Flow visualization and skin friction determination in transitional channel flow
Flow visualization and skin friction determination in transitional channel flow
复制标题
过渡通道流动中的流动可视化和表面摩擦力测定
DOI:
10.1007/s00348-020-03102-6
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发表时间:
2021
影响因子:
2.4
通讯作者:
M.
中科院分区:
文献类型:
--
作者:
Yimprasert;S.;Kvick;M.;Alfredsson;P.H.;Matsubara;M.
AbstractThe present study experimentally determines the transitional Reynolds number range for plane channel flow and characterizes its transitional state. The pressure along the channel is measured to determine the skin friction coefficient as function of Reynolds number from the laminar state, through the transitional region into the fully turbulent state. The flow structure was studied through flow visualisation which shows that as the Reynolds number increases from the laminar state the transitional region starts showing randomly occurring turbulent spots. With increasing Reynolds number the spots shift into oblique patches and bands of small scale turbulence that form across the channel width, together with large-scale streaky structures found in areas between the turbulent regions. An image analysing technique was used to determine the intermittency factor, i.e. the turbulence fraction in the flow, as function of Reynolds number. It is found that the skin friction coefficient reaches its turbulent value before the flow is fully turbulent (the intermittency factor is still below one). This suggests that the observed streaky structures in non-turbulent regions contribute to the enhancement of the wall-normal transfer of momentum. Also above the Reynolds numbers where the turbulent skin friction coefficient has been established large-scale features consisting of irregular streaky structures are found. They have an oblique shape similar to the non-turbulent and turbulent patches in the transitional flow indicating that the transition process is not fully complete even above the Reynolds number where the skin friction reaches its turbulent level.Graphic abstractProcessing of flow visualization images to determine the turbulence intermittency in the transitional region. Flow is from left to right, (a) unprocessed, (b) filtered (c) standard deviation of (b), (d) binary picture
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影响因子:
1.5
作者:
E. Zanoun;H. Nagib;F. Durst
通讯作者:
E. Zanoun;H. Nagib;F. Durst
影响因子:
2.4
作者:
Durst, F;Kikura, H;Ye, Q
通讯作者:
Ye, Q
DOI:
10.1299/jsmeicjwsf.2013.4._1222-1_
发表时间:
2013
期刊:
--
影响因子:
--
作者:
Matsubara Masaharu;Miyazaki Makoto;Watanabe Kenta;Kvick Mathias;L. Fredrik;S. Daniel
通讯作者:
S. Daniel
DOI:
10.1016/j.ijheatfluidflow.2016.11.009
发表时间:
2016
影响因子:
2.6
作者:
M. Matsubara;Shun Horii;Y. Sagawa;Y. Takahashi;Daisuke Saito
通讯作者:
Daisuke Saito
影响因子:
4.6
作者:
Schultz, M. P.;Flack, K. A.
通讯作者:
Flack, K. A.