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Repicturing viscoelastic drag-reducing turbulence by introducing dynamics of elasto-inertial turbulence

Published online by Cambridge University Press:  11 April 2022

Wen-Hua Zhang
Affiliation:
Key Laboratory of Efficient Utilization of Low and Medium Grade Energy, MOE, School of Mechanical Engineering, Tianjin University, Tianjin 300350, PR China
Hong-Na Zhang*
Affiliation:
Key Laboratory of Efficient Utilization of Low and Medium Grade Energy, MOE, School of Mechanical Engineering, Tianjin University, Tianjin 300350, PR China
Zi-Mu Wang
Affiliation:
Department of Mechanical and Aerospace Engineering, The Hong Kong University of Science and Technology, Clear Water Bay, Kowloon, Hong Kong, PR China
Yu-Ke Li
Affiliation:
Department of Physics of Complex System, Weizmann Institute of Science, Rehovot 7610001, Israel
Bo Yu
Affiliation:
School of Mechanical Engineering, Beijing Institute of Petrochemical Technology, Beijing 102617, PR China
Feng-Chen Li*
Affiliation:
Key Laboratory of Efficient Utilization of Low and Medium Grade Energy, MOE, School of Mechanical Engineering, Tianjin University, Tianjin 300350, PR China
*
†Email addresses for correspondence: hongna@tju.edu.cn, lifch@tju.edu.cn
†Email addresses for correspondence: hongna@tju.edu.cn, lifch@tju.edu.cn

Abstract

Recently, the nature of viscoelastic drag-reducing turbulence (DRT), especially the maximum drag reduction (MDR) state, has become a focus of controversy. It has long been regarded as polymer-modulated inertial turbulence (IT), but is challenged by the newly proposed concept of elasto-inertial turbulence (EIT). This study is to repicture DRT in parallel plane channels by introducing dynamics of EIT through statistical, structural and budget analysis for a series of flow regimes from the onset of drag reduction to EIT. Some underlying mechanistic links between DRT and EIT are revealed. Energy conversion between velocity fluctuations and polymers as well as pressure redistribution effects are of particular concern, based on which a new energy self-sustaining process (SSP) of DRT is repictured. The numerical results indicate that at low Reynolds number ($Re$), weak IT flow is replaced by a laminar regime before the barrier of EIT dynamics is established with the increase of elasticity, whereas, at moderate $Re$, EIT-related SSP can get involved and survive from being relaminarized. This further explains the reason why relaminarization phenomenon is observed for low $Re$ while the flow directly enters MDR and EIT at moderate $Re$. Moreover, with the proposed energy picture, the newly discovered phenomenon that streamwise velocity fluctuations lag behind those in the wall-normal direction can be well explained. The repictured SSP certainly justifies the conjecture that IT nature is gradually replaced by that of EIT in DRT with the increase of elasticity.

Information

Type
JFM Papers
Copyright
© The Author(s), 2022. Published by Cambridge University Press
Figure 0

Table 1.Calculation conditions. Here $N$ and $V$ denote Newtonian and viscoelastic fluids, respectively; no drag reduction (NDR); low drag reduction (LDR); high drag reduction (HDR); drag-reducing flows with no DR effect (i.e. MDR); $0\,\% < {\rm DR}\,\% < 40\,\%, 40\,\% \le {\rm DR}\,\% < {\rm MDR}$ and ${\rm DR}\,\%={\rm MDR}$.

Figure 1

Figure 1.Evolution of statistics with $Wi$: (a) friction coefficient $f$; (b) global TKE $e_k$ and TEE $e_e$; (c) global TKE production ${P_{{k}} = - \int _0^2 {\overline {{{u'}^{* } }{{v'}^{* } }} ({{\partial {{\bar u}^ * }}}/{{\partial {y^ * }}})\, \textrm {d} {y^ * }} }$ and TEE production rate ${P_{{e}} = - \int _0^2 {\bar \tau _{E2}^{{ \ast }}({{\partial {{\bar u}^ * }}}/{{\partial {y^ * }}})\, \textrm {d} {y^ * }} }$; (d) global energy transformation rate ${G = \int _0^2 {\overline {\tau '^{*}_{ij} ({{\partial u'^{*}_i}}/{{\partial x_j^*}})} \, \textrm {d} {y^ * }} }$. The MDR asymptote of Virk (1975) in (a) is $f=0.58 {Re}^{-0.58}$. Here $G^* >0$ represents the energy that is globally transferred from polymers to the flow structures, otherwise from the flow structures to the polymers.

Figure 2

Figure 2.Distributions of $C_{uv}(y^*,\xi ^*)$: (a) in the $\xi$–$y$ plane; (b) at $y^* \approx 0.5$ and normalized by RSS here. Inset is $\xi _{{max}}^*$ versus $Wi$ at different $Re$. Here $\xi _{{max}}^*$ corresponds to the position where $C_{uv}(\xi ^*)$ reaches the maximum.

Figure 3

Figure 3.Instantaneous contours of streamwise polymer extension ($R_x=\sqrt {c_{xx}}$) in the $x$–$y$ plane at active state. The superimposed isolines represent $Q$ in different subgraphs: green, negative; red, positive. The abscissa and ordinate of the subgraphs are $x^*$ and $y^*$ (from 0 to 2), respectively: (a) $x^*\in (0, 5{\rm \pi} )$; (b) $x^*\in (0, 7{\rm \pi} )$; (c) $x^*\in (0, 11{\rm \pi} )$; (d) $x^*\in (0, 16{\rm \pi} )$.

Figure 4

Figure 4.Instantaneous contours of streamwise polymer extension ($R_x=\sqrt {c_{xx}}$) in the $x$–$y$ plane at active state. The superimposed isolines represent $G_{xx}$ in different subgraphs: green, negative; red, positive. The abscissa and ordinate of the subgraphs are $x^*$ and $y^*$ (from 0 to 2), respectively: (a) $x^*\in (0, 5{\rm \pi} )$; (b) $x^*\in (0, 7{\rm \pi} )$; (c) $x^*\in (0, 11{\rm \pi} )$; (d) $x^*\in (0, 16{\rm \pi} )$.

Figure 5

Figure 5.Instantaneous contours of wall-normal polymer extension in the $x$–$y$ plane at active state. The superimposed isolines represent $Q$ in different subgraphs: green, negative; red, positive. The abscissa and ordinate of the subgraphs are $x^*$ and $y^*$ (from 0 to 2), respectively: (a) $x^*\in (0, 5{\rm \pi} )$; (b) $x^*\in (0, 7{\rm \pi} )$; (c) $x^*\in (0, 11{\rm \pi} )$; (d) $x^*\in (0, 16{\rm \pi} )$.

Figure 6

Figure 6.Instantaneous contours of wall-normal polymer extension in the $x$–$y$ plane at active state. The superimposed isolines represent $G_{yy}$ in different subgraphs: green, negative; red, positive. The abscissa and ordinate of the subgraphs are $x^*$ and $y^*$ (from 0 to 2), respectively: (a) $x^*\in (0, 5{\rm \pi} )$; (b) $x^*\in (0, 7{\rm \pi} )$; (c) $x^*\in (0, 11{\rm \pi} )$; (d) $x^*\in (0, 16{\rm \pi} )$.

Figure 7

Figure 7.Budgets analysis for $\overline {{{u'}^{* }}{{u'}^{*}}}$, $\overline {{{v'}^{* }}{{v'}^{*}}}$, $\overline {{{u'}^{* }}{{v'}^{*}}}$, $\overline {\tau _{xx}^*}$, $\overline {\tau _{yy}^*}$ and $\overline {\tau _{xy}^*}$ at $Re=6000$, where ${P_{ij}^{{R}}}$ is Reynolds production rate; ${P_{ij}^{{E}}}$ is elastic production rate; ${\varepsilon _{ij}}$ is dissipation rate; ${G_{ij}}$ is elastic stress–strain term. Especially, ${P_{xx}^{{E2}}}=2\tau _{E2}\partial \bar u^*/\partial y^*$ is the elastic production by NESS.

Figure 8

Figure 8.Budgets analysis for $\overline {{{u'}^{* }}{{u'}^{*}}}$, $\overline {{{v'}^{* }}{{v'}^{*}}}$, $\overline {{{u'}^{* }}{{v'}^{*}}}$, $\overline {\tau _{xx}^*}$, $\overline {\tau _{yy}^*}$ and $\overline {\tau _{xy}^*}$ at $Re=2500$, where ${P_{ij}^{{R}}}$ is Reynolds production rate; ${P_{ij}^{{E}}}$ is elastic production rate; ${\varepsilon _{ij}}$ is dissipation rate; ${G_{ij}}$ is elastic stress–strain term. Especially, ${P_{xx}^{{E2}}}=2\tau _{E2}\partial \bar u^*/\partial y^*$ is the elastic production by NESS.

Figure 9

Figure 9.Pressure r.m.s. as a function of $y^*$: (a–d) total, rapid, slow and polymeric contribution (see panel (a) for legend) at $Re=6000$; (e–h) total, rapid, slow and polymeric contribution (see panel (e) for legend) at $Re=2500$.

Figure 10

Figure 10.Profiles of total pressure distribution at $Re=6000$ on $\overline {{{u'}^{* }}{{u'}^{*}}}$, $\overline {{{v'}^{* }}{{v'}^{*}}}$ and the divided rapid, slow and elastic contributions (see panel (h) for legend), where ${\varPhi _{xx} =2{\overline {{{p'}^{* } }({{{\partial u'^{* } }}/{{\partial x^{* } }}} )} }}$; ${\varPhi _{yy} =2{\overline {{{p'}^{* } }( {{{\partial v'^{* } }}/{{\partial y^{* } }}} )} }}$; ${{{p'}^{* } }( \boldsymbol {x} ) = {p'}_R^{* } ( \boldsymbol {x} ) +{p'}_S^{* } ( \boldsymbol {x} ) +{p'}_P^{* } ( \boldsymbol {x} )}$.

Figure 11

Figure 11.Profiles of total pressure distribution at $Re=2500$ on $\overline {{{u'}^{* }}{{u'}^{*}}}$, $\overline {{{v'}^{* }}{{v'}^{*}}}$ and the divided rapid, slow and elastic contributions (see panel (h) for legend), where ${\varPhi _{xx} =2{\overline {{{p'}^{* } }( {{{\partial u'^{* } }}/{{\partial x^{* } }}} )} }}$; ${\varPhi _{yy} =2{\overline {{{p'}^{* } }( {{{\partial v'^{* } }}/{{\partial y^{* } }}} )} }}$; ${{{p'}^{* } }( \boldsymbol {x} ) = {p'}_R^{* } ( \boldsymbol {x} ) +{p'}_S^{* } ( \boldsymbol {x} ) +{p'}_P^{* } ( \boldsymbol {x} )}$.

Figure 12

Figure 12.Energy picture of viscoelastic DRT: —— (cyan) and —— (blue), SSP cycles in IT and EIT, respectively; —— (orange), the bypass of energy process caused by the passive response of polymers on IT; —— (red), energy source and dissipation.

Figure 13

Figure 13.Instantaneous contours of streamwise velocity in the $x$–$z$ plane close to the channel centre. The abscissa and ordinate of the subgraphs are $x^*$ (from 0 to 20${\rm \pi}$) and $z^*$ (from 0 to 5${\rm \pi}$), respectively.