Performance analysis of the airfoil-slat arrangements for hydro and wind turbine applications
Standard airfoils historically used for wind and hydrokinetic turbines had maximum lift coefficients of around 1.3 at stall angles of attack, which is about 12°. At these conditions, the minimum flow velocities to generate electric power were about 7 m/s and 2 m/s for the wind turbine and the hydrok...
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Published in: | Renewable energy Vol. 74; pp. 414 - 421 |
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Abstract | Standard airfoils historically used for wind and hydrokinetic turbines had maximum lift coefficients of around 1.3 at stall angles of attack, which is about 12°. At these conditions, the minimum flow velocities to generate electric power were about 7 m/s and 2 m/s for the wind turbine and the hydrokinetic turbine cases, respectively. In this study, NACA4412-NACA6411 slat–airfoil arrangement was chosen for these two cases in order to investigate the potential performance improvements. Aerodynamic performances of these cases were both numerically and experimentally investigated. The 2D and 3D numerical analysis software were used and the optimum geometric and flow conditions leading to the maximum power coefficient or the maximum lift to drag ratio were obtained. The maximum lift to drag ratio of 24.16 was obtained at the optimum geometric and flow parameters. The maximum power coefficient of 0.506 and the maximum torque were determined at the tip speed ratios of 5.5 and 4.0 respectively. The experimental work conducted in a towing tank gave the power coefficient to be 0.47 which is about %7 lower than the numerical results obtained. Hence, there is reasonable agreement between numerical end experimental values. It may be concluded that slat-hydrofoil or airfoil arrangements may be applied in the design of wind and hydrokinetic turbines for electrical power generation in lower wind velocities (3–4 m/s) and current velocities (about 1 m/s).
•The study was considered the performance characteristics of the slat arrangements.•The 3D flow CFD and experimental analyses were applied on the systems.•Torque, pressure, turbulence intensity values in different λ values were acquired. |
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AbstractList | Standard airfoils historically used for wind and hydrokinetic turbines had maximum lift coefficients of around 1.3 at stall angles of attack, which is about 12 degree . At these conditions, the minimum flow velocities to generate electric power were about 7 m/s and 2 m/s for the wind turbine and the hydrokinetic turbine cases, respectively. In this study, NACA4412-NACA6411 slat-airfoil arrangement was chosen for these two cases in order to investigate the potential performance improvements. Aerodynamic performances of these cases were both numerically and experimentally investigated. The 2D and 3D numerical analysis software were used and the optimum geometric and flow conditions leading to the maximum power coefficient or the maximum lift to drag ratio were obtained. The maximum lift to drag ratio of 24.16 was obtained at the optimum geometric and flow parameters. The maximum power coefficient of 0.506 and the maximum torque were determined at the tip speed ratios of 5.5 and 4.0 respectively. The experimental work conducted in a towing tank gave the power coefficient to be 0.47 which is about %7 lower than the numerical results obtained. Hence, there is reasonable agreement between numerical end experimental values. It may be concluded that slat-hydrofoil or airfoil arrangements may be applied in the design of wind and hydrokinetic turbines for electrical power generation in lower wind velocities (3-4 m/s) and current velocities (about 1 m/s). Standard airfoils historically used for wind and hydrokinetic turbines had maximum lift coefficients of around 1.3 at stall angles of attack, which is about 12°. At these conditions, the minimum flow velocities to generate electric power were about 7 m/s and 2 m/s for the wind turbine and the hydrokinetic turbine cases, respectively. In this study, NACA4412-NACA6411 slat–airfoil arrangement was chosen for these two cases in order to investigate the potential performance improvements. Aerodynamic performances of these cases were both numerically and experimentally investigated. The 2D and 3D numerical analysis software were used and the optimum geometric and flow conditions leading to the maximum power coefficient or the maximum lift to drag ratio were obtained. The maximum lift to drag ratio of 24.16 was obtained at the optimum geometric and flow parameters. The maximum power coefficient of 0.506 and the maximum torque were determined at the tip speed ratios of 5.5 and 4.0 respectively. The experimental work conducted in a towing tank gave the power coefficient to be 0.47 which is about %7 lower than the numerical results obtained. Hence, there is reasonable agreement between numerical end experimental values. It may be concluded that slat-hydrofoil or airfoil arrangements may be applied in the design of wind and hydrokinetic turbines for electrical power generation in lower wind velocities (3–4 m/s) and current velocities (about 1 m/s). •The study was considered the performance characteristics of the slat arrangements.•The 3D flow CFD and experimental analyses were applied on the systems.•Torque, pressure, turbulence intensity values in different λ values were acquired. |
Author | Koç, E. Balas, C. Kılkış, B. Erol, Ö. Aydemir, T. Yavuz, T. |
Author_xml | – sequence: 1 givenname: T. surname: Yavuz fullname: Yavuz, T. email: tyavuz@baskent.edu.tr organization: Baskent University, Department of Mechanical Engineering, Ankara, Turkey – sequence: 2 givenname: E. surname: Koç fullname: Koç, E. organization: Baskent University, Department of Mechanical Engineering, Ankara, Turkey – sequence: 3 givenname: B. surname: Kılkış fullname: Kılkış, B. organization: Baskent University, Department of Mechanical Engineering, Ankara, Turkey – sequence: 4 givenname: Ö. surname: Erol fullname: Erol, Ö. organization: Baskent University, Department of Mechanical Engineering, Ankara, Turkey – sequence: 5 givenname: C. surname: Balas fullname: Balas, C. organization: Gazi University, Faculty of Engineering, Ankara, Turkey – sequence: 6 givenname: T. surname: Aydemir fullname: Aydemir, T. organization: Gazi University, Faculty of Engineering, Ankara, Turkey |
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Cites_doi | 10.1016/j.enconman.2012.01.032 10.1115/1.483261 10.1243/09544100JAERO434 10.2514/3.44192 10.1016/j.renene.2011.08.017 10.2514/3.59049 10.2514/3.60268 10.1017/S0022112059000015 |
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Keywords | Hydrokinetic turbine Towing tank Wind turbine Tip speed ratio Hydrofoil-slat arrangement |
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fullname: Jo – year: 2011 ident: 10.1016/j.renene.2014.08.049_bib14 contributor: fullname: Yavuz – year: 1999 ident: 10.1016/j.renene.2014.08.049_bib24 article-title: Horizontal axis wind turbine aerodynamics: three-dimensional, unsteady, and separated flow influences contributor: fullname: Robinson – year: 2009 ident: 10.1016/j.renene.2014.08.049_bib1 article-title: Hydrodynamic optimization method and design code for stall-regulated hydrokinetic turbine rotors contributor: fullname: Sale – year: 1928 ident: 10.1016/j.renene.2014.08.049_bib7 contributor: fullname: Prandtl |
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Snippet | Standard airfoils historically used for wind and hydrokinetic turbines had maximum lift coefficients of around 1.3 at stall angles of attack, which is about... Standard airfoils historically used for wind and hydrokinetic turbines had maximum lift coefficients of around 1.3 at stall angles of attack, which is about 12... |
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SubjectTerms | Airfoils Drag Electric power generation Hydrofoil-slat arrangement Hydrokinetic turbine Lift Mathematical models Maximum power Tip speed ratio Towing tank Turbines Wind turbine Wind turbines |
Title | Performance analysis of the airfoil-slat arrangements for hydro and wind turbine applications |
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