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NREL Phase Ⅵ 수평축 풍력터빈의 공력특성에 관한 수치적 연구

A Numerical Study on the Aerodynamic Characteristics for a HAWT of NREL Phase Ⅵ

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초록

The purpose of this work is to compare and analyze computed results with experimental data of NREL (National Renewable Energy Laboratory) Phase Ⅵ for the whole operating conditions of various wind speeds using    turbulence model provided in the commercial code, FLUENT. Performance results such as power coefficient, shaft torque, pressure coefficient show a good agreement with experimental data. But, root bending moment is over-predicted than the experimentally measured value by about 30% for the whole operating conditions because of indefinite measurement reference. Nevertheless, these results qualitatively show a good tendency in the aspect of aerodynamic performance. As wind speed increases, streamlines on the surface of blade show more and more complex pattern.

Abstract

The purpose of this work is to compare and analyze computed results with experimental data of NREL (National Renewable Energy Laboratory) Phase Ⅵ for the whole operating conditions of various wind speeds using    turbulence model provided in the commercial code, FLUENT. Performance results such as power coefficient, shaft torque, pressure coefficient show a good agreement with experimental data. But, root bending moment is over-predicted than the experimentally measured value by about 30% for the whole operating conditions because of indefinite measurement reference. Nevertheless, these results qualitatively show a good tendency in the aspect of aerodynamic performance. As wind speed increases, streamlines on the surface of blade show more and more complex pattern.

참고문헌 (8)

  1. 저풍속형 풍력발전기 핵심기술 개발(Ⅰ), , 공공기술연구회, ~ (2007)
  2. 중대형 풍력발전 시스템의 성능평가 기반 및 기술기준 확보, , 산업자원부, ~ (2007)
  3. 김범석, "CFD에 의한 NREL Phase Ⅵ 풍력터빈 성능 해석", 제5회 유체공학학술대회 (2008)
  4. 김범석, "수평축 풍력발전용 터빈 블레이드 최적설계 및 공력성능해석에 관한 연구", 박사, pp.2005
  5. NREL unsteady aerodynamics experiment in the NASA-Ames wind tunnel: A comparison of predictions to measurements, "D. Simms", NREL, ~, pp.TP-500-29494 (2001)
  6. F. R. Menter, "Two-equation eddy-viscosity turbulence models for engineering applications", AIAA Journal, 32(8), pp.1598~1605 (1994)
  7. P. H. Cook, "Aerofoil RAE 2822 Pressure Distributions, and Boundary Layer and Wake Measurements", AGARD AR, 138(A6) (1979)
  8. Calculation of flowfield around an airfoil with spoiler, "H. Ok", AIAA, ~, pp.Paper 93-0527 (1993)

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