Design criteria and CFD analysis of a small wind turbine installed at Banihal top in snow bound high altitude area: A case study

G. Kumar, Rakesh Kumar Aggrawal, Amod Kumar
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引用次数: 5

Abstract

To explore wind energy in high altitude Himalayan region a small wind turbine of 10 kW capacity is installed at the altitude of 2900 m at Banihal top (Jammu and Kashmir, India). Wind data from 1997 to 2007 are analysed to evaluate the capacity of wind power at the site. The design wind speed 14 m/sec is found with 2.5 Weibull k-factor. The hump of the ridge line is considered for installation of wind turbine. Computational fluid dynamics (CFD) analysis of the wind profile is carried out for the DEM of the area to obtain optimum height 8m of wind turbine tower. The standard IEC 61400-2 is adopted for designing S-special class small wind turbine for average rated wind speed 14 m/s. The wind turbine blade is selected after considering its fatigue and permissible bending stress at extreme wind speed of 35 m/sec at the site during 1997-2007. CFD analysis at different wind speed and angle of attack is carried out on the selected blade airfoil NACA 23015 for their optimum value. Lift and drag force coefficients are analyzed at various velocity and angle of attack with the help of ANSYS Fluent software. The cut-in speed of wind is decreased from 3.5m/s to 3.0 m/s by changing the angle of attack from 14° to 16° and by increasing effective swept area with special attachment to the hub. It helped to increase the efficiency and performance of wind turbine at low wind velocity without changing the blade profile and its length.
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高海拔地区Banihal顶部小型风力涡轮机的设计标准与CFD分析:一个案例研究
为了在高海拔的喜马拉雅地区探索风能,在海拔2900米的Banihal顶部(印度查谟和克什米尔)安装了一个容量为10千瓦的小型风力涡轮机。分析了1997年至2007年的风力数据,以评估该站点的风力发电能力。设计风速为14 m/s,威布尔系数为2.5。考虑在脊线的驼峰处安装风力发电机。对该区域的DEM进行了风廓线计算流体力学(CFD)分析,以获得风电塔的最佳高度8m。s -特殊级小型风力机的设计采用IEC 61400-2标准,平均额定风速为14 m/s。风机叶片的选择考虑了1997-2007年现场极限风速35米/秒下的疲劳和允许弯曲应力。对选定的叶片翼型NACA 23015进行了不同风速和迎角下的CFD分析,得到了它们的最优值。利用ANSYS Fluent软件对不同速度和迎角下的升力和阻力系数进行了分析。通过将迎角从14°改变为16°,并在轮毂上加装特殊附件,增加有效掠面积,将截风速度从3.5m/s降低到3.0 m/s。在不改变叶片型线和叶片长度的情况下,提高了风力机在低风速下的效率和性能。
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