期刊文献+

利用双参数非线性拟合求解湍流边界层壁面摩擦速度 被引量:2

Determination of Wall Friction Velocity of the Turbulent Boundary Layer by Two-Parameter Nonlinear Curve Fitting
下载PDF
导出
摘要 热线风速仪是流场测量的基本手段,广泛应用于湍流研究。在低速风洞中用绊线和粗糙带获得充分发展的湍流边界层流动,利用IFA-300恒温热线风速仪测量了湍流边界层不同流向站位的时均速度型。以湍流边界层的无量纲速度型模型White Law为目标曲线,分析了通过速度型拟合反推壁面摩擦速度方法的应用问题,编制了关于双参数壁面坐标理论零点位置y0和壁面摩擦速度uτ的非线性曲线拟合MATLAB程序。以实验测量的测点速度为原始拟合数据,讨论了初始搜索区间和搜索步长、拟合数据范围对拟合结果的影响,并最终求解得到y0和uτ。研究结果表明:所提方法编程思路简单,容易实现,合理选取用于曲线拟合的测点速度数据范围,利用该方法可以求得较高精度的壁面摩擦速度值。 Hot-wire anemometer is a fundamental tool for flow field measurement,and has been widely adopted in research of turbulent flow.A turbulent boundary layer was generated by a trip wire and a piece of sandpaper in the low-speed wind tunnel,and the time-averaged velocity profiles at three different streamwise stations in the boundary layer were measured with IFA-300 constant temperature anemometer.Targeting the dimensionless velocity profile model White Law of the turbulent boundary layer,a nonlinear curve fitting MATLAB program for two parameters,which were theoretical original point of wall coordinate y and wall friction velocity u,was developed.Based on the measured time-averaged velocity profiles,the program was adopted to determine y and u of the three streamwise stations.It is found that the initial search domain and search step size of y and u have no effect on the fitting results if the physical solutions are included in the domain.It is also found that the selected fitting velocities data are closely related to the results.The value of the friction velocity with high precision will be obtained by this nonlinear curve fitting method if the highest fitting velocity data point dose not fall into the wake region.The method given in this paper is simple in programming and reliable in fitting results,and it is of practical to obtain the wall friction velocity of the turbulent boundary layer.
作者 陆连山 李栋 LU Lianshan;LI Dong(School of Aeronautics, Northwestern Polytechnical University, Xi′an 710072, China)
出处 《西北工业大学学报》 EI CAS CSCD 北大核心 2020年第2期253-260,共8页 Journal of Northwestern Polytechnical University
基金 中欧航空科技合作项目(MJ-2015-H-F-106)资助。
关键词 湍流边界层 WHITE Law 无量纲速度型 壁面摩擦速度 非线性拟合 热线风速仪 MATLAB程序 turbulent boundary layer White Law dimensionless velocity profile wall friction velocity nonlinear curve fitting hot-wire anemometer MATLAB program
  • 相关文献

参考文献4

二级参考文献14

共引文献30

同被引文献19

引证文献2

二级引证文献2

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部