• Title/Summary/Keyword: 풍력 터빈 날개 단면

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Viscous Flow Analysis around a Wind Turbine Blade with End Plate and Rake (풍력터빈 날개의 끝판과 레이크 효과에 대한 점성유동장 해석)

  • Kim, Ju-In;Kim, Wu-Joan
    • Journal of the Korean Society for Marine Environment & Energy
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    • v.14 no.4
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    • pp.273-279
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    • 2011
  • Turbulent flow analysis around a wind turbine blade was performed to evaluate the power performance of offshore wind turbine. Fluent package was utilized to solve the Reynolds-averaged Navier-Stokes equations in non-inertial rotating coordinates. The realizable k-$\varepsilon$ model was used for turbulence closure and the grid system combining structured and unstructured grids was generated. In the first, lift and drag forces of 2-D foil section were calculated and compared with existing experimental data for the validation. Then torque and thrust of the wind turbine blade having NACA 4-series sections were calculated with fixed pitch angle and rpm. Tip speed ratio was varied by changing wind speed. In the next, three kinds of end plate were attached at the tip of blade in order to increase the power of the wind turbine. Among them the end plate attached at the suction side of the blade was found to be most effective. Furthermore, performance analysis with tilt angle and rake was also performed.

PREDICTION OF AERODYNAMIC PERFORMANCE LOSS OF A WIND TURBINE BLADE SECTION DUE TO CONTAMINANT ACCUMULATION (외부 오염물 증착에 의한 풍력 터빈 날개 단면의 공력 성능 저하 예측)

  • Yang, T.H.;Choi, J.H.;Yu, D.O.;Kwon, O.J.
    • Journal of computational fluids engineering
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    • v.18 no.1
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    • pp.91-97
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    • 2013
  • In the present study, the effects of contaminant accumulation and surface roughness on the aerodynamic performance of wind turbine blade sections were numerically investigated by using a flow solver based on unstructured meshes. The turbulent flow over the rough surface was modeled by a modified ${\kappa}-{\omega}$ SST turbulence model. The calculations were made for the NREL S809 airfoil with varying contaminant sizes and positions at several angles of attack. It was found that as the contaminant size increases, the degradation of the airfoil performance becomes more significant, and this trend is further amplified near the stall condition. When the contaminant is located at the upper surface near the leading edge, the loss in the aerodynamic performance of the blade section becomes more critical. It was also found that the surface roughness leads to a significant reduction of lift, in addition to increased drag.

Numerical Analysis of Aerodynamics Characteristics of Two-Dimensional Blade Section with Elastic Flap (탄성 플랩을 갖는 2차원 날개 단면 공력 특성 전산해석)

  • Bae, Gi-Seong;Won, Chang-Hui;Lee, Seung-Su
    • Proceeding of EDISON Challenge
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    • 2014.03a
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    • pp.637-642
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    • 2014
  • 선행 연구에서 블레이드 뒷전에 탄성 플랩이 장착되면 받음각에 따라 양력의 증가가 항력의 증가보다 상대적으로 더 커지게 되어 전체적인 양항비(앙력과 항력의 비)가 증가하는 것을 확인하였다. 본 논문에서는 선행의 연구를 참조하여 플랩의 길이가 변함에 따라서 양력과 항력의 변화를 비교하였다. 블레이드의 종류와 플랩의 제원은 현재 이용되는 수직축 풍력 발전기의 제품과 동일하게 사용하였다. EDISON_CFD와 MIDAS_IT를 이용하여 플랩이 장착된 블레이드 주변의 유체 유동을 해석하고, 플랩의 상하변위를 계산하였다. 이 과정을 반복 수행하여 플랩의 거동을 분석하고 플랩의 길이와 받음각에 따른 양항비를 비교하여 이전보다 효율적인 플랩을 설계하였다.

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