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Maximum drag enhancement asymptote in spanwise-rotating viscoelastic plane Couette flow of dilute polymeric solutions

Published online by Cambridge University Press:  01 March 2023

Yabiao Zhu
Affiliation:
Department of Modern Mechanics, University of Science and Technology of China, Hefei, Anhui 230026, PR China Yangzhou Collaborative Innovation Research Institute, Shenyang ADRI, Yangzhou, Jiangsu 225000, PR China
Zhenhua Wan
Affiliation:
Department of Modern Mechanics, University of Science and Technology of China, Hefei, Anhui 230026, PR China
Fenghui Lin
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

The existence of a maximum drag enhancement (MDE) asymptote at high rotation ($Ro$) and Weissenberg ($Wi$) numbers in turbulent viscoelastic spanwise-rotating plane Couette flow has been demonstrated. Specifically, it is shown that above a critical $Wi$, drag enhancement plateaus and the MDE asymptote is realized in a broad range of $Ro$. The mean velocity profiles at MDE appear to closely follow a log-law profile that has a nearly identical slope but different intercepts as a function of $Ro$. Much like the maximum drag reduction (MDR) asymptote, the logarithmic function in MDE is closely followed if the mean velocity is plotted using the traditional inner variable scaling; however, the logarithmic function is not well defined when examined by the indicator function. Hence, in this study, we have used the logarithmic fit as a visual guide for the mean velocity profile. Last and perhaps the most intriguing finding of this study is that MDE occurs in the elasto-inertial turbulence (EIT) flow state; hence, it is mainly sustained by elastic forces much like the MDR flow state. To that end, a universal picture of elastically induced drag modification asymptotes is emerging, namely these asymptotic states are an inherent property of the elastically sustained EIT flow state.

Information

Type
JFM Papers
Copyright
© The Author(s), 2023. Published by Cambridge University Press
Figure 0

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

Figure 1

Figure 2. (a) Frictional Reynolds number $Re_\tau =\rho u_\tau h/\eta _t$ versus $Wi$ at various $Ro$ with $u_\tau =\sqrt {\tau _w/\rho }$ being the frictional velocity and $\tau _w$ the total wall stress (the sum of viscous stress and polymer stress). Here, DE is evaluated as $(Re_\tau ^2-Re_{{\tau }0}^2)/Re_{{\tau }0}^2$, where $Re_{\tau 0}$ is the frictional Reynolds number of the Newtonian flow. (b) Log plot of mean velocity profile $\langle u^+ \rangle$ in the lower half of the channel for each $Ro$ versus wall-normal distance $y^+$ at $Wi=0, 5, 10, 20, 40, 60, 80, 100$, where $\langle \ \rangle$ denotes the ensemble average. Here, $\langle u^+ \rangle \equiv \langle (u+U_w)^+ \rangle$, and hereafter $\langle u^+ \rangle =\kappa _K^{-1}\ln {y^+}+B$ with $\kappa _K=0.85$ is plotted as a visual guide. The square of the correlation coefficients $R^2$ between the simulation results and the linear fitting curves for $Ro=0.3, 0.4, 0.7$ at $Wi=100$ are obtained, respectively, as $R^2\approx 0.993, 0.995, 0.991$.

Figure 2

Figure 3. Indicator function $\zeta =y^{+}\langle u^+ \rangle /{{\rm d} y}^{+}$ typically used to indicate logarithmic dependence of the mean velocity profile: (a) $Ro=0.3$; (b) $Ro=0.4$; (c) $Ro=0.7$.

Figure 3

Figure 4. Instantaneous vortical structures of $Re=1300, Ro=0.7$ identified by the $Q$ criterion with $Q=0.2$ and coloured as a function of distance from the lower wall. The upper and lower plots are the full and front ($x$-direction) views, respectively. (a) Newtonian; (b) $Wi=40$; (c) $Wi=60$; (d) $Wi=100$.

Figure 4

Figure 5. The root-mean-square value of streamwise vorticity fluctuation for $Wi=0, 5, 10, 20, 40, 60, 80, 100$ at (a) $Ro=0.3$, (b) $Ro=0.4$ and (c) $Ro=0.7$.

Figure 5

Figure 6. The volume-averaged Reynolds stress (red lines) and polymer stress (blue lines) for $Ro=0.3, 0.4, 0.7$ calculated as $J^u_R=({1}/{2h}){{\int }_{-h}^h}{\langle -u'v'\rangle }\,{{\rm d} y}$ and $J^u_p=({1}/{2h}){{\int }_{-h}^h}{\langle (({1-\beta })/{Re})\tau _{xy}^p\rangle }\,{{\rm d} y}$, respectively (Zhu et al.2020, 2022), where $\boldsymbol {u}'=\boldsymbol {u}-\langle \boldsymbol {u}\rangle$.

Figure 6

Figure 7. Energy exchange between turbulent motions and polymer chains denoted by $-P^t_{p}=-\langle {\tau ^{p}_{ik}}'(\partial {u'_i} / \partial {x_k})\rangle$ for $Ro=0.7$ (Zhu et al.2020, 2022).

Figure 7

Figure 8. (a) Frictional Reynolds number $Re_\tau$ versus $Wi$ at $Re=1300, Ro=0.7, Sc=0.15, 0.31, 0.51, 1.30$. (b) Volume-averaged Reynolds stress (red lines and symbols) and polymer stress (blue lines and symbols) for $Ro=0.7$ at various $Sc$.

Figure 8

Figure 9. Log plot of mean velocity profile $\langle u^+ \rangle$ for $Re=1300$, $Ro=0.7$ and $Wi=0, 5, 10, 20, 40, 60, 100$ versus wall-normal distance $y^+$ at (a) $Sc=0.31$, (b) $Sc=0.51$ and (c) $Sc=1.30$. The square of the correlation coefficient $R^2$ of the log law of $\langle u^+ \rangle$ fitted for $Wi=100$ is obtained as $R^2=0.999$, 0.998 and 0.997 for (a–c), respectively.

Figure 9

Figure 10. (a) Frictional Reynolds number $Re_\tau$ versus $Wi$ at $Re=1300, 2600, 3900$ and $Ro=0.7$ and (b) the corresponding logarithmic-like mean velocity profile $\langle u^+ \rangle$ versus wall-normal distance $y^+$ at various $Wi$. For the log law of $\langle u^+ \rangle$ fitted at $Wi=60$, $R^2$ is obtained as 0.991 and 0.998 for $Re=2600$ and 3900, respectively.

Figure 10

Figure 11. Prototypical instantaneous snapshots of vortical structures at $Re=3900, Ro=0.7$ identified by the $Q$ criterion with $Q=0.2$ and coloured as a function distance from the lower wall. The upper and lower plots are the full and front ($x$-direction) views, respectively. (a) Newtonian; (b) $Wi=20$; (c) $Wi=40$; (d) $Wi=60$.