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Polymer-induced flow relaminarization and drag enhancement in spanwise-rotating plane Couette flow

Published online by Cambridge University Press:  27 October 2020

Yabiao Zhu
Affiliation:
Department of Modern Mechanics, University of Science and Technology of China, Hefei Anhui 230026, PR China
Jiaxing Song
Affiliation:
Department of Modern Mechanics, University of Science and Technology of China, Hefei Anhui 230026, PR China
Nansheng Liu*
Affiliation:
Department of Modern Mechanics, University of Science and Technology of China, Hefei Anhui 230026, PR China
Xiyun Lu
Affiliation:
Department of Modern Mechanics, University of Science and Technology of China, Hefei Anhui 230026, PR China
Bamin Khomami*
Affiliation:
Department of Chemical and Biomolecular Engineering, University of Tennessee, Knoxville, TN 37996, USA
*
†Email addresses for correspondence: lns@ustc.edu.cn, bkhomami@utk.edu
†Email addresses for correspondence: lns@ustc.edu.cn, bkhomami@utk.edu

Abstract

Direct numerical simulation of polymer-induced flow relaminarization of turbulent spanwise-rotating plane Couette flow (RPCF) is reported for the first time. Specifically, the reverse transition pathway from a Newtonian turbulent RPCF to a fully relaminarized drag enhanced viscoelastic flow has been elucidated. Evidently, this transition occurs gradually by weakening and eventual elimination of small-scale vortices as the Weissenberg number ($Wi$) is enhanced, paving the way for a two-dimensional laminar flow consisting of large-scale and highly organized roll cells. The influence of polymer additives on convective momentum exchange by large-scale roll cells and small-scale turbulent vortices, namely, the drag reduction (DR) realized by elimination of turbulent vortices and the significant drag enhancement (DE) that results from polymer roll cell interactions has been identified as the mechanism of DE. The observed vortical changes point to a universal mechanism for the coupling of polymer chains and turbulent vortices in wall-bounded viscoelastic DE and DR flows.

Information

Type
JFM Papers
Copyright
© The Author(s), 2020. Published by Cambridge University Press
Figure 0

Figure 1.Sketch of spanwise-rotating plane Couette flow.

Figure 1

Figure 2.Flow relaminarization pathway visualized by instantaneous vortical structures that are identified by $Q$-criterion and coloured by the $Q$ value (red/blue for positive/negative values). Q is defined as the difference between the magnitudes of fluid rotation and strain. $(a)\, {\rm Newtonian}, Q = \pm 0.5, Re_{\tau} = 106.2; (b)\, Wi = 5, Q = \pm 0.1, Re_{\tau} =114.9,$$DE = 17\,\%; (c)\ Wi = 10, Q = \pm 0.1, Re_{\tau} =117.9, DE = 23\,\%;$$(d)\ Wi = 20, Q = \pm 0.1,$$Re_{\tau} =120, DE\,{=}\,28\,\%; (e)\, Wi\,{=}\,30, Q\,{=}\,\pm 0.1, Re_{\tau}\,{=}\,127.8, DE\,{=}\,45\,\%;$$(f)\, Wi\,{=}\,40, Q\,{=}\,\pm 0.1, Re_{\tau} = 130.5, DE = 51\,\%.$

Figure 2

Figure 3.One-dimensional spectra of (a) the streamwise turbulent kinetic energy ($\langle u'u'\rangle$) at the channel centre and (b) time series of the near-wall streamwise velocity $u$ sampled at $y=0.97h$. Here, the fluctuating part of $u$ is obtained as $u'=u-\langle u\rangle$; $\langle \,\rangle$ denotes hereafter the ensemble averaging.

Figure 3

Figure 4.Instantaneous vortical structures visualized by streamline plots of the velocity vector ($v$, $w$) in the $(y, z)$ plane at $x=L_x/2$ for (a) Newtonian flow, (b) $Wi=5$, (c) $Wi=10$, (d) $Wi=20$, (e) $Wi=30$ and (f) $Wi=40$. The contour patterns are plotted based on the value of polymer stress term $J^u_p$.

Figure 4

Figure 5.(a) Reynolds stress term $J^u_R$ and (b) polymer stress term $J^u_p$.

Figure 5

Figure 6.Reynolds stress decomposed into contributions of (a) roll cells ($J^u_{r}=-\langle {u^r}{v^r}\rangle$) and (b) turbulent vortices ($J^u_{t}=-\langle u''v''\rangle$), as $-{\langle u'v'\rangle }=-{\langle {u^r}{v^r}\rangle }-{\langle u''v''\rangle }$. Here, the variable of the roll cells is defined as $\phi ^r={\langle \phi \rangle }_{x,t}-\langle \phi \rangle$, and that of the turbulent vortices as $\phi ''=\phi -{\langle \phi \rangle }_{x,t}$, with ${\langle \rangle }_{x,t}$ denoting averaging in the $x$-direction and in time (Bech & Andersson 1996; Gai et al.2016; Xia et al.2019).

Figure 6

Figure 7.Turbulent vortices identified by $Q''$ and coloured by the $J^u_t$ value. Here, $Q''$ is calculated by the $Q$-criterion based on the instantaneous fluctuating velocity $(u'',v'',w'')$. The upper and lower plots are the full and front ($x$-direction) views, respectively. $(a)\ {\rm Newtonian}, Q'' = \pm 0.5; (b)\ Wi = 5, Q'' = \pm 0.1; (c)\ Wi = 10, Q'' = \pm 0.1;$$(d)\ Wi = 20, Q'' = \pm 0.1; (e)\ Wi = 30, Q'' = \pm 0.1; (\,f)\ Wi = 40, Q'' = \pm 0.1.$

Figure 7

Figure 8.Energy exchange between turbulent motions and mean flow (a) quantified as $P^t_{m}=-\langle {u''}{v''}\rangle (\textrm {d}\langle u\rangle /\textrm {d}y)$, and that between turbulent motions and polymer chains (b) quantified as $-P^t_{p}=-\langle \tau '_{ik}(\partial {u''_i} / \partial {x_k})\rangle$.

Figure 8

Figure 9.Comparison of (a–d) instantaneous vortical structures identified by $Q$-criterion at different $Sc$ and mesh sizes. The test calculations are performed with mesh size $256\times 129\times 256$ (in the $x\times y\times z$ directions) for $Sc=0.15$ and 0.19, and $512\times 129\times 512$ for $Sc=0.26$ and $Sc=0.38$.

Figure 9

Figure 10.(a) The momentum flux associated with the polymer stress ($J^u_p$) and the Reynolds stress of roll cells ($J^u_r$) and that of turbulent vortices ($J^u_t$) at different $Sc$. (b) The deviation of the maximum value of $J^u_i$ for different $Sc$ from that for $Sc=0.15$, where $i=r, p, t$ for $J^u_r, J^u_p, J^u_t$, respectively.