首页> 外文会议>World Renewable Energy Congress >Blade Element Momentum Theory and CFD Modeling as a Tool for Optimizing Wind Turbine Blade Design
【24h】

Blade Element Momentum Theory and CFD Modeling as a Tool for Optimizing Wind Turbine Blade Design

机译:刀片元素动量理论和CFD建模作为优化风力涡轮机叶片设计的工具

获取原文
获取外文期刊封面目录资料

摘要

The present chapter focuses on the comparison of the capabilities of Blade Element Momentum Theory (BEMT) in relation to computational fluid dynamics (CFD) modeling as a tool for the design and performance optimization of a horizontal axial wind turbine (HAWT). A generated blade is examined in different scales by BEMT with the use of the QBlade software. The same wind turbine blade design was then incorporated in a detailed 3D CFD model (in ANSYS CFX). Computations were performed and the results were compared to the ones produced with the BEMT method. For the CFD modeling, a National Advisory Committee for Aeronautics (NACA) profile was initially validated through a two-dimensional analysis and flow field investigation regarding lift and drag coefficients for a variety of angles of attack (AoA). For computation reasons, a rotating domain was applied. The domain is discretized into 4,320,733 elements, most of which are tetrahedral, creating 781,582 nodes. An extra inflation layer is used on the turbine boundary and mesh density is higher in that vicinity. After the validation of the two-dimensional analysis, the wind turbine blade design was incorporated in a detailed 3D CFD model and computations were performed and compared to the ones of the BEMT method. Detailed transition formulas were applied and compared and a mesh independent solution was achieved. Furthermore, pressure and velocity distribution on the blade are analyzed and Cp graphs were produced. The shear stress transport (SST) turbulence model capability to simulate the flow around an airfoil in the pro stall region was verified, while, the angle of attack at which stall begins could also be predicted using CFD modeling. The study revealed the superior performance and advantages of CFD modeling in relation to BEMT since CFD can take into account the 3D effects of actual flow around a turbine blade which cannot be obtained by BEMT methodology.
机译:本章重点的叶片元件动量理论(BEMT)的能力相对于计算流体动力学(CFD)建模为对于水平轴风力涡轮机(HAWT)的设计和性能优化的工具的比较。所产生的叶片在不同的尺度由BEMT与使用QBlade软件的检查。然后将相同的风力涡轮机叶片的设计是在一个详细的3D CFD模型并入(以ANSYS CFX)。进行计算,并将结果进行比较,以与BEMT方法生产的那些。对于CFD模拟,国家航空咨询委员会(NACA)的个人资料通过关于为各种攻击(AOA)的角度的升力和阻力系数的二维分析和流场调查初步验证。为了计算的原因,旋转域应用。域离散为4320733层的元件,其中大部分是四面体,创造781582个节点。一个额外膨胀层被用来在涡轮机的边界上和网眼密度是在那附近高。二维分析的验证之后,风力涡轮机叶片的设计在详细的3D CFD模型被合并并进行和比较,BEMT方法的那些计算。详细过渡式施加和比较并获得一个网状独立的解决方案。此外,压力和速度分布在叶片上进行了分析和的Cp图表是生产。剪切应力传输(SST)湍流模型的能力,以模拟在亲失速区域周围的翼面的流动进行了验证,同时,攻击的失速开始的角度还可以使用CFD模拟预测。该研究显示在相对于所述BEMT优越的性能和CFD模拟的优点,因为CFD能够考虑周围不能由BEMT方法来获得一个涡轮机叶片的实际流量的3D效果。

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