...
首页> 外文期刊>International Journal of Renewable Energy Development >The Effects of Different Roughness Configurations on Aerodynamic Performance of Wind Turbine Airfoil and Blade
【24h】

The Effects of Different Roughness Configurations on Aerodynamic Performance of Wind Turbine Airfoil and Blade

机译:不同粗糙度配置对风力机翼型和叶片气动性能的影响

获取原文
           

摘要

In this research, viscous and turbulent flow is simulated numerically on an E387 airfoil as well as on a turbine blade. The main objective of this paper is to investigate various configurations of roughness to find a solution in order to mitigate roughness destructive impacts. Hence, the sand grain roughness is distributed uniformly along pressure side, suction side and both sides during the manufacturing process. Navier-Stokes equations are discretized by the finite volume method and are solved by SIMPLE algorithm. Results indicated that in contrast with previous studies, the roughness will be useful if it is applied on only pressure side of the airfoil. In this condition, the lift coefficient is increased to ?and 1.2% compare to the airfoil with rough and smooth sides, respectively. However, in 3-D simulation, the lift coefficient of the blade with pressure surface roughness is less than smooth blade, but still its destructive impacts are much less than of both surfaces roughness and suction surfaces roughness. Therefore, it can be deduced that in order to reveal the influence of roughness, the simulation must be accomplished in three dimensions. Article History : Received Jun 12 th 2017; Received in revised form August 27 th 2017; Accepted Oct 3 rd 2017; Available online How to Cite This Article : Jafari, K., Djavareshkian, M.H., Feshalami, B.H. (2017) The Effects of Different Roughness Configurations on Aerodynamic Performance of Wind Turbine Airfoil and Blade. International Journal of Renewable Energy Develeopment, 6(3), 273-281. https://doi.org/10.14710/ijred.6.3.273-281
机译:在这项研究中,在E387机翼以及涡轮叶片上对粘性和湍流进行了数值模拟。本文的主要目的是研究粗糙度的各种配置,以找到解决方案,以减轻粗糙度的破坏性影响。因此,在制造过程中,砂粒粗糙度沿压力侧,吸力侧和两侧均匀地分布。 Navier-Stokes方程通过有限体积法离散化,并通过SIMPLE算法求解。结果表明,与以前的研究相反,如果仅在翼型的压力侧施加粗糙度,则它将是有用的。在这种情况下,与具有粗糙和光滑侧面的翼型相比,升力系数分别增加到and和1.2%。然而,在3-D模拟中,具有压力表面粗糙度的叶片升力系数小于光滑叶片,但其破坏性影响仍远小于表面粗糙度和吸力表面粗糙度。因此,可以推断出,为了揭示粗糙度的影响,必须在三个维度上完成仿真。文章历史:于2017年6月12日收到;于2017年8月27日收到修订版; 2017年10月3日接受;在线提供如何引用本文:贾法里(Kafari),达卡列什安(Djavareshkian),麻萨诸塞州(Feshalami) (2017)不同粗糙度配置对风力涡轮机翼型和叶片气动性能的影响。国际可再生​​能源发展杂志,6(3),273-281。 https://doi.org/10.14710/ijred.6.3.273-281

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号