首页> 外文会议>Asia-Pacific Power and Energy Engineering Conference;APPEEC 2009 >Navier-Stocks Computations of Wind-Turbine Airfoil using Low Mach Number Preconditioning
【24h】

Navier-Stocks Computations of Wind-Turbine Airfoil using Low Mach Number Preconditioning

机译:低马赫数预处理的风力机翼型Navier-Stocks计算

获取原文

摘要

Wind turbine airfoil is numerical simulated by using the governing equations of compressible fluids in this paper. The Reynolds averaged Navier-Stokes computations are combined with low Mach preconditioning and implicit matrix-free lower-upper symmetric Gauss-Seidel (LUSGS) iteration on unstructured meshes, and the results are improved at the very low velocity speeds which are representative of the flow field around a wind turbine airfoil. Detailed LUSGS algorithm with preconditioning is present in this paper, which is improved to cost less data storage and computational time for steady flow. The steady and unsteady characteristics of static 2D-S809 airfoil are analyzed by the numerical results and compared between calculations and tests. Aerodynamic coefficients have been got using the algorithm of this work at all angles of attack. The unsteadiness induced separation bubble shedding has been captured by this method finally.
机译:利用可压缩流体的控制方程对风力机翼型进行了数值模拟。雷诺平均Navier-Stokes计算与低Mach预处理和非结构化网格上的无隐含的无矩阵上下对称高斯-赛德尔(LUSGS)迭代相结合,并且在代表流动的极低速度下改善了结果风力涡轮机机翼周围的磁场。本文提出了一种具有预处理功能的详细LUSGS算法,该算法经过改进,可减少数据存储量和稳定流的计算时间。通过数值结果分析了静态2D-S809机翼的稳态和非稳态特性,并在计算和测试之间进行了比较。使用这项工作的算法在所有迎角都获得了空气动力学系数。最终通过这种方法捕获了由不稳定引起的分离气泡脱落。

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