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Streamwise inclination angle of wall-attached eddies in turbulent channel flows

Cheng Cheng\aff1    Wei Shyy\aff1    Lin Fu\aff1,\aff2,\aff3,\corresp [email protected] \aff1Department of Mechanical and Aerospace Engineering, The Hong Kong University of Science and Technology, Clear Water Bay, Kowloon, Hong Kong \aff2Department of Mathematics, The Hong Kong University of Science and Technology, Clear Water Bay, Kowloon, Hong Kong \aff3 Center for Ocean Research in Hong Kong and Macau (CORE), The Hong Kong University of Science and Technology, Clear Water Bay, Kowloon, Hong Kong
Abstract

We develop a new methodology to assess the streamwise inclination angles (SIAs) of the wall-attached eddies populating the logarithmic region with a given wall-normal height. To remove the influences originating from other scales on the SIA estimated via two-point correlation, the footprints of the targeted eddies in the vicinity of the wall and the corresponding streamwise velocity fluctuations carried by them are isolated simultaneously, by coupling the spectral stochastic estimation with the attached-eddy hypothesis. Datasets produced with direct numerical simulations spanning ReτO(102)O(103)Re_{\tau}\sim O(10^{2})-O(10^{3}) are dissected to study the Reynolds-number effect. The present results show, for the first time, that the SIAs of attached eddies are Reynolds-number dependent in low and medium Reynolds numbers and tend to saturate at 4545^{\circ} as the Reynolds number increases. The mean SIA reported by vast previous experimental studies are demonstrated to be the outcomes of the additive effect contributed by multi-scale attached eddies. These findings clarify the long-term debate and perfect the picture of the attached-eddy model.

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1 Introduction

It is generally recognized that the high-Reynolds number wall-bounded turbulence is filled with coherent motions of disparate scales, which are responsible for the energy transfer and the fluctuation generation of turbulence. Till now, the most elegant conceptual model describing these energy-containing motions is the attached-eddy model (Townsend, 1976; Perry & Chong, 1982). It hypothesizes that the logarithmic region is occupied by an array of randomly-distributed and self-similar energy-containing motions (or eddies) with their roots attached to the near-wall region (see Fig. 1). During the recent decades, a growing body of evidence that supports the attached-eddy hypothesis has emerged rapidly, e.g., Hwang (2015), Hwang & Sung (2018), Cheng et al. (2020b), Hwang et al. (2020), to name a few. The reader is referred to a recent review work by Marusic & Monty (2019) for more details. Throughout the paper, the terms ‘eddy’ and ‘motion’ are exchangeable. It should be noted that the terms of ‘wall-attached motions’ and ‘wall-attached eddies’ used in the present study do not only refer to the self-similar eddies in the logarithmic region, but also the very-large-scale motions (VLSMs) or superstructures, as some recent studies have shown that VLSMs are also wall-attached, despite that their physical characteristics do not match the attached-eddy model (Hwang & Sung, 2018; Yoon et al., 2020).

Previous studies have established that the energy-containing eddies populating the logarithmic and outer regions bear characteristic SIAs due to the mean shear (see Fig. 1(aa)). As early as the 1970s, Kovasznay et al. (1970) found that the large-scale structures in the outer intermittent region of a turbulent boundary layer have a moderate tilt in the streamwise direction. On the other hand, for the eddies in the logarithmic region of wall turbulence, the wall-attached Λ\Lambda-vortex was used by Perry & Chong (1982) to illustrate them. According to Adrian et al. (2000), these Λ\Lambda-vortexes are apt to cluster along the flow direction and form an integral whole (generally called as vortex packets). Further observations in channel flows (Christensen & Adrian, 2001) demonstrated that the heads of Λ\Lambda-vortexes among the vortex packets tend to slope away from the wall in a statistical sense, with SIAs between 1212^{\circ} and 1313^{\circ}. Most additional studies have shown a similar result, and it is widely accepted that the approximate SIAs of eddies are in the range of 1010^{\circ} to 1616^{\circ} (Boppe et al., 1999; Christensen & Adrian, 2001; Carper & Porté-Agel, 2004; Marusic & Heuer, 2007; Baars et al., 2016). Besides, the SIA is also found to be Reynolds-number independent (Marusic & Heuer, 2007).

Refer to caption
Figure 1: A schematic of the attached-eddy model: (aa) xx-yy plane and (bb) yy-zz plane view. Each parallelogram in (aa) and circle in (bb) represents an individual attached eddy. Here, xx, yy and zz denote the streamwise, wall-normal, and spanwise directions, respectively. ys+y_{s}^{+} (100) and ye+y_{e}^{+} (0.2h+0.2h^{+}) denote the lower and upper bound of the logarithmic region, respectively (Jiménez, 2018; Baars & Marusic, 2020a; Wang et al., 2021). yo+y_{o}^{+} is the outer reference height. Δy+\Delta y^{+} is the local grid spacing along the wall-normal direction. αm\alpha_{m} and αs\alpha_{s} are the mean and individual SIA of attached eddies, respectively. These two figures are merely conceptual sketches, and the eddy population density is not in accordance with that of Perry & Chong (1982).

However, the SIA estimated by experimentalists using the traditional statistical approach is the mean structure angle indeed (Marusic & Heuer, 2007; Deshpande et al., 2019). The common procedure to obtain the SIA is based on the calculation of the cross correlation between the streamwise wall-shear stress fluctuation (τx\tau_{x}^{\prime}) and the streamwise velocity fluctuation (uu^{\prime}) at a wall-normal position in the log region (yoy_{o}). The cross correlation can be expressed as

Rτxu(Δx)=τx(x)u(x+Δx,yo)τx2u2,R_{\tau_{x}^{\prime}u^{\prime}}(\Delta x)=\frac{\langle\tau_{x}^{\prime}(x)u^{\prime}(x+\Delta x,y_{o})\rangle}{\sqrt{\left\langle\tau_{x}^{\prime 2}\right\rangle\left\langle u^{{}^{\prime}2}\right\rangle}}, (1)

where <><\cdot> represents the ensemble spatial average, and Δx\Delta x the streamwise delay. The SIA can be estimated by

αm=arctan(yoΔxp),\alpha_{m}=\arctan(\frac{y_{o}}{\Delta x_{p}}), (2)

where Δxp\Delta x_{p} denotes the streamwise delay corresponding to the peak in RτxuR_{\tau_{x}^{\prime}u^{\prime}}. Considering that an array of wall-attached eddies with distinct wall-normal heights can simultaneously convect past the reference position yoy_{o}, αm\alpha_{m} in Eq. (2) should be regarded as the mean angle of these eddies. Hence, the subscript ‘m’ in Eq. (2) refers to ‘mean’.

To estimate the SIAs of the largest wall-attached eddies, Deshpande et al. (2019) introduced a spanwise offset between the near-wall and logarithmic probes to isolate these wall-attached motions in the log region. They found that their SIAs are approximately 4545^{\circ}. This observation is consistent with several theoretical analyses. For example, Moin & Kim (1985) and Perry et al. (1992) proposed that for the flows with two-dimensional mean flows, the characteristic angles of the energy-containing eddies should follow the direction of the principal rate of mean strain. More specifically, their SIAs should be 4545^{\circ} for a zero-pressure-gradient turbulent boundary layer (Perry et al., 1992). Marusic (2001) found that the mean SIA of the induced turbulence field by attached eddies is akin to the experimental measurements, if the hierarchical attached eddies tilt away from the wall with individual SIA being 4545^{\circ} and organize like the vortex packets observed in numerical and laboratory experiments.

Reviewing the work of predecessors, it can be found the SIAs of attached eddies at a given length scale are ambiguous. Traditional measurements are only applicable for the assessment of the mean SIA (Brown & Thomas, 1977; Boppe et al., 1999; Marusic & Heuer, 2007). Moreover, the technique adopted by Deshpande et al. (2019) can only isolate the largest wall-attached motions in the logarithmic region. Considering the characteristic scale of an individual attached eddy being its wall-normal height as per the attached-eddy model (Townsend, 1976; Perry & Chong, 1982), it is self-evident that it is of great importance to assess the SIAs of attached eddies with any heights in the logarithmic region, not only for the completeness of attached-eddy hypothesis, but also the accuracy of turbulence simulations (Marusic, 2001; Carper & Porté-Agel, 2004). In the present study, we aim to achieve this goal by leaning upon the modified spectral stochastic estimation (SSE) proposed by Baars et al. (2016), and dissecting the direct numerical simulations (DNS) database spanning broad-band Reynolds numbers. We will also discuss the relationship between the mean SIA and the scale-based SIA.

2 DNS database and methodology to calculate the SIA

2.1 DNS database

The DNS database adopted in the present study has been extensively validated by Jiménez and co-workers (Del Álamo & Jiménez, 2003; Del Álamo et al., 2004; Hoyas & Jiménez, 2006; Lozano-Durán & Jiménez, 2014). Four cases at ReτRe_{\tau}=545, 934, 2003 and 4179 are used and named as Re550, Re950, Re2000 and Re4200, respectively (Reτ=huτ/νRe_{\tau}=hu_{\tau}/\nu, hh denotes the channel half-height, uτu_{\tau} the wall friction velocity and ν\nu the kinematic viscosity). All these data are provided by the Polytechnic University of Madrid. Details of the parameter settings are listed in Table 1. Note that the relatively smaller computational domain size of Re4200 may influence the estimation of SIAs of the attached eddies populating the upper part of the logarithmic region. This limitation will be discussed in section 3 and Appendix A.

CaseCase ReτRe_{\tau} Lx(h)L_{x}(h) Ly(h)L_{y}(h) Lz(h)L_{z}(h) Δx+\Delta x^{+} Δz+\Delta z^{+} Δymin+\Delta y_{min}^{+} Δymax+\Delta y_{max}^{+} NFN_{F} Tuτ/hTu_{\tau}/h
Re550 547 8π8\pi 2 4π4\pi 13.4 6.8 0.04 6.7 142 22
Re950 934 8π8\pi 2 3π3\pi 11.5 5.7 0.03 7.6 73 12
Re2000 2003 8π8\pi 2 3π3\pi 12.3 6.2 0.32 8.9 48 11
Re4200 4179 2π2\pi 2 π\pi 12.3 6.2 0.32 10.6 40 15
Table 1: Parameter settings of the DNS database. Here, LxL_{x}, LyL_{y} and LzL_{z} are the sizes of the computational domain in the streamwise, wall-normal and spanwise directions, respectively. Δx+\Delta x^{+} and Δz+\Delta z^{+} denote the streamwise and spanwise grid resolutions in viscous units, respectively. Δymin+\Delta y_{min}^{+} and Δymax+\Delta y_{max}^{+} denote the finest and coarsest resolution in the wall-normal direction, respectively. NFN_{F} and Tuτ/hTu_{\tau}/h indicate the number of instantaneous flow fields and the total eddy turnover time used to accumulate statistics, respectively.

2.2 Spectral stochastic estimation

According to the inner-outer interaction model (Marusic et al., 2010), the large-scale motions would exert the footprints on the near-wall region, i.e., the superposition effects. Baars et al. (2016) demonstrated that this component (denoted as uL+(x+,y+,z+)u_{L}^{{}^{\prime}+}(x^{+},y^{+},z^{+})) can be obtained by the spectral stochastic estimation of the streamwise velocity fluctuation at the logarithmic region yo+y_{o}^{+}, namely by

uL+(x+,y+,z+)=Fx1{HL(λx+,y+)Fx[uo+(x+,yo+,z+)]},u_{L}^{{}^{\prime}+}\left(x^{+},y^{+},z^{+}\right)=F_{x}^{-1}\left\{H_{L}\left(\lambda_{x}^{+},y^{+}\right)F_{x}\left[u_{o}^{{}^{\prime}+}\left(x^{+},y_{o}^{+},z^{+}\right)\right]\right\}, (3)

where uo+u_{o}^{{}^{\prime}+} is the streamwise velocity fluctuation at yo+y_{o}^{+} in the logarithmic region, and, FxF_{x} and Fx1F_{x}^{-1} denote the FFT and the inverse FFT in the streamwise direction, respectively. HLH_{L} is the transfer kernel, which evaluates the correlation between u^(y+)\hat{u^{\prime}}(y^{+}) and uo^(yo+)\hat{u_{o}^{\prime}}(y_{o}^{+}) at a given length scale λx+\lambda_{x}^{+}, and can be calculated as

HL(λx+,yo+)=u^(λx+,y+,z+)uo^¯(λx+,yo+,z+)uo^(λx+,yo+,z+)uo^¯(λx+,yo+,z+),H_{L}\left(\lambda_{x}^{+},y_{o}^{+}\right)=\frac{\left\langle\hat{u^{\prime}}\left(\lambda_{x}^{+},y^{+},z^{+}\right)\overline{\hat{u_{o}^{\prime}}}\left(\lambda_{x}^{+},y_{o}^{+},z^{+}\right)\right\rangle}{\left\langle\hat{u_{o}^{\prime}}\left(\lambda_{x}^{+},y_{o}^{+},z^{+}\right)\overline{\hat{u_{o}^{\prime}}}\left(\lambda_{x}^{+},y_{o}^{+},z^{+}\right)\right\rangle}, (4)

where u^\hat{u^{\prime}} is the Fourier coefficient of uu^{\prime}, and u^¯\overline{\hat{u^{\prime}}} is the complex conjugate of u^\hat{u^{\prime}}. y+y^{+} is set as y+=0.3y^{+}=0.3, and the outer reference height yo+y_{o}^{+} varies from 100100 to the outer region 0.7h+0.7h^{+} according to the wall-normal grid distribution. Once uL+u_{L}^{{}^{\prime}+} is obtained, the superposition component of τx+\tau_{x}^{{}^{\prime}+} can be calculated by definition (i.e., uL+y+\frac{\partial u_{L}^{{}^{\prime}+}}{\partial y^{+}} at the wall) and denoted as τx,L+(yo+)\tau_{x,L}^{{}^{\prime}+}(y_{o}^{+}).

Analogously, to eliminate the effects from the wall-detached eddies with random orientations, which contribute significantly to the streamwise velocity fluctuations at yo+y_{o}^{+}, we can also use the near-wall streamwise velocity fluctuation in viscous layer y+y^{+} to reconstruct the wall-coherent streamwise velocity fluctuation in the logarithmic region yo+y_{o}^{+} by spectral stochastic estimation (Adrian, 1979), i.e.,

uW+(x+,yo+,z+)=Fx1{HW(λx+,y+)Fx[u+(x+,y+,z+)]},u_{W}^{{}^{\prime}+}\left(x^{+},y_{o}^{+},z^{+}\right)=F_{x}^{-1}\left\{H_{W}\left(\lambda_{x}^{+},y^{+}\right)F_{x}\left[u^{{}^{\prime}+}\left(x^{+},y^{+},z^{+}\right)\right]\right\}, (5)

where uW+u_{W}^{{}^{\prime}+} is the wall-coherent component of uo+u_{o}^{{}^{\prime}+}. The wall-based transfer kernel HWH_{W} can be calculated as

HW(λx+,yo+)=uo^(λx+,yo+,z+)u^¯(λx+,y+,z+)u^(λx+,y+,z+)u^¯(λx+,y+,z+).H_{W}\left(\lambda_{x}^{+},y_{o}^{+}\right)=\frac{\left\langle\hat{u_{o}^{\prime}}\left(\lambda_{x}^{+},y_{o}^{+},z^{+}\right)\overline{\hat{u^{\prime}}}\left(\lambda_{x}^{+},y^{+},z^{+}\right)\right\rangle}{\left\langle\hat{u^{\prime}}\left(\lambda_{x}^{+},y^{+},z^{+}\right)\overline{\hat{u^{\prime}}}\left(\lambda_{x}^{+},y^{+},z^{+}\right)\right\rangle}. (6)
Refer to caption
Figure 2: (aa) Variation of the statistic uW2+\langle u_{W}^{{}^{\prime}2+}\rangle as a function of yo/hy_{o}/h, and the full-channel data u2+\langle u^{{}^{\prime}2+}\rangle are included for comparison; (bb) variations of the indicator functions Ξ\Xi as functions of yo/hy_{o}/h. The red line in (aa) denotes the logarithmic decaying Eq. (7) with C1=0.54C_{1}=0.54.

Fig. 2(aa) shows the variation of uW2+\langle u_{W}^{{}^{\prime}2+}\rangle as a function of yo/hy_{o}/h in the case Re2000. The full-channel data are included for comparison. It can be seen that uW2+\langle u_{W}^{{}^{\prime}2+}\rangle roughly follows the logarithmic decay for 0.09yo/h0.20.09\leq y_{o}/h\leq 0.2, i.e., the logarithmic region. To quantify the logarithmic decay systematically, we define the indicator function Ξ=y(u2+/y)\Xi=y(\partial\langle u^{{}^{\prime}2+}\rangle/\partial y), and display their variations in Fig. 2(bb). Comparing with the full-channel data, a comparatively well-defined plateau is observed for uW2+\langle u_{W}^{{}^{\prime}2+}\rangle. The logarithmic variance of uW2+\langle u_{W}^{{}^{\prime}2+}\rangle shown in Fig. 2 is the consequence of the additive attached eddies (Townsend, 1976), and can be expressed as

uW2+=C2C1ln(yo/h),\langle u_{W}^{{}^{\prime}2+}\rangle=C_{2}-C_{1}\ln(y_{o}/h), (7)

where C2C_{2} and C1C_{1} are two constants, and C1C_{1} is approximately equal to 0.54. Actually, the magnitude of the slope of the logarithmic decaying is affected by the Reynolds number, the configuration of the wall turbulence, the methodology for isolating the signals carried by the attached eddies, and the effects of the VLSMs. The indicator function Ξ\Xi of the fully-channel data shown in Fig. 2(bb) suggests that the logarithmic region of case Re2000 is not full-developed, as the slope value of the logarithmic decaying is smaller than the Townsend-Perry constant 1.261.26 reported at high-Reynolds number experiments (Marusic et al., 2013), and close to the magnitude of C1C_{1} observed here. Furthermore, Baars & Marusic (2020b) reported that C1=0.98C_{1}=0.98 in turbulent boundary layers by analyzing the streamwise velocity fluctuations carried by the attached eddies in the logarithmic region, while Hu et al. (2020) and Hwang et al. (2020) showed that C1=0.8C_{1}=0.8 and 0.37 in channel flows, respectively. Hu et al. (2020) adopted a scale-based filter to extract the streamwise velocity fluctuations associated with the attached eddies in the logarithmic region and did not take their imperfect coherence with the near-wall flow at each scale into account. The wall-based transfer kernel HWH_{W} in Eq. (6) employed here can achieve this. Hwang et al. (2020) utilized the three-dimensional clustering method to identify the wall-attached structures in a channel flow. The differences among these decomposition methodologies may be the reason why the magnitude of C1C_{1} for turbulent channel flows reported by Hu et al. (2020) and Hwang et al. (2020) is not identical to that of the present study. Besides, it is noted that the effects of VLSMs are also retained in uW2+\langle u_{W}^{{}^{\prime}2+}\rangle, and their impacts on the logarithmic decaying are non-negligible. By the way, the methodology introduced in section 2.3 to estimate the SIAs of attached eddies at a single scale can effectively diminish the effects originating from the VLSMs (see Fig. 4). In summary, these observations demonstrate that uWu_{W}^{{}^{\prime}} can be approximately considered as the streamwise velocity fluctuations carried by the multi-scale wall-attached eddies. We will focus on the statistics in the logarithmic region in the following sections.

2.3 Methodology to isolate targeted eddies

Apparently, the SIAs of attached eddies at a single scale (αs\alpha_{s}) can not be pursued by Eq. (1)-(2). It is worth noting that in Eq. (1)-(2), the input parameter and signals are yoy_{o}, τx\tau_{x}^{\prime} and u(yo)u^{\prime}(y_{o}). Thus, to obtain an accurate αs\alpha_{s}, yoy_{o} should be set reasonably, and τx\tau_{x}^{\prime} and u(yo)u^{\prime}(y_{o}) should also be properly processed, to characterize the properties of the attached eddies at the targeted scale. Our new approach is based on this understanding.

According to the hierarchical distribution of the multi-scale attached eddies in high-Reynolds number wall turbulence (see Fig. 1(bb), also Fig. 14 of Perry & Chong (1982)), τx,L+(yo+)\tau_{x,L}^{{}^{\prime}+}(y_{o}^{+}) represents the superposition contributed from the wall-attached motions with their height larger than yo+y_{o}^{+}. Thus, the difference value Δτx,L+(yo+)=τx,L+(yo+)τx,L+(yo++Δy+)\Delta\tau_{x,L}^{{}^{\prime}+}(y_{o}^{+})=\tau_{x,L}^{{}^{\prime}+}(y_{o}^{+})-\tau_{x,L}^{{}^{\prime}+}(y_{o}^{+}+\Delta y^{+}) can be interpreted as the superposition contribution generated by the wall-attached eddies with their wall-normal heights between yo+y_{o}^{+} and yo++Δy+y_{o}^{+}+\Delta y^{+}. Here, yo++Δy+y_{o}^{+}+\Delta y^{+} is the location of the adjacent wall-normal grid cell of that at yo+y_{o}^{+}, as Δy+\Delta y^{+} is the local grid spacing along the wall-normal direction, in viscous units, and determined by the simulation setups. The similar numerical framework has been verified by our previous study (Cheng & Fu, 2022). Correspondingly, the difference value ΔuW+(yo+)=uW+(yo+)uW+(yo++Δy+)\Delta u_{W}^{{}^{\prime}+}(y_{o}^{+})=u_{W}^{{}^{\prime}+}(y_{o}^{+})-u_{W}^{{}^{\prime}+}(y_{o}^{+}+\Delta y^{+}) is the streamwise velocity fluctuation carried by attached eddies populating the region between yo+y_{o}^{+} and yo++Δy+y_{o}^{+}+\Delta y^{+}. In this way, the SIAs of these eddies can be assessed by

αs(ym)=arctan(ymΔxp),\alpha_{s}(y_{m})=\arctan(\frac{y_{m}}{\Delta x_{p}}), (8)

where ym=yo+(yo+Δy)2y_{m}=\frac{y_{o}+(y_{o}+\Delta y)}{2}, and Δxp\Delta x_{p} is the streamwise delay associated with the peak of the cross correlation

RLW(Δx)=Δτx,L+(x,yo+)ΔuW+(x+Δx,yo+)Δτx,L+2ΔuW+2.R_{LW}(\Delta x)=\frac{\langle\Delta\tau_{x,L}^{{}^{\prime}+}(x,y_{o}^{+})\Delta u_{W}^{{}^{\prime}+}(x+\Delta x,y_{o}^{+})\rangle}{\sqrt{\left\langle\Delta\tau_{x,L}^{{}^{\prime}+2}\right\rangle\left\langle\Delta u_{W}^{{}^{\prime}+2}\right\rangle}}. (9)
Refer to caption
Figure 3: Variations of Δy+\Delta y^{+} as functions of yo+y_{o}^{+} in the logarithmic region for all cases.

As the statistical characteristics of an individual attached eddy being self-similar with its wall-normal height as per the attached-eddy hypothesis (Townsend, 1976), ymy_{m} is just the characteristic scale of the wall-attached motions within yo+y_{o}^{+} and yo++Δy+y_{o}^{+}+\Delta y^{+}. Fig. 3 shows the variations of Δy+\Delta y^{+} as functions of yo+y_{o}^{+} in the logarithmic region for all cases. It can be seen that the maximum values of Δy+\Delta y^{+} are less than 7 in the case Re4200. In this regard, treating ymy_{m} as the mean height of the attached eddies populating the region between yoy_{o} and yo+Δyy_{o}+\Delta y is reasonable, as the zone between yoy_{o} and yo+Δyy_{o}+\Delta y is narrow compared to the spanning of the logarithmic region. The new procedure isolates the attached eddies at a given scale from the rest of the turbulence. The cross correlation, i.e., Eq. (9), gets rid of the influences originated from other scales, and preserves the phase information of the wall-attached motions with wall-normal height ymy_{m}.

At last, the critical assumptions of the present approach and its realization merit a discussion. Our methodology is based on the hierarchical distribution of the attached eddies, and the hypothesis that the characteristic velocity scales carried by the attached eddies with different wall-normal heights are identical with their scale interactions omitted. That’s to say, the attached eddies in each hierarchy contribute equally to the streamwise wall-shear fluctuations on the wall surface and the streamwise turbulence intensity in the lower bound of the logarithmic region. Only in this way, both Δτx,L+\Delta\tau_{x,L}^{{}^{\prime}+} and ΔuW+\Delta u_{W}^{{}^{\prime}+} approximately reflect the characteristics of the attached eddies at ymy_{m}. In fact, these assumptions are also the key elements when developing the attached-eddy model (Townsend, 1976; Perry & Chong, 1982; Woodcock & Marusic, 2015; Yang et al., 2016; Mouri, 2017; Yang & Lozano-Durán, 2017), and some of them may be valid only in high-Reynolds number wall turbulence. For example, the hierarchical distribution of the multi-scale attached eddies is prominent at high-Reynolds number turbulence (De Silva et al., 2016; Marusic & Monty, 2019; Cheng et al., 2019). However, when the DNS data listed in Table 1 are utilized to study the characteristics of the attached eddies, the finite Reynolds-number effects and the intricate scale interactions would take effects inevitably. Besides, the VLSMs, which can not be depicted by the attached-eddy model, would also impose non-trivial impacts (Perry & Marusic, 1995; Hwang et al., 2020; Baars & Marusic, 2020a). Accordingly, the subtraction between uW+(yo+)u_{W}^{{}^{\prime}+}(y_{o}^{+}) and uW+(yo++Δy+)u_{W}^{{}^{\prime}+}(y_{o}^{+}+\Delta y^{+}) can not achieve a sharp cut-off at the targeted scale in the spectral space, and hereby the spectrum of ΔuW+(yo+)\Delta u_{W}^{{}^{\prime}+}(y_{o}^{+}) would be comparatively small but not negligible at the smaller and larger scales of the targeted one. The finiteness of Δy+\Delta y^{+} is another factor, which is worth attention in some scenarios. Due to the limitations of numerical simulation, Δy+\Delta y^{+} is a finitely small quantity. When assessing the SIA of the attached eddies at a given wall-normal height, treating ym+y_{m}^{+} as their characteristic scales (therefore, neglecting the effects of the narrowband between y+y^{+} and y++Δy+y^{+}+\Delta y^{+}) is acceptable, because Δy+\Delta y^{+} is rather small compared to the spanning of the whole logarithmic region. The linear growth of the typical length scales of Δτx,L+\Delta\tau_{x,L}^{{}^{\prime}+} and ΔuW+\Delta u_{W}^{{}^{\prime}+} shown in Fig. 6(bb) can verify this validity. On the other hand, when the spectral characteristics of ΔuW+\Delta u_{W}^{{}^{\prime}+} are considered, ΔuW+\Delta u_{W}^{{}^{\prime}+} should be interpreted as the additive outcomes of the attached eddies with their wall-normal heights within y+y^{+} and y++Δy+y^{+}+\Delta y^{+}, strictly speaking. Under this circumstance, the spectral energy distribution that corresponds to the self-similar attached eddies within this range should be observed to peak around the dominate wavelength and vary continuously and locally. The results shown in Fig. 5 confirm our proposition. Details will be discussed in the following section.

3 Results

Before investigating the SIAs of attached eddies, it is important to study the characteristic scales of Δτx,L\Delta\tau_{x,L}^{{}^{\prime}} and ΔuW\Delta u_{W}^{{}^{\prime}} first. Figs. 4(aa) and 4(bb) show their streamwise premultiplied spectra at yo=0.1hy_{o}=0.1h and yo=0.2hy_{o}=0.2h for Re2000, respectively. The spectra of τx\tau_{x}^{{}^{\prime}} and uu^{\prime} of the full-channel data are also included for comparison. Each spectrum is normalized with its maximum value. It can be seen that the spectra of Δτx,L\Delta\tau_{x,L}^{{}^{\prime}} and ΔuW\Delta u_{W}^{{}^{\prime}} are roughly coincident, and peak at λx=2.1h\lambda_{x}=2.1h for y=0.1hy=0.1h, and λx=4.2h\lambda_{x}=4.2h for y=0.2hy=0.2h, respectively. By contrast, the spectra of τx\tau_{x}^{{}^{\prime}} and uu^{\prime} do not share similar spectral characteristics. It is noted that ΔuW2\Delta u_{W}^{{}^{\prime}2} and Δτx,L2\Delta\tau_{x,L}^{{}^{\prime}2} only account for very little energy of the full-channel signals at the same wall-normal positions. For example, ΔuW2\Delta u_{W}^{{}^{\prime}2} at yo=0.1hy_{o}=0.1h and yo=0.2hy_{o}=0.2h occupies 0.0034%\% and 0.002%\% of u2u^{{}^{\prime}2} at the corresponding positions, respectively, whereas Δτx,L2\Delta\tau_{x,L}^{{}^{\prime}2} for yo=0.1hy_{o}=0.1h and yo=0.2hy_{o}=0.2h occupies 0.012%\% and 0.0045%\% of τx2\tau_{x}^{{}^{\prime}2}, respectively. Moreover, comparing with the spectra of the full-channel data, the spectra of ΔuW\Delta u_{W}^{{}^{\prime}} decay rapidly when λx4h\lambda_{x}\geq 4h (see Figs. 4), which indicates that the effects of VLSMs on ΔuW\Delta u_{W}^{{}^{\prime}} are rather limited.

Fig. 5 shows the streamwise premultiplied spectra of ΔuW\Delta u_{W}^{{}^{\prime}} around yo=0.05hy_{o}=0.05h and yo=0.1hy_{o}=0.1h. Each spectrum is normalized by the energy of ΔuW\Delta u_{W}^{{}^{\prime}} at a given ymy_{m}. Clear plateau regions can be observed around the spectral peaks. For yo=0.05hy_{o}=0.05h, the region is between 18λx/ym3018\leq\lambda_{x}/y_{m}\leq 30, and for yo=0.1hy_{o}=0.1h, it is between 17λx/ym3117\leq\lambda_{x}/y_{m}\leq 31 , which corresponds to the kx1k_{x}^{-1} region in the spectrum predicated by the attached-eddy model, and can be considered as the spectral signatures of the attached eddies (Perry & Chong, 1982; Perry et al., 1986; Hwang et al., 2020; Deshpande et al., 2021). Besides, the spectra shown here resemble the spectrum of the type A eddies hypothesized by Marusic & Perry (1995), i.e., the energy fraction captured by the attached-eddy model. These observations support the proposition that the ΔuW\Delta u_{W}^{{}^{\prime}} signals are the streamwise velocity fluctuations carried by the self-similar attached eddies predominantly. Moreover, they also indicate that the streamwise length scales of the dominant eddies increase with yoy_{o}, as the self-similar range is not altered significantly with increasing yoy_{o}.

Refer to caption
Figure 4: Streamwise premultiplied spectra of Δτx,L\Delta\tau_{x,L}^{{}^{\prime}} , ΔuW\Delta u_{W}^{{}^{\prime}}, τx\tau_{x}^{{}^{\prime}} and uu^{\prime} for (aa) yo=0.1hy_{o}=0.1h and (bb) yo=0.2hy_{o}=0.2h in the case Re2000. Each spectrum is normalized with its maximum value. The vertical dashed lines in (aa) and (bb) are plotted to highlight the corresponding λx/h\lambda_{x}/h of the maximum values of the premultiplied spectra of Δτx,L\Delta\tau_{x,L}^{{}^{\prime}} and ΔuW\Delta u_{W}^{{}^{\prime}}.

To further investigate the scale characteristics of Δτx,L\Delta\tau_{x,L}^{{}^{\prime}} and ΔuW\Delta u_{W}^{{}^{\prime}}, the autocorrelation function of ΔuW,p+\Delta u_{W,p}^{{}^{\prime}+} (the signals that are extracted from the spectral peaks shown in Fig. 5, i.e., filtered ΔuW\Delta u_{W}^{{}^{\prime}} with wavelength larger than 17ym17y_{m}, but smaller than 31ym31y_{m}) is considered, which takes the form of

RΔuW,pΔuW,p(Δx,yo)=ΔuW,p(x,yo,z)ΔuW,p(x+Δx,yo,z)ΔuW,p2(x,yo,z),R_{\Delta u_{W,p}^{{}^{\prime}}\Delta u_{W,p}^{{}^{\prime}}}(\Delta x,y_{o})=\frac{\langle\Delta u_{W,p}^{\prime}\left(x,y_{o},z\right)\Delta u_{W,p}^{\prime}\left(x+\Delta x,y_{o},z\right)\rangle}{\langle\Delta u_{W,p}^{\prime 2}\left(x,y_{o},z\right)\rangle}, (10)

and the counterpart of Δτx,L+\Delta\tau_{x,L}^{{}^{\prime}+} can also be defined similarly. Fig. 6(aa) shows the variations of RΔuW,pΔuW,pR_{\Delta u_{W,p}^{{}^{\prime}}\Delta u_{W,p}^{{}^{\prime}}} as functions of Δx/h\Delta x/h for two selected yoy_{o}. The larger yoy_{o}, the broader the RΔuW,pΔuW,pR_{\Delta u_{W,p}^{{}^{\prime}}\Delta u_{W,p}^{{}^{\prime}}}. As a measure of the typical length scale, we employ Δs/h\Delta s/h, which is the streamwise delay corresponding to RΔuW,pΔuW,p=0.05R_{\Delta u_{W,p}^{{}^{\prime}}\Delta u_{W,p}^{{}^{\prime}}}=0.05 or RΔτx,L,pΔτx,L,p=0.05R_{\Delta\tau_{x,L,p}^{{}^{\prime}}\Delta\tau_{x,L,p}^{{}^{\prime}}}=0.05 (here, 0.05 is an empirical small positive threshold). Fig. 6(bb) shows the variations of 2Δs/h2\Delta s/h as functions of ym/hy_{m}/h for Δτx,L,p+\Delta\tau_{x,L,p}^{{}^{\prime}+} and ΔuW,p+\Delta u_{W,p}^{{}^{\prime}+}. For both Δτx,L,p+\Delta\tau_{x,L,p}^{{}^{\prime}+} and ΔuW,p+\Delta u_{W,p}^{{}^{\prime}+}, 2Δs/h2\Delta s/h increases linearly with ym/hy_{m}/h throughout most of the logarithmic region. This observation is consistent with the attached-eddy hypothesis, which states that the length scales of the attached eddies grow linearly with their wall-normal heights (Hwang, 2015; Marusic & Monty, 2019). Moreover, both the streamwise length scales of Δτx,L,p+\Delta\tau_{x,L,p}^{{}^{\prime}+} and ΔuW,p+\Delta u_{W,p}^{{}^{\prime}+} follow 2Δs=10.8ym2\Delta s=10.8y_{m} (consider the symmetry of the autocorrelation function with respect to Δx=0\Delta x=0, 2Δs2\Delta s truly represents the streamwise length scale of the signals). This scale characteristic agrees well with some previous studies. For example, Baars et al. (2017) showed that the streamwise/wall-normal aspect ratio of the wall-attached eddy structure is λx/y=14\lambda_{x}/y=14 in turbulent boundary layers, which is close to the result here. Hwang et al. (2020) reported that the spectra of the self-similar wall-attached structures agree with the attached-eddy hypothesis at λx=12y\lambda_{x}=12y, which is consistent with the estimation of the present study. All these observations indicate that Δτx,L+\Delta\tau_{x,L}^{{}^{\prime}+} and ΔuW+\Delta u_{W}^{{}^{\prime}+} are representative of the attached eddies at a certain wall-normal height, though the minor influences of VLSMs still exist, and treating ym+y_{m}^{+} as their characteristic scales is reasonable.

Refer to caption
Figure 5: Premultiplied one-dimensional streamwise spectra of ΔuW\Delta u_{W}^{{}^{\prime}} around (aa) yo=0.05hy_{o}=0.05h; (bb) yo=0.1hy_{o}=0.1h in Re2000. The horizontal dashed lines represent the plateaus or peaks of the spectra. The vertical lines are plotted to highlight the self-similar regions of each spectrum.
Refer to caption
Figure 6: (aa) Variations of RΔuW,pΔuW,pR_{\Delta u_{W,p}^{{}^{\prime}}\Delta u_{W,p}^{{}^{\prime}}} as functions of Δx/h\Delta x/h for two selected yoy_{o}; (bb) variations of Δs/h\Delta s/h as functions of ym+y_{m}^{+} for Δτx,L,p+\Delta\tau_{x,L,p}^{{}^{\prime}+} and ΔuW,p+\Delta u_{W,p}^{{}^{\prime}+}. The line in (bb) denotes the linear variation 2Δs=10.8ym2\Delta s=10.8y_{m}.

In summary, all the observations mentioned above indicate that Δτx,L\Delta\tau_{x,L}^{{}^{\prime}} and ΔuW\Delta u_{W}^{{}^{\prime}} are the outcomes of the energy-containing motions with the wall-normal heights approximately equal to ymy_{m}, and the cross correlation, i.e., Eq. (9), truly reflects the phase difference between the streamwise velocity fluctuations carried by these motions and their footprints in the near-wall region. Other wall-normal positions and DNS cases yield similar results and are not shown here for brevity.

Refer to caption
Figure 7: (aa) Variations of RLWR_{LW}, i.e., the cross correlation between Δτx,L+(yo+)\Delta\tau_{x,L}^{{}^{\prime}+}(y_{o}^{+}) and ΔuW+(yo+)\Delta u_{W}^{{}^{\prime}+}(y_{o}^{+}), as functions of Δx\Delta x for some selected yoy_{o} in the case Re2000; (bb) variations of the normalized RLWR_{LW} as functions of Δx/ym\Delta x/y_{m} for some selected yoy_{o} in the case Re2000. The RLWR_{LW} profiles are normalized with their maximum values in (bb). The vertical dashed lines in (aa) are plotted to highlight the maximum values of RLWR_{LW} and their corresponding Δx/h\Delta_{x}/h.

Fig. 7(aa) shows the variations of RLWR_{LW} as functions of the streamwise delay for some selected wall-normal positions in the case Re2000. Since the streamwise length scales of the energy-containing motions are increased with their normal heights (see Fig. 4), RLWR_{LW} becomes wider about the peak with increasing yoy_{o}. Δxp\Delta x_{p} can be identified obviously from the cross-correlation profiles, and the SIAs of the attached eddies at a given wall-normal height can be calculated according to Eq. (8). Fig. 7(bb) plots the variations of the normalized RLWR_{LW} as functions of Δx/ym\Delta x/y_{m} for some selected yoy_{o} in the case Re2000. The RLWR_{LW} distributions are normalized with their maximum values RLW,maxR_{LW,max}. It can be seen that the profiles of RLW/RLW,maxR_{LW}/R_{LW,max} for different wall-normal heights coincide well with each other, which indicates the self-similar characteristics of the energy-containing motions in the logarithmic region. We have checked that the correlations calculated from the raw data, i.e., RτxuR_{\tau_{x}^{\prime}u^{\prime}} in Eq. (1) can not coincide if normalized in this manner. Again, it demonstrates that the new methodology is capable of capturing the main properties of the attached eddies.

Fig. 8 plots the variations of αs\alpha_{s} as functions of ym+y_{m}^{+} for all cases. αs\alpha_{s} increases approximately from 2727^{\circ} for Re550, to 4040^{\circ} for Re4200. For a given case, αs\alpha_{s} changes little spanning the logarithmic region except for the upper part of logarithmic region in Re4200. Deshpande et al. (2019) isolated the large wall-attached structures in a DNS of turbulent boundary layer at Reτ2000Re_{\tau}\approx 2000, and found the corresponding SIAs to be 3232^{\circ} (see Fig. 4(aa) of their paper). Their observation is consistent with the results of the present study. However, Deshpande et al. (2019) only calculated the SIAs of the largest wall-attached motions in the logarithmic region due to the limitation of the methodology adopted in their study, whereas we make a thorough investigation on the SIAs of attached eddies with any wall-normal heights in the logarithmic region. Moreover, Deshpande et al. (2019) reported that the SIAs of the large wall-attached motions identified in a wind-tunnel boundary layer with Reτ=14000Re_{\tau}=14000 are approximately 5050^{\circ}. They ascribed the result difference between DNS and experiment to the limited streamwise scale range owing to the DNS domain size selected for analysis. Our results reveal that the Reynolds number effects play a non-negligible role in the formation of SIAs of attached eddies. To the authors’ knowledge, this is the first time that the Reynolds-number dependence of SIAs of the wall-attached motions at a given length scale has been clearly shown. At last, it should be noted that αs\alpha_{s} of Re4200 decreases rapidly for ym+>500y_{m}^{+}>500 (not shown here). This diversity is due to the small computational domain size along the streamwise direction in this database. Thus, in the discussion below, the statistics of αs\alpha_{s} in the range of ym+>500y_{m}^{+}>500 in Re4200 will not be taken into account. The sensitivity of the presented results to the number of instantaneous flow fields employed for accumulating statistics is examined in the Appendix A.

Refer to caption
Figure 8: αs\alpha_{s} as functions of ym+y_{m}^{+} for all cases, and the red dashed lines denote the mean αs\alpha_{s} across the logarithmic region of each case.
Refer to caption
Figure 9: (aa) Variations of the mean αs\alpha_{s} (αs,m\alpha_{s,m}) statistic in the range of logarithmic region as a function of the friction Reynolds number, and the experimental results of turbulent boundary layers (Deshpande et al., 2019) are also included for comparison; (bb) αm\alpha_{m} and αSSE,m\alpha_{SSE,m} as a function of yo+y_{o}^{+} for Re2000. The solid black line in (aa) denotes the theoretical prediction angle 4545^{\circ}, and the dashed lines in (aa) indicates the asymptotic behavior of αs,m\alpha_{s,m}.

Fig. 9(aa) shows the mean αs\alpha_{s} (αs,m\alpha_{s,m}) distribution in the range of logarithmic region as a function of the friction Reynolds number. It can be seen that the SIA may reach the theoretical prediction angle 4545^{\circ} (Perry et al., 1992) when ReτO(104)Re_{\tau}\sim O(10^{4}). The results of DNS of a turbulent boundary layer and wind-tunnel experiment of Deshpande et al. (2019) are roughly agreed with the tendency. The minor differences may result from the distinct configurations of the wall-bounded turbulence.

4 Disscussion

4.1 Effects of near-wall and detached motions

To clarify the effects of near-wall and detached motions on the SIA assessment, we calculate the mean SIA based on the predictive signals, i.e.,

αSSE,m=arctan(yoΔxp),\alpha_{SSE,m}=\arctan(\frac{y_{o}}{\Delta x_{p}}), (11)

where Δxp\Delta x_{p} is the streamwise delay associated with the peak of the following cross correlation

Rτx,LuW(Δx)=τx,L(x)uW(x+Δx,yo)τx,L2uW2.R_{\tau_{x,L}^{\prime}u_{W}^{\prime}}(\Delta x)=\frac{\langle\tau_{x,L}^{{}^{\prime}}(x)u_{W}^{\prime}(x+\Delta x,y_{o})\rangle}{\sqrt{\left\langle\tau_{x,L}^{{}^{\prime}2}\right\rangle\left\langle u_{W}^{{}^{\prime}2}\right\rangle}}. (12)

Fig. 9(bb) shows the variations of αSSE,m\alpha_{SSE,m} as a function of yo+y_{o}^{+} for Re2000, and the statistics of αm\alpha_{m} are also included for comparison. We can see that αSSE,m\alpha_{SSE,m} distribution is very closed to that of αm\alpha_{m}. It highlights the fact that the phase information embedded in the raw signals u(yo+)u^{\prime}(y_{o}^{+}) and τx\tau_{x}^{\prime} is preserved by SSE. It also suggests that the near-wall and wall-detached motions, which can not be captured by SSE, have a negligible impact on the magnitudes of SIA.

4.2 αs\alpha_{s} versus αm\alpha_{m}

Reviewing the approach to obtain the αm\alpha_{m} (i.e., Eq. (1)-(2)), the proposition that αm\alpha_{m} being the mean SIA of attached eddies manifests in three aspects: (11) the generation of τx\tau_{x}^{\prime} is not only the outcome of the near-wall motions, but also the footprints of all the wall-attached eddies (Cho et al., 2018; Cheng et al., 2020a); (22) uu^{\prime} in logarithmic region results from a sum of random contributions from the wall-attached eddies with distinct characteristic length scales (Yang et al., 2016), and a portion of contributions from the wall-detached eddies (Baars & Marusic, 2020b); (33) yoy_{o} is a wall-normal position located in the logarithmic region and chosen arbitrarily. As mentioned above, an array of wall-attached eddies with distinct wall-normal heights can simultaneously convect past this reference position.

Here, an additive SIA is calculated to highlight the relationship between αs\alpha_{s} and αm\alpha_{m}, namely,

αadd=arctan(ysΔxp),\alpha_{add}=\arctan(\frac{y_{s}}{\Delta x_{p}}), (13)

where ys+=100y_{s}^{+}=100 is the lower boundary of logarithmic region, and Δxp\Delta x_{p} is the streamwise delay associated with the peak of the following cross correlation, i.e.,

Radd(Δx)=(τx,L+(x,ys+)τx,L+(x,yo+))(uW+(x+Δx,ys+)uW+(x+Δx,yo+))(τx,L+(x,ys+)τx,L+(x,yo+))2(uW+(x,ys+)uW+(x,yo+))2,R_{add}(\Delta x)=\frac{\langle(\tau_{x,L}^{{}^{\prime}+}(x,y_{s}^{+})-\tau_{x,L}^{{}^{\prime}+}(x,y_{o}^{+}))(u_{W}^{{}^{\prime}+}(x+\Delta x,y_{s}^{+})-u_{W}^{{}^{\prime}+}(x+\Delta x,y_{o}^{+}))\rangle}{\sqrt{\left\langle(\tau_{x,L}^{{}^{\prime}+}(x,y_{s}^{+})-\tau_{x,L}^{{}^{\prime}+}(x,y_{o}^{+}))^{2}\right\rangle\left\langle(u_{W}^{{}^{\prime}+}(x,y_{s}^{+})-u_{W}^{{}^{\prime}+}(x,y_{o}^{+}))^{2}\right\rangle}}, (14)

where the reference position yo+y_{o}^{+} varies from ys++Δy+y_{s}^{+}+\Delta y^{+} (equals to 104) to 0.7h+0.7h^{+}. Fig. 10(aa) shows the variations of αadd\alpha_{add} as a function of yo+y_{o}^{+} for Re2000. It can be seen that αadd\alpha_{add} decreases from 37.837.8^{\circ} to 1414^{\circ} as yo+y_{o}^{+} increases, which corresponds to αs(ym+=102)\alpha_{s}(y_{m}^{+}=102) and αm(yo+=100)\alpha_{m}(y_{o}^{+}=100), respectively. In other words, αadd\alpha_{add} converges from the SIAs of attached eddies with wall-normal height approximately 100100 in viscous units to the mean SIA at yo+=100y_{o}^{+}=100. This observation can be explained through the prism of the hierarchical attached eddies in high-Reynolds number wall turbulence. The increase of yo+y_{o}^{+} indicates that τx,L+(ys+)τx,L+(yo+)\tau_{x,L}^{{}^{\prime}+}(y_{s}^{+})-\tau_{x,L}^{{}^{\prime}+}(y_{o}^{+}) and uW+(ys+)uW+(yo+)u_{W}^{{}^{\prime}+}(y_{s}^{+})-u_{W}^{{}^{\prime}+}(y_{o}^{+}) are contributed by more and more wall-attached eddies with their normal heights larger than ys+y_{s}^{+}, and gradually become equal to τx,L+(ys+)\tau_{x,L}^{{}^{\prime}+}(y_{s}^{+}) and uW+(ys+)u_{W}^{{}^{\prime}+}(y_{s}^{+}), respectively, when yo+y_{o}^{+} approaches h+h^{+}. Thus, RaddR_{add} would also gradually converge to Rτx,LuWR_{\tau_{x,L}^{\prime}u_{W}^{\prime}} in Eq. (12), and αadd\alpha_{add} converges to αm\alpha_{m} and αSSE,m\alpha_{SSE,m} concurrently.

Refer to caption
Figure 10: (aa) Variations of the additive SIA αadd\alpha_{add} as a function of yo+y_{o}^{+} for Re2000; (bb) the mean SIAs αm\alpha_{m} as functions of yo+y_{o}^{+} for all cases.

Additionally, this study helps to understand the variation tendency of αm\alpha_{m}. Fig. 10(bb) plots the variations of αm\alpha_{m} for all cases. It is clearly observed that αm\alpha_{m} increases continuously with yo+y_{o}^{+}. Taking Re2000 as an example, αm\alpha_{m} increases from 1414^{\circ} for ys+y_{s}^{+} to 15.315.3^{\circ} for ye+y_{e}^{+}. Increasing yo+y_{o}^{+} implies that fewer and fewer wall-attached eddies contribute to uu^{\prime}. In this way, αm\alpha_{m} would converge to αs\alpha_{s} as yo+y_{o}^{+} increases, albeit more slowly.

4.3 Scale-dependent inclination angles of wall-attached eddies

An alternative approach for calculating the scale-dependent inclination angle (SDIA) has been reported by Baars et al. (2016). The following are the primary processes and outcomes. The scale-specific phase between uu^{\prime} at y+y^{+} and yo+y_{o}^{+} can be estimated as

Φ(λx)=arctan{Im[ϕuou(λx,y+,yo+)]Re[ϕuou(λx,y+,yo+)]},\Phi\left(\lambda_{x}\right)=\arctan\left\{\frac{\operatorname{Im}\left[\phi_{u_{o}^{\prime}u^{\prime}}\left(\lambda_{x},y^{+},y_{o}^{+}\right)\right]}{\operatorname{Re}\left[\phi_{u_{o}^{\prime}u^{\prime}}\left(\lambda_{x},y^{+},y_{o}^{+}\right)\right]}\right\}, (15)

where Im(\cdot) and Re(\cdot) denote the imaginary and real parts of ϕuou\phi_{u_{o}^{\prime}u^{\prime}}, namely, the numerator of Eq. (4). The scale-dependent streamwise shift can be calculated as

l(λx)=Φ(λx)λx2π.l(\lambda_{x})=\frac{\Phi\left(\lambda_{x}\right)\lambda_{x}}{2\pi}. (16)

Accordingly, the SDIA can be estimated as

αsd(λx)=arctan(yoyl(λx)).\alpha_{sd}(\lambda_{x})=\arctan(\frac{y_{o}-y}{l(\lambda_{x})}). (17)

A positive αsd\alpha_{sd} value corresponds to a spatially forward-leaning structure.

Refer to caption
Figure 11: Variations of the scale-dependent inclination angles for three selected wall-normal positions in the case Re2000. The vertical line denotes λx/yo=14\lambda_{x}/y_{o}=14.

Fig. 11 shows the SDIAs as functions of λx/yo\lambda_{x}/y_{o} for three selected wall-normal positions in the case Re2000. For λx/yo>18\lambda_{x}/y_{o}>18, the SDIAs of the large-scale motions are shown to be approximately equal to 1414^{\circ} (in fact, this is not the real SIA of the large-scale wall-attached structures, according to the study of Deshpande et al. (2019)). However, for the smaller length scales, the SDIAs tend to be negative and vary rapidly with λx/yo\lambda_{x}/y_{o}. This is the range of self-similar structures reported by previous studies, especially those with λx/yo=14\lambda_{x}/y_{o}=14 (Baars et al., 2017; Baidya et al., 2019). Similar results have also been reported by Baars et al. (2016) (see Fig. 5 of their paper). It indicates that the phase spectrum shown in Fig. 11 cannot be interpreted with any physical relevance at these scales, as the scale-specific phases of them are random indeed. The contamination from the detached eddies with random orientations could be the source of this problem. This is the main purpose of the present study, i.e., to eliminate the corruption caused by the wall-detached motions and appropriately measure the SIAs of the wall-attached eddies at a certain wall-normal height.

5 Concluding remarks

In the present study, we develop a methodology to assess the streamwise inclination angles of the wall-attached eddies at a given wall-normal height in turbulent channel flows, by coupling the spectral stochastic estimation with the attached-eddy hypothesis. Our results show, for the first time, that the SIAs of the attached eddies are Reynolds-number dependent in low and medium Reynolds numbers and tend to be consistent with the theoretical prediction (i.e., αs=45\alpha_{s}=45^{\circ}) as Reynolds number increased. We further reveal that the mean SIA reported by vast previous studies are the outcomes of the additive effect contributed by multi-scale attached eddies.

The attached-eddy model has been the guidance for the reconstruction of the velocity field in wall turbulence (Perry & Marusic, 1995; Chandran et al., 2017; Baidya et al., 2017). Hierarchical vortex packets which consist of Λ\Lambda-vortexes with αs=45\alpha_{s}=45^{\circ} are distributed on the wall surface to mimic the attached eddies. The present results suggest that a lower SIA of representative structures might be helpful for a more accurate reconstruction when the Reynolds number is not high enough. Moreover, within the state-of-the-art wall-modelled large-eddy simulation (WMLES) framework, one may estimate the instantaneous τx\tau_{x} based on the velocities carried by the log-region eddies (Fu et al., 2021, 2022). The Reynolds-number dependence of SIAs of these eddies should be accounted for by an advanced model in this sense.

Acknowledgments

L.F. acknowledges the fund from CORE as a joint research center for ocean research between QNLM and HKUST, and the fund from Guangdong Basic and Applied Basic Research Foundation (No. 2022A1515011779). We would like to thank Professor Jiménez for making the DNS data available. We also express our gratitude to the reviewers of this paper for their kind and constructive comments.

Declaration of interests

The authors report no conflict of interest.

Appendix A. Statistic sensitivity to NFN_{F}

Refer to caption
Figure 12: αs\alpha_{s} as functions of ym+y_{m}^{+} for the cases Re2000 and Re4200 with different NFN_{F}. The dashed lines denote the mean value of αs\alpha_{s} in the logarithmic region.

The influences of the number of instantaneous flow fields for accumulating statistics are examined. Fig. 12 shows the effect of NFN_{F} on the statistic αs\alpha_{s} for the cases Re2000 and Re4200. Alteration of the statistical samples mainly affects the relative standard deviations (RSD) of the results. To be specific, when NFN_{F} increases from 4848 to 9494, RSD decreases from 3.9%3.9\% to 3.3%3.3\% for Re2000; but for Re4200, RSD decreases from 6.5%6.5\% to 3.7%3.7\% when NFN_{F} increases from 2020 to 4040. Given the fact that the case Re4200 has limited domain size, raising NFN_{F} can effectively reduce the wiggles in the outputs. Nevertheless, the mean value of αs\alpha_{s} in the logarithmic region seems to be insensitive to NFN_{F}.

References

  • Adrian (1979) Adrian, R.J. 1979 Conditional eddies in isotropic turbulence. Phys. Fluids 22 (11), 2065–2070.
  • Adrian et al. (2000) Adrian, R.J., Meinhart, C.D. & Tomkins, C.D. 2000 Vortex organization in the outer region of the turbulent boundary layer. J. Fluid Mech. 422, 1–54.
  • Baars et al. (2017) Baars, W.J., Hutchins, N. & Marusic, I. 2017 Self-similarity of wall-attached turbulence in boundary layers. J. Fluid Mech. 823, R2.
  • Baars & Marusic (2020a) Baars, W.J. & Marusic, I. 2020a Data-driven decomposition of the streamwise turbulence kinetic energy in boundary layers. part 1. energy spectra. J. Fluid Mech. 882, A25.
  • Baars & Marusic (2020b) Baars, W.J. & Marusic, I. 2020b Data-driven decomposition of the streamwise turbulence kinetic energy in boundary layers. part 2. integrated energy and a1a_{1}. J. Fluid Mech. 882, A26.
  • Baars et al. (2016) Baars, W. J, Hutchins, N. & Marusic, I. 2016 Spectral stochastic estimation of high-Reynolds-number wall-bounded turbulence for a refined inner-outer interaction model. Phys. Rev. Fluids 1 (5), 054406.
  • Baidya et al. (2019) Baidya, R., Baars, W. J., Zimmerman, S., Samie, M., Hearst, R. J., Dogan, E., Mascotelli, L., Zheng, X., Bellani, G., Talamelli, A. & et al. 2019 Simultaneous skin friction and velocity measurements in high Reynolds number pipe and boundary layer flows. J. Fluid Mech. 871, 377–400.
  • Baidya et al. (2017) Baidya, R., Philip, J., Hutchins, N., Monty, J.P. & Marusic, I. 2017 Distance-from-the-wall scaling of turbulent motions in wall-bounded flows. Phys. Fluids 29 (2), 020712.
  • Boppe et al. (1999) Boppe, R.S., Neu, W.L. & Shuai, H. 1999 Large-scale motions in the marine atmospheric surface layer. Boundary-layer meteorology 92 (2), 165–183.
  • Brown & Thomas (1977) Brown, G.L. & Thomas, A.S. 1977 Large structure in a turbulent boundary layer. Phys. Fluids 20 (10), S243–S252.
  • Carper & Porté-Agel (2004) Carper, M.A. & Porté-Agel, F. 2004 The role of coherent structures in subfilter-scale dissipation of turbulence measured in the atmospheric surface layer. J. Turbul. 5 (1), 32–55.
  • Chandran et al. (2017) Chandran, D., Baidya, R., Monty, J.P. & Marusic, I. 2017 Two-dimensional energy spectra in high-Reynolds-number turbulent boundary layers. J. Fluid Mech. 826, R1.
  • Cheng & Fu (2022) Cheng, C. & Fu, L. 2022 Consistency between the attached eddy model and the inner outer interaction model: a study of streamwise wall shear stress fluctuations in a turbulent channel flow. J. Fluid Mech. 942, R9.
  • Cheng et al. (2019) Cheng, C., Li, W., Lozano-Durán, A. & Liu, H. 2019 Identity of attached eddies in turbulent channel flows with bidimensional empirical mode decomposition. J. Fluid Mech 870, 1037–1071.
  • Cheng et al. (2020a) Cheng, C., Li, W., Lozano-Durán, A. & Liu, H. 2020a On the structure of streamwise wall-shear stress fluctuations in turbulent channel flows. J. Fluid Mech. 903, A29.
  • Cheng et al. (2020b) Cheng, C., Li, W., Lozano-Durán, A. & Liu, H. 2020b Uncovering townsend wall-attached eddies in low-reynolds-number wall turbulence. J. Fluid Mech. 889, A29.
  • Cho et al. (2018) Cho, M., Hwang, Y. & Choi, H. 2018 Scale interactions and spectral energy transfer in turbulent channel flow. J. Fluid Mech. 854, 474–504.
  • Christensen & Adrian (2001) Christensen, K.T. & Adrian, R.J. 2001 Statistical evidence of hairpin vortex packets in wall turbulence. J. Fluid Mech. 431, 433–443.
  • De Silva et al. (2016) De Silva, C.M., Marusic, I. & Hutchins, N. 2016 Uniform momentum zones in turbulent boundary layers. J. Fluid Mech. 786, 309–331.
  • Del Álamo & Jiménez (2003) Del Álamo, J. C. & Jiménez, J. 2003 Spectra of the very large anisotropic scales in turbulent channels. Phys. Fluids 15 (6), L41–L44.
  • Del Álamo et al. (2004) Del Álamo, J. C., Jiménez, J., Zandonade, P. & Moser, R.D. 2004 Scaling of the energy spectra of turbulent channels. J. Fluid Mech. 500, 135–144.
  • Deshpande et al. (2021) Deshpande, R., Monty, J.P. & Marusic, I. 2021 Active and inactive components of the streamwise velocity in wall-bounded turbulence. J. Fluid Mech. 914, A5.
  • Deshpande et al. (2019) Deshpande, R., Monty, Jason P. & Marusic, I. 2019 Streamwise inclination angle of large wall-attached structures in turbulent boundary layers. J. Fluid Mech. 877, R4.
  • Fu et al. (2022) Fu, L., Bose, S. & Moin, P. 2022 Prediction of aerothermal characteristics of a generic hypersonic inlet flow. Theor. Comput. Fluid Dyn. 36 (2), 345–368.
  • Fu et al. (2021) Fu, L., Karp, M., Bose, S.T., Moin, P. & Urzay, J. 2021 Shock-induced heating and transition to turbulence in a hypersonic boundary layer. J. Fluid Mech. 909, A8.
  • Hoyas & Jiménez (2006) Hoyas, S. & Jiménez, J. 2006 Scaling of the velocity fluctuations in turbulent channels up to 𝑅𝑒τ=2003\mathit{Re}_{{\it\tau}}=2003. Phys. Fluids 18 (1), 011702.
  • Hu et al. (2020) Hu, R., Yang, X.I. A. & Zheng, X. 2020 Wall-attached and wall-detached eddies in wall-bounded turbulent flows. J. Fluid Mech. 885, A30.
  • Hwang et al. (2020) Hwang, J., Lee, J. & Sung, H. 2020 Statistical behaviour of self-similar structures in canonical wall turbulence. J. Fluid Mech. 905, A6.
  • Hwang & Sung (2018) Hwang, J. & Sung, H.J. 2018 Wall-attached structures of velocity fluctuations in a turbulent boundary layer. J. Fluid Mech. 856, 958–983.
  • Hwang (2015) Hwang, Y. 2015 Statistical structure of self-sustaining attached eddies in turbulent channel flow. J. Fluid Mech. 767, 254–289.
  • Jiménez (2018) Jiménez, J. 2018 Coherent structures in wall-bounded turbulence. J. Fluid Mech. 842, P1.
  • Kovasznay et al. (1970) Kovasznay, L.S.G., Kibens, V. & Blackwelder, R.F. 1970 Large-scale motion in the intermittent region of a turbulent boundary layer. J Fluid Mech 41 (2), 283–325.
  • Lozano-Durán & Jiménez (2014) Lozano-Durán, A. & Jiménez, J. 2014 Effect of the computational domain on direct simulations of turbulent channels up to 𝑅𝑒τ=4200\mathit{Re}_{{\it\tau}}=4200. Phys. Fluids 26 (1), 011702.
  • Marusic (2001) Marusic, I. 2001 On the role of large-scale structures in wall turbulence. Phys. Fluids 13 (3), 735–743.
  • Marusic & Heuer (2007) Marusic, I. & Heuer, W.D.C. 2007 Reynolds number invariance of the structure inclination angle in wall turbulence. Phys. Rev. Lett. 99 (11), 114504.
  • Marusic et al. (2010) Marusic, I., Mathis, R. & Hutchins, N. 2010 Predictive model for wall-bounded turbulent flow. Science 329 (5988), 193–196.
  • Marusic & Monty (2019) Marusic, I. & Monty, J.P. 2019 Attached eddy model of wall turbulence. Annu. Rev. Fluid Mech. 51, 49–74.
  • Marusic et al. (2013) Marusic, I., Monty, J.P., Hultmark, M. & Smits, A.J. 2013 On the logarithmic region in wall turbulence. J. Fluid Mech. 716, R3.
  • Marusic & Perry (1995) Marusic, I. & Perry, A.E. 1995 A wall-wake model for the turbulence structure of boundary layers. part 2. further experimental support. J. Fluid Mech. 298, 389–407.
  • Moin & Kim (1985) Moin, P. & Kim, J. 1985 The structure of the vorticity field in turbulent channel flow. part 1. analysis of instantaneous fields and statistical correlations. J. Fluid Mech. 155, 441–464.
  • Mouri (2017) Mouri, H. 2017 Two-point correlation in wall turbulence according to the attached-eddy hypothesis. J. Fluid Mech. 821, 343–357.
  • Perry et al. (1992) Perry, A.E., Uddin, A.K. M. & Marusic, I. 1992 An experimental and computational study on the orientation of attached eddies in turbulent boundary layers. In Proceedings of the 11th Australasian Fluid Mechanics Conference, Hobart, Australia. .
  • Perry & Chong (1982) Perry, A. E. & Chong, M. S 1982 On the mechanism of wall turbulence. J. Fluid Mech. 119 (119), 173–217.
  • Perry et al. (1986) Perry, A. E., Henbest, S. & Chong, M. S. 1986 A theoretical and experimental study of wall turbulence. J. Fluid Mech. 165, 163–199.
  • Perry & Marusic (1995) Perry, A. E. & Marusic, I 1995 A wall-wake model for the turbulence structure of boundary layers. part 1. extension of the attached eddy hypothesis. J. Fluid Mech. 298 (298), 361–388.
  • Townsend (1976) Townsend, A. A. 1976 The structure of turbulent shear flow, 2nd edn. Cambridge University Press.
  • Wang et al. (2021) Wang, L., Hu, R. & Zheng, X. 2021 A scaling improved inner–outer decomposition of near-wall turbulent motions. Physics of Fluids 33 (4), 045120.
  • Woodcock & Marusic (2015) Woodcock, J. D. & Marusic, I. 2015 The statistical behaviour of attached eddies. Phys. Fluids 27 (1), 97–120.
  • Yang & Lozano-Durán (2017) Yang, X.I.A. & Lozano-Durán, A. 2017 A multifractal model for the momentum transfer process in wall-bounded flows. J. Fluid Mech. 824, R2.
  • Yang et al. (2016) Yang, X.I. A., Marusic, I. & Meneveau, C. 2016 Moment generating functions and scaling laws in the inertial layer of turbulent wall-bounded flows. J Fluid Mech 791, R2.
  • Yoon et al. (2020) Yoon, M., Hwang, J., Yang, J. & Sung, H.J. 2020 Wall-attached structures of streamwise velocity fluctuations in an adverse-pressure-gradient turbulent boundary layer. J. Fluid Mech. 885, A12.