various steady and unsteady flow problems. Viscous flow simulations are car… Show more

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Cited by 4 publications
(15 citation statements)
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“…This is because the blades were disturbed at the suction side close to the tower, which caused the flow velocity to decelerate and eventually increased the pressure. Figure 14A shows that when comparing the simulation results with the data presented by Alesbe et al, 22 the value of Cp significantly differed in the range of 0.18 < x/c < 0.45. Compared with the SST k–ω turbulence model, the realizable k–ε turbulence model used herein slightly underestimated the surface pressure at a high angle of attack ( normalα = 10 °).…”
Section: Resultsmentioning
confidence: 76%
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“…This is because the blades were disturbed at the suction side close to the tower, which caused the flow velocity to decelerate and eventually increased the pressure. Figure 14A shows that when comparing the simulation results with the data presented by Alesbe et al, 22 the value of Cp significantly differed in the range of 0.18 < x/c < 0.45. Compared with the SST k–ω turbulence model, the realizable k–ε turbulence model used herein slightly underestimated the surface pressure at a high angle of attack ( normalα = 10 °).…”
Section: Resultsmentioning
confidence: 76%
“…Due to their limited data, only the case of the wind turbine rotor was adopted for comparison. Although there are rare data showing the distribution of Cp around the wind turbine blade, the numerical data of Alesbe et al 22 at U0 = 11.4 m/s still can be used to compare with our simulation results. The results indicate that the peak values of Cp on the pressure and suction sides of the root generally appeared near the leading edge (where x/c approaches 0), while the values of Cp on both sides were the closest at the root of the blade where x/c = 0.3.…”
Section: Resultsmentioning
confidence: 96%
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“…The rotor was the first example. The rotor with the tower was the second case, which was solved using a panel method and a RANSE method [9]. In 2016, Samal, Ashis Kumar S et al presented a study on how deflection and stress were distributed in a long, thin cantilever bundle with a regular rectangular cross-section and linear and homogenous elastic material characteristics.…”
Section: Introductionmentioning
confidence: 99%