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Non-monotonic effect of Stokes number on turbulence modulation in particle-laden channel flow

Published online by Cambridge University Press:  24 July 2025

Zi-Mo Liao
Affiliation:
State Key Laboratory of High Temperature Gas Dynamics, School of Engineering Science, University of Science and Technology of China, Hefei 230027, PR China
Fenghui Lin
Affiliation:
State Key Laboratory of High Temperature Gas Dynamics, School of Engineering Science, University of Science and Technology of China, Hefei 230027, PR China
Luoqin Liu
Affiliation:
State Key Laboratory of High Temperature Gas Dynamics, School of Engineering Science, University of Science and Technology of China, Hefei 230027, PR China
Nan-Sheng Liu*
Affiliation:
State Key Laboratory of High Temperature Gas Dynamics, School of Engineering Science, University of Science and Technology of China, Hefei 230027, PR China
Xi-Yun Lu*
Affiliation:
State Key Laboratory of High Temperature Gas Dynamics, School of Engineering Science, University of Science and Technology of China, Hefei 230027, PR China
*
Corresponding authors: Nan-Sheng Liu, lns@ustc.edu.cn; Xi-Yun Lu, xlu@ustc.edu.cn
Corresponding authors: Nan-Sheng Liu, lns@ustc.edu.cn; Xi-Yun Lu, xlu@ustc.edu.cn

Abstract

The effect of Stokes number on turbulence modulation in particle-laden channel flow is investigated through four-way coupled point-particle direct numerical simulations, with the mass loading fixed at 0.6 and the friction Stokes number $St^+$ varying from 3 to 300. A full transition pathway is observed, from a drag-enhanced to a drag-reduced regime, eventually approaching the single-phase state as $St^+$ increases towards 300. A set of transport equations for the particle phase is derived analytically to characterise the interphase coupling, within the framework of the point-based statistical description of particle-laden turbulence. By virtue of this, two dominant mechanisms are identified and quantitatively characterised: a positive, particle-induced extra transport that decreases monotonically with increasing $St^+$, and a negative, particle-induced extra dissipation that varies non-monotonically with $St^+$. The coupling of these two mechanisms leads to a direct contribution of the particle phase to the shear stress balance, the turbulent kinetic energy budgets and the Reynolds stress budgets. Consequently, as $St^+$ increases, the self-sustaining cycle of near-wall turbulence transitions from being augmented to being suppressed and, eventually, returns to the single-phase state. This gives rise to an indirect effect, manifested as a non-monotonic modulation of Reynolds shear stress and turbulence production rate. Taken together, complex interplays between particle-modified turbulent transport, particle-induced extra transport and extra dissipation are analysed and summarised, providing a holistic physical picture composed of consistent interpretations of turbulence modulation induced by small heavy particles.

Information

Type
JFM Papers
Copyright
© The Author(s), 2025. Published by Cambridge University Press
Figure 0

Figure 1.Schematic of the computational domain used in the present simulations. The contour plot represents an instantaneous streamwise velocity field for the St030 case. Half of the computational domain is set to be translucent to visualise the dispersed particles (light blue spheres).

Figure 1

Table 1.Simulation set-ups for the particle phase. The particle volume fraction $\phi _v$ varies from ${\sim} 10^{-3}$ to ${\sim} 10^{-5}$ corresponding to a mass loading ${\Phi }_m$ fixed at 0.6, lying in the (semi-)dilute suspension regime. $N_s$ and $\mathcal{T}$ denote the number of snapshots and the time window widths, respectively, adopted in each case for calculating the statistics.

Figure 2

Figure 2.Time series of wall shear stress $\tau _w(t)$ during the sampling window (solid lines). The dashed lines of the corresponding colours represent the time-averaged quantities.

Figure 3

Figure 3.Mean profiles of: $(a)$ streamwise flow velocity in wall units; $(b)$ streamwise particle velocity in outer units; $(c)$ streamwise particle velocity in wall units and $(d)$ normalised particle concentration.

Figure 4

Table 2.Overall statistics of the present simulations. Here, the skin-friction coefficient is $C_f\equiv 2\tau _w/(\rho U_b^2)$. The drag-modification coefficient is defined as $\text{DM}\equiv (C_f-C_f^{{SP}})/C_f^{{SP}}$.

Figure 5

Figure 4.Shear stress balance profiles for four typical cases: $(a)$ St003; $(b)$ St010; $(c)$ St100 and $(d)$ St300. In panel $(d)$, the SP results are also shown as dashed lines of corresponding colours, representing the $St^+\to \infty$ limit of SSB.

Figure 6

Figure 5.Profiles of $(a)$$\bar {\tau }^{\textit{T}}$, $(b)$$\bar {\tau }^{\textit{P}}$ and $(c)$$\bar {\tau }^{\textit{E}} = \bar {\tau }^{\textit{T}} + \bar {\tau }^{\textit{P}}$, and the $(d)$$C_f$–$St^+$ curves.

Figure 7

Figure 6.$(a)$ Streamwise momentum coupling term and $(b)$ mean streamwise slip velocity.

Figure 8

Figure 7.TKE budget profiles of three typical cases: $(a)$ St003, $(b)$ St100 and $(c)$ St300 and $(d)$ the SP results. Hereafter, all the budget terms are scaled by $(u_\tau ^{{SP}})^4/\nu$.

Figure 9

Figure 8.PFKE budget profiles of three typical particle-laden cases: $(a)$ St003, $(b)$ St100 and $(c)$ St300.

Figure 10

Figure 9.Terms that are critical to the TKE, PFKE budgets and TKE–PFKE transfer, including $(a)$$P$, $(b)$${\mathcal{W}}^F$, $(c)$$P_p$, $(d)$$W^F$, $(e)$$\epsilon ^{p,F}$ in solid and $\alpha$ in dashed lines. For clarity, only the near-wall region is displayed, as their values in the outer layer gradually decay to zero. Panel $(f)$ shows the integrals of dominant terms, where $P^E\equiv P+{\mathcal{W}}^F$ denotes the effective production rate, and all the quantities are normalised using the integral of single-phase production rate $\mathcal{I}(P^{{SP}})$.

Figure 11

Figure 10.Reynolds stress budgets of the present single-phase channel flow: $(a)$$r_{11}$; $(b)$$r_{22}$; $(c)$$r_{12}$. Similar to the previous section, the budget terms are scaled by $(u_\tau ^{{SP}})^4/\nu$.

Figure 12

Figure 11.Fluid-phase Reynolds stress budgets of the $(a, b, c)$ St003 and $(d, e, f)$ St100 cases: $(a, d)$$r_{11}$; $(b, e)$$r_{22}$; $(c, f)$$r_{12}$.

Figure 13

Figure 12.Particle-phase Reynolds stress budgets of the $(a, b, c)$ St003 and $(d, e, f)$ St100 cases: $(a, d)$$r_{p,11}$; $(b, e)$$r_{p,22}$; $(c, f)$$r_{p,12}$.

Figure 14

Figure 13.Decomposition of particle–fluid interaction term (5.13) versus Stokes number: $(a)$$ij=11$; $(b)$$ij=22$; $(c)$$ij=12$.

Figure 15

Figure 14.Reynolds stress budget integrals: $(a, d)$$r_{11}$; $(b, e)$$r_{22}$; $(c, f)$$r_{12}$. In panels $(d, e, f)$, the budget integrals are normalised such that, in each case, the summation of their squares equals one. Here, we denote $D_{ij}=D_{ij}^v+D_{ij}^t$.

Figure 16

Figure 15.Collision frequency (number of collisions per outer time scale, $h/U_b$) as a function of ($a$) $St^+$ and ($b$) $\phi _v$, with both axes shown in logarithmic scales.

Figure 17

Figure 16.($a$) Collision frequency distribution along the wall-normal direction and ($b$) the inter-particle collision terms: $\mathit{\Pi }_{p,22}$ in solid and $\mathit{\Pi }_{p,33}$ in dashed lines.

Figure 18

Figure 17.Mapping of the drag modification results based on $St^+$ and $\Phi _m$, with both axes shown on logarithmic scales. Symbols mark data resources; colours indicate whether the drag is enhanced or reduced; sizes indicate the amplitude of drag modification on a logarithmic scale, $\propto (\ln |DM|+C)$, where the constant $C$ ensures positive circle sizes. In the legend, ‘N’ (numerical) and ‘E’ (experimental) denote data types; ‘CH’ (channel) and ‘PI’ (pipe) indicate flow configurations, with the prefix ‘V’ for vertical placement. Other data sets (e.g. Kulick 1994; Paris 2001; Shokri et al.2017; Fong, Amili & Coletti 2019) did not include measurement of flow resistance and the equivalent pressure drop, and are not included in this figure.

Figure 19

Figure 18.Wall-normal profiles of the $(a)$ mean flow velocity and the shear stress balance for $(b)$$St^+=6$ and $(c)$$St^+=30$ cases. Thick lines, present results; symbols, reference data adapted from Dave & Kasbaoui (2023).

Figure 20

Table 3.Computational grids employed for grid-convergence tests: F (fine), M (medium), C (coarse). The single-phase turbulence statistics, $Re_\tau ^{{SP}}$ and $C_f^{{SP}}$, are listed to demonstrate convergence.

Figure 21

Table 4.Statistical results for the grid-convergence test, obtained for $St^+=100$. $N_s$ and $\mathcal{T}$ denote the number of snapshots and the time window widths, respectively, adopted in each case for calculating the statistics.

Figure 22

Figure 19.Mean velocity profiles for the grid-convergence test of particle-laden channel flow at $St^+=100$: (a) flow velocity; (b) particle velocity.