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Self-sustaining process of minimal attached eddies in turbulent channel flow

Published online by Cambridge University Press:  20 April 2016

Yongyun Hwang*
Affiliation:
Department of Aeronautics, Imperial College London, South Kensington, London SW7 2AZ, UK
Yacine Bengana
Affiliation:
Départment de Mécanique, Université de Pierre et Marie Curie, 4 Place Jussieu, 75005 Paris, France
*
†Email address for correspondence: y.hwang@imperial.ac.uk

Abstract

It has been recently shown that the energy-containing motions (i.e. coherent structures) in turbulent channel flow exist in the form of Townsend’s attached eddies by a numerical experiment which simulates the energy-containing motions only at a prescribed spanwise length scale using their self-sustaining nature (Hwang, J. Fluid Mech., vol. 767, 2015, pp. 254–289). In the present study, a detailed investigation of the self-sustaining process of the energy-containing motions at each spanwise length scale (i.e. the attached eddies) in the logarithmic and outer regions is carried out with an emphasis on its relevance to ‘bursting’, which refers to an energetic temporal oscillation of the motions (Flores & Jiménez, Phys. Fluids, vol. 22, 2010, 071704). It is shown that the attached eddies in the logarithmic and outer regions, composed of streaks and quasi-streamwise vortical structures, bear the self-sustaining process remarkably similar to that in the near-wall region: i.e. the streaks are significantly amplified by the quasi-streamwise vortices via the lift-up effect; the amplified streaks subsequently undergo a‘rapid streamwise meandering motion’, reminiscent of streak instability or transient growth, which eventually results in breakdown of the streaks and regeneration of new quasi-streamwise vortices. For the attached eddies at a given spanwise length scale ${\it\lambda}_{z}$ between ${\it\lambda}_{z}^{+}\simeq 100$ and ${\it\lambda}_{z}\simeq 1.5h$ , the single turnover time period of the self-sustaining process is found to be $Tu_{{\it\tau}}/{\it\lambda}_{z}\simeq 2$ ( $u_{{\it\tau}}$ is the friction velocity), which corresponds well to the time scale of the bursting. Two additional numerical experiments, designed to artificially suppress the lift-up effect and the streak meandering motions, respectively, reveal that these processes are essential ingredients of the self-sustaining process of the attached eddies in the logarithmic and outer regions, consistent with several previous theoretical studies. It is also shown that the artificial suppression of the lift-up effect of the attached eddies in the logarithmic and outer regions leads to substantial amounts of turbulent skin-friction reduction.

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© 2016 Cambridge University Press 
Figure 0

Table 1.Simulation parameters in the present study. Here, $Re_{m}$ is the Reynolds number based on the bulk velocity and $T_{avg}$ is the time interval for the average. In the names of the simulations, $L$ indicates ‘logarithmic’, $O$ ‘outer’ and $S$ ‘self-sustaining’.

Figure 1

Figure 1.(a) Mean-velocity profile and (b) turbulent velocity fluctuations of the reference simulation: ——, $O950$ without the filtering (2.1); – – – –, $O950$; – - – - –, DNS at $Re_{{\it\tau}}=934$ (del Álamo et al.2004).

Figure 2

Figure 2.Normalised second-order statistics of the attached eddies, scaled with the given spanwise length $L_{z}$: (a) streamwise velocity, $y=0.3L_{z}$; (b) wall-normal velocity, $y=0.4L_{z}$; (c) spanwise velocity, $y=0.4L_{z}$; (d) Reynolds stress, $y=0.2L_{z}$. Here, – – – –, from $Re_{{\it\tau}}\simeq 950$ ($SL950a$, $SL950b$); ——, from $Re_{{\it\tau}}\simeq 1800$ ($SL1800a$, $SL1800b$, $SL1800c$).

Figure 3

Figure 3.Time evolution of the flow field of $O950$: (a) time trace of $E_{u}^{+}$ (solid) and $E_{v}^{+}$ (dashed); (b) magnification of (a) for $tu_{{\it\tau}}/h\in [158,164]$; (c–f) the corresponding flow visualisation at $tu_{{\it\tau}}/h=159,160.2,160.9,162$. In (c–f), the red and blue iso surfaces indicate $u^{+}=-3.2$ and $v^{+}=1.4$, respectively.

Figure 4

Figure 4.Time evolution of the flow field of $SO950$: (a) time trace of $E_{u}^{+}$ (solid) and $E_{v}$ (dashed); (b) magnification of (a) for $tu_{{\it\tau}}/h\in [564,572]$; (c–f) the corresponding flow visualisation at $tu_{{\it\tau}}/h=565,568.5,569.3,570$. In (c–f), the red and blue iso surfaces indicate $u^{+}=-4$ and $v^{+}=1.5$, respectively.

Figure 5

Figure 5.Time correlation functions of (a,c) $O950$ and (b,d) $SO950$. In (a,b), ——, $C_{uu}({\it\tau})$; – – – –, $C_{vv}({\it\tau})$; – - – - –, $C_{ww}({\it\tau})$. In (c,d), ——, $C_{uv}({\it\tau})$; – – – –, $C_{uw}({\it\tau})$; – - – - –, $C_{vw}({\it\tau})$.

Figure 6

Figure 6.Time correlation functions of (a,c) $O950$ and (b,d) $SO950$. In (a,b), ——, $C_{00}({\it\tau})$; – – – –, $C_{11}({\it\tau})$; – - – - –, $C_{01}({\it\tau})$. In (c,d), ——, $C_{0u}({\it\tau})$; – – – –, $C_{0v}({\it\tau})$; – - – - –, $C_{1v}({\it\tau})$.

Figure 7

Figure 7.Auto-correlation functions: (a,b) $C_{uu}({\it\tau})$; (c,d) $C_{vv}({\it\tau})$; (e,f) $C_{11}({\it\tau})$. In (a,c,e), —— $L950a$; – – – – $L950b$; – - – - – $L1800a$; –$\cdot \cdot$–$\cdot \cdot$– $L1800b$; $\cdots \cdots$ $L1800c$, while, in (b,d,f), —— $LS950a$; – – – – $LS950b$; – - – - – $LS1800a$; –$\cdot \cdot$–$\cdot \cdot$– $LS1800b$; $\cdots \cdots$ $LS1800c$.

Figure 8

Figure 8.Cross-correlation functions: (a,b) $C_{uv}({\it\tau})$; (c,d) $C_{vw}({\it\tau})$; (e,f) $C_{1v}({\it\tau})$. In (a,c,e), —— $L950a$; – – – – $L950b$; – - – - – $L1800a$; –$\cdot \cdot$–$\cdot \cdot$– $L1800b$; $\cdots \cdots$ $L1800c$, while, in (b,d,f), —— $SL950a$; – – – – $SL950b$; – - – - – $SL1800a$; –$\cdot \cdot$–$\cdot \cdot$– $SL1800b$; $\cdots \cdots$ $SL1800c$.

Figure 9

Figure 9.A schematic diagram of self-sustaining process of the attached eddies (originally proposed by Hamilton et al. (1995) for the near-wall motions). The diagram incorporates the streak transient growth proposed by Schoppa & Hussain (2002) for the near-wall motions as well as the Orr mechanism proposed by Jiménez (2013, 2015). Here, $u_{s}$ denotes the streamwise velocity given with the amplified streaks.

Figure 10

Figure 10.Time trace of $E_{u}$ and $E_{v}$ of $SO950$. At $tU_{e}/h=7500$ ($U_{e}$ is the centreline velocity of the laminar velocity profile with the same volume flux), the streamwise momentum equation is replaced by (4.3). Here, $E_{u}$ and $E_{v}$ are normalised with $U_{e}$.

Figure 11

Figure 11.One-dimensional spanwise wavenumber spectra of (a,b) the streamwise and (c,d) the wall-normal velocities: (a,c) $O950$; (b,d) $O950$ with (4.3). Here, the spectra are normalised with $U_{e}$ for the purpose of comparison.

Figure 12

Figure 12.One-dimensional streamwise wavenumber spectra of (a,b) the streamwise and (c,d) the wall-normal velocities: (a,c) $O950$; (b,d) $O950$ with (4.3). Here, the spectra are normalised with $U_{e}$ for the purpose of comparison.

Figure 13

Table 2.Skin-friction reduction ${\rm\Delta}C_{f}$ by suppressing the lift-up effect with (4.3).

Figure 14

Figure 13.Time trace of $E_{u}$ and $E_{v}$ of $SO950$. At $tU_{e}/h=7500$, (4.4) is applied. Here, $E_{u}$ and $E_{v}$ are normalised with $U_{e}$.

Figure 15

Figure 14.One-dimensional spanwise wavenumber spectra of (a,b) the streamwise and (c,d) the wall-normal velocities: (a,c) $O950$; (b,d) $O950$ with (4.4). Here, the spectra are normalised with $U_{e}$ for the purpose of comparison.

Figure 16

Figure 15.One-dimensional streamwise wavenumber spectra of (a,b) the streamwise and (c,d) the wall-normal velocities: (a,c) $O950$; (b,d) $O950$ with (4.4). Here, the spectra are normalised with $U_{e}$ for the purpose of comparison.

Figure 17

Figure 16.Time correlation functions of (a) $O950$ without (2.1) and (b) $O950$. Here, ——, $C_{uu}({\it\tau})$; – – – –, $C_{vv}({\it\tau})$; – - – - –, $C_{uv}({\it\tau})$; –$\cdot \cdot$–$\cdot \cdot$–, $C_{vw}({\it\tau})$.

Figure 18

Figure 17.Comparison of the second-order statistics of the self-sustaining attached eddies in the minimal unit ($SL1800c$ in the present study) with those in the long streamwise domain ($L1800c$ in Hwang 2015): (a) the streamwise, wall-normal and spanwise velocities; (b) Reynolds stress. Here, ——, $SL1800c$ in the present study; – – – –, $L1800c$ in Hwang (2015).