k-ω SST (shear stress transport) turbulence model calibration: A case study on a small scale horizontal axis wind turbine

被引:144
|
作者
Costa Rocha, P. A. [1 ]
Barbosa Rocha, H. H. [1 ]
Moura Carneiro, F. O. [1 ]
Vieira da Silva, M. E. [2 ]
Valente Bueno, A. [3 ]
机构
[1] Univ Fed Ceara, Dept Mech Engn, Lab Aerodynam & Fluid Mech LAero, BR-60440554 Fortaleza, CE, Brazil
[2] Solar Energy & Nat Gas Lab, BR-60440554 Fortaleza, CE, Brazil
[3] Univ Fed Ceara, Dept Mech Engn, Lab Internal Combust Engines, BR-60440554 Fortaleza, CE, Brazil
关键词
Aerodynamic performance; k-omega SST turbulence model; Model calibration; Small scale HAWT; Wind energy; PART I; BLADE; DESIGN;
D O I
10.1016/j.energy.2013.11.050
中图分类号
O414.1 [热力学];
学科分类号
摘要
This work deals with a computational investigation emphasized on the calibration of a turbulence model regarding to the operational capability of a SS-HAWT (small-scale horizontal axis wind turbine). Experimental field tests were carried out to collect data to evaluate the performance (power) coefficient, C-p, as a function of the tip-speed ratio, lambda. The prototype examined was a three-bladed wind turbine (NACA (National Advisory Committee for Aeronautics) 0012 profile) designed for fixed tip-speed ratio (with lambda = 5), constructed and operated at the Federal University of Ceara. The maximum value experimentally achieved for C-p was about 14%. The k-omega SST (shear stress transport) turbulence model, solved by the open source CFD (computational fluid dynamics) toolbox OpenFOAM (Open Source Field Operation and Manipulation), assessed the wind turbine performance. The experimental data information obtained reporting the aerodynamic performance of the SS-HAWT prototype was required to calibrate the model. The turbulence intensity and the characteristic length were studied in terms of the beta* parameter. The power coefficient numerically predicted tends to agree with the experimental assessment. The variation of beta mainly affects viscous friction over the blades. (C) 2013 Elsevier Ltd. All rights reserved.
引用
收藏
页码:412 / 418
页数:7
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