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Polymer-induced flow transitions in turbulent Taylor–Couette flow with co- and counter-rotating cylinders

Published online by Cambridge University Press:  25 May 2026

Jiawei Cui
Affiliation:
Department of Modern Mechanics, University of Science and Technology of China, Hefei, Anhui 230026, PR China
Peng-Jun-Yi Zhang
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
Nan-Sheng Liu
Affiliation:
Department of Modern Mechanics, University of Science and Technology of China, Hefei, Anhui 230026, PR China
Xi-Yun 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
*
Corresponding author: Fenghui Lin, linfh@ustc.edu.cn

Abstract

Direct numerical simulations are performed to elucidate the influence of counter- and co-rotation on turbulent viscoelastic Taylor–Couette flow in the Rossby number range $ \textit{Ro}^{-1}=-0.6$ to $ \textit{Ro}^{-1}=1$. A novel polymer-induced transition pathway is discovered that is fundamentally different from Newtonian flows. In the counter-rotation regime, the neutral surface is elastically modified and separates the turbulent inner-wall region containing chaotic vortices from the relaminarised layer adjacent to the outer cylinder. Strikingly, co-rotation triggers an elasto-rotational instability, which leads to the breakdown of large-scale Taylor vortices into small-scale penetrating structures, thereby preventing the relaminarisation at high co-rotation rates. Examination of turbulence dynamics demonstrates that the structural changes with increasing $ \textit{Ro}^{-1}$ are accompanied by a transition from elasto-inertial to elastically dominated turbulence. Specifically, the polymer stress progressively exceeds the Reynolds stress and monotonically enhances angular momentum transport, which eliminates the optimal transport characteristic found in the Newtonian flow. The elastically dominated nature of the turbulent flow under co-rotation is further corroborated by the more significant elastic production of the turbulent kinetic energy, as well as the monotonic enhancement of the polymer elongation as $ \textit{Ro}^{-1}$ increases. Furthermore, it is indicated that the polymer orientation strongly depends on vortical structures, with enhanced radial alignment occurring in the boundary region between adjacent vortices. This vortex-mediated polymer orientation is crucial for generating substantial polymer shear stress, establishing a direct link between coherent structures and polymer dynamics.

Information

Type
JFM Papers
Copyright
© The Author(s), 2026. Published by Cambridge University Press
Figure 0

Figure 1. Flow regimes in the $ \textit{Re}$–$ \textit{Ro}^{-1}$ parameter space of Newtonian TCF with independently rotating inner and outer cylinders. Here, Lam BL means laminar boundary layer, and UR means ultimate regime. The grey lines, which are adopted from Ostilla et al. (2013), denote the boundaries between different flow states. Only the data points mentioned in the Introduction have been included; readers may refer to Grossmann et al. (2016) for a more comprehensive phase map.

Figure 1

Figure 2. Flow regimes in the $ \textit{Re}$–$ \textit{Ro}^{-1}$ parameter space of viscoelastic TCF with independently rotating inner and outer cylinders. Here, WVF means wavy vortex flow, WVF(h) means wavy vortex flow with higher azimuthal frequency, and DRSW means disordered rotating standing waves.

Figure 2

Figure 3. Schematic of the Taylor–Couette system. Here, $R_i$ and $R_o$ denote the inner and outer cylinder radii, respectively, with $\eta = R_i/R_o$ being the radius ratio and $d = R_o - R_i$ the gap width, $\varOmega _i$ and $\varOmega _o$ are the respective angular velocities, and $L_z$ represents the axial length of the periodic computational domain.

Figure 3

Table 1. The rotation effect considered in this study, which is quantified by the Rossby number $ \textit{Ro}^{-1}$ and covers both counter- and co-rotating regimes. To facilitate comparison with existing studies, the control parameters in the rotating frame of reference have also been expressed as two Reynolds numbers corresponding to the inner and outer cylinders, $ \textit{Re}_{i,o}=\rho R_{i,o}\varOmega _{i,o} d/\eta _t$.

Figure 4

Figure 4. Profiles of root mean square values of $(a)$ three velocity components and $(b)$ the typical polymer stress component $\tau _{\mathit{r\theta }}$ at $ \textit{Ro}^{-1}=0$ with various mesh sizes. Here, $\tilde {r}=(r-R_i)/d$ is the dimensionless distance to the inner cylinder wall.

Figure 5

Figure 5. Time and $\theta$-direction averaged vectors of radial $(\langle u_r\rangle _{\mathit{\theta ,t}})$ and axial $(\langle u_z\rangle _{{\theta ,t}})$ velocities and contour plots of streamwise vorticity $\langle \omega _{\theta }\rangle _{{\theta ,t}}$ in the $(r,z)$ plane for ($a$) viscoelastic and ($b$) Newtonian TCF at various $ \textit{Ro}^{-1}$.

Figure 6

Figure 6. ($a$) Contour plots of the time and $\theta$-direction averaged angular velocity $\langle {\omega }\rangle _{\theta ,t}$, with neutral surface indicated by the black solid line for various $ \textit{Ro}^{-1}$. For a discernible comparison, the left- and right-hand halves are shown for Newtonian and viscoelastic flows, respectively. The red dashed lines shown in the viscoelastic flows correspond to the right-hand side of (3.1). Here, for each specific $ \textit{Ro}^{-1}$, an identical scaling factor for vector length has been applied in both the Newtonian and viscoelastic cases to ensure a fair and meaningful comparison. ($b$) The variation of the axially averaged neutral surface position $\tilde {r}_N$ and the corresponding effective elasticity number $El_{\textit{eff}}$ as a function of $ \textit{Ro}^{-1}$.

Figure 7

Figure 7. Ensemble-averaged radial polymer body force $f_{pr}$ for ($a$) counter-rotating cylinders and ($b$) co-rotating cylinders.

Figure 8

Figure 8. The various production terms in the streamwise enstrophy budget for (a,b) counter-rotating and (c,d) co-rotating outer cylinders. Here, only the near-wall regions, where these production terms are most intense, are shown.

Figure 9

Figure 9. ($a$) Plots of $ \textit{Nu}_{\omega }$ as a function of $ \textit{Ro}^{{-1}}$. Here, $ \textit{Nu}_{\omega }$ is obtained as ${J^{\omega }}/{J^{\omega }_{\textit{lam}}}$, where $J^{\omega }_{\textit{lam}}$ is the laminar value of $J^{\omega }$. Previous DNS results for a Newtonian TCF at the same $ \textit{Re}$ (Ostilla et al.2013) are included for comparison. ($b$) Volume-averaged angular momentum fluxes as a function of $ \textit{Ro}^{-1}$. Here, the volume-averaged values are obtained by the integral across the gap, e.g. $J^{v}_c = (1/d) {\int _{R_i}^{R_o}{J^{\omega }_c}\,{\rm d}r}$ and $J^{v}_p = (1/d) {\int _{R_i}^{R_o}{J^{\omega }_p}\,{\rm d}r}$. (c,d) The balance of angular momentum flux for viscoelastic TCF at two representative values of $ \textit{Ro}^{-1}$: $-0.5$ and $0.83$, respectively.

Figure 10

Figure 10. Ensemble-averaged Reynolds stress $\langle {u'_r{u'_\theta }}\rangle$ and polymer shear stress $-(1-\beta )\langle {\tau _{r\theta }}\rangle /\textit{Re}$ for ($a$) counter-rotation and ($b$) co-rotation. Here, the polymer stress has been rescaled by $(1-\beta )/\textit{Re}$ for a more reasonable comparison with the Reynolds stress.

Figure 11

Figure 11. Rotation-induced modifications in the elastic production $P_{e}$ and the inertial production $P_{t}$ of TKE for $(a)$ counter-rotation and $(b)$ co-rotation.

Figure 12

Figure 12. Rotation-induced modifications in the production of Reynolds stress: ($a$) the Coriolis force term $Co_{r\theta }$, and ($b$) the elastic production term $E_{r\theta }$.

Figure 13

Figure 13. Ensemble-averaged ($a$) polymer chain extension rate $\langle {\text{tr}(\boldsymbol{C})}\rangle /L^{\textrm {2}}$ and its ($b$) azimuthal, ($c$) radial and ($d$) axial components at various $ \textit{Ro}^{-1}$ values. Note that the vertical axis in ($c$) has been adjusted to clearly show the variations in $\langle {C_{\textit{rr}}}\rangle /L^{\textrm {2}}$.

Figure 14

Figure 14. Ensemble-averaged polymer normal stresses: ($a$) $\langle {\tau _{\theta \theta }}\rangle$, ($b$) $\langle {\tau _{\textit{rr}}}\rangle$, ($c$) $\langle {\tau _{zz}}\rangle$ for various $ \textit{Ro}^{-1}$ values. Here, the polymer stress has been rescaled by $(1-\beta )/\textit{Re}$ for a more reasonable comparison with the Reynolds stress.

Figure 15

Figure 15. Snapshots for the alignments between the first principal direction of $\boldsymbol{C}$, denoted as $\boldsymbol{e^{C}}_1$, and the three unit vectors $\boldsymbol{e}_\theta$, $\boldsymbol{e}_r$ and $\boldsymbol{e}_z$. For brevity, the angles between $\boldsymbol{e^{C}}_1$ and $\boldsymbol{e}_\theta$, $\boldsymbol{e}_r$, $\boldsymbol{e}_z$ are represented as $\varphi , \gamma, \psi$, respectively. Here, contours illustrate the cosine values of these angles in (a–c) counter-rotation case $ \textit{Ro}^{-1}=-0.5$, (d–f) ICRO case $ \textit{Ro}^{-1}=0$, and (g–i) co-rotation case $ \textit{Ro}^{-1}=0.83$. The $(r,z)$ plane streamlines are plotted using the $(u_r,u_z)$ velocities. To clearly show the vortex-induced polymer orientation, the visualisation is limited to the axial region $z=1.0{-}2.0$, within which the results are normalised by their respective maximum values to facilitate comparison.

Figure 16

Figure 16. Ensemble-averaged alignments between $\boldsymbol{e^{C}}_1$ and the three unit vectors for various $ \textit{Ro}^{-1}$ values: (a,b) $\langle \cos {\varphi }\rangle$, (c,d) $\langle \cos {\gamma }\rangle$ and (e, f) $\langle \cos {\psi }\rangle$ for (a,c,e) $ \textit{Ro}^{-1} \leqslant 0$ and (b,d, f) $ \textit{Ro}^{-1}\geqslant 0$, thereby highlighting the effect of the outer cylinder’s rotation direction.

Figure 17

Figure 17. The correlation between the polymer shear stress $\tau _{r\theta }$ (contour) and polymer behaviour $\cos \gamma$ (line, the alignment between $\boldsymbol{e^{C}}_{1}$ and $\boldsymbol{e}_{r}$) for $(a)$ counter-rotation case $ \textit{Ro}^{{-1}}={-0.5}$, $(b)$ ICRO case $ \textit{Ro}^{ {-1}}=\textrm {0}$, and $(c)$ co-rotation case $ \textit{Ro}^{{-1}}=\textrm {0.83}$, with dark grey frames marking the regions with large values of $\cos {\gamma }$.

Figure 18

Figure 18. The TKE budget for viscoelastic TCF at $(a)$ counter-rotating $ \textit{Ro}^{{-1}}=-0.5$ and $(b)$ co-rotating $ \textit{Ro}^{{-1}}=0.83$. The inset of $(b)$ depicts the zoom-in of the inner-wall region to clearly show the distributions of each term of the TKE budget.

Figure 19

Figure 19. Reynolds stress budget for viscoelastic TCF at $(a)$ counter-rotating $ \textit{Ro}^{{-1}}=-0.5$ and $(b)$ co-rotating $ \textit{Ro}^{{-1}}=0.83$. The inset of $(b)$ depicts the zoom-in of the inner-wall region to clearly show the variation of various terms.

Figure 20

Figure 20. Two-point autocorrelation functions of $u_r'$ at the middle of the gap ($\tilde {r}=0.5$) in ($a$) the streamwise (azimuthal) and ($b$) the axial directions for $ \textit{Ro}^{-1} \ge 0$. The triangles in ($a$) and ($b$) denote the location of the first minimum, which serves as a measure of the characteristic spatial scales of the coherent structures. ($c$) The variation of the identified streamwise and axial length scales as a function of $ \textit{Ro}^{-1}$. For comparison, the scales associated with large-scale TV at $ \textit{Ro}^{-1}=0$ are indicated by diamonds.

Figure 21

Figure 21. Instantaneous spatial correlation coefficients ($a$) $R_{u_r, \cos \gamma }$, ($b$) $R_{\cos \gamma , \tau _{r\theta }}$ and ($c$) $R_{u_r, \tau _{r\theta }}$ for different rotation cases: (i) counter-rotation at $ \textit{Ro}^{-1} = -0.5$, (ii) ICRO at $ \textit{Ro}^{-1} = 0$, and (iii) co-rotation at $ \textit{Ro}^{-1} = 0.83$. Dark grey frames highlight regions of significant spatial synchronisation, where the vortex-mediated polymer orientation leads to substantial polymer shear stress.