The turbulent rotating-disk boundary layer

被引:13
|
作者
Imayama, Shintaro [1 ]
Lingwood, R. J. [1 ,2 ]
Alfredsson, P. Henrik [1 ]
机构
[1] Royal Inst Technol, KTH Mech, Linne FLOW Ctr, S-10044 Stockholm, Sweden
[2] Univ Cambridge, Cambridge CB23 8AQ, England
基金
瑞典研究理事会;
关键词
Near-wall turbulence; Hot-wire anemometer; Skin friction; ABSOLUTE INSTABILITY; SECONDARY INSTABILITY; FLOW; TRANSITION; VORTICES; LAMINAR; FLUID;
D O I
10.1016/j.euromechflu.2014.03.009
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The turbulent boundary layer on a rotating disk is studied with the aim of giving a statistical description of the azimuthal velocity field and to compare it with the streamwise velocity of a turbulent two-dimensional flat-plate boundary layer. Determining the friction velocity accurately is particularly challenging and here this is done through direct measurement of the velocity distribution close to the rotating disk in the very thin viscous sublayer using hot-wire anemometry. Compared with other flow cases, the rotating-disk flow has the advantage that the highest relative velocity with respect to a stationary hot wire is at the wall itself, thereby limiting the effect of heat conduction to the wall from the hot-wire probe. Experimental results of mean, rms, skewness and flatness as well as spectral information are provided. Comparison with the two-dimensional boundary layer shows that turbulence statistics are similar in the inner region, although the rms-level is lower and the maximum spectral content is found at smaller wavelengths for the rotating case. These features both indicate that the outer flow structures are less influential in the inner region for the rotating case. (C) 2014 Elsevier Masson SAS. All rights reserved.
引用
收藏
页码:245 / 253
页数:9
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