# Convergence of numerical simulations of turbulent wall-bounded flows and mean cross-flow structure of rectangular ducts

- 809 Downloads
- 17 Citations

## Abstract

Convergence criteria for direct numerical simulations of turbulent channel and duct flows are proposed. The convergence indicator for channels is defined as the deviation of the nondimensional total shear-stress profile with respect to a linear profile, whereas the one for the duct is based on a nondimensional streamwise momentum balance at the duct centerplane. We identify the starting (\(T_{S}\)) and averaging times (\(T_{A}\)) necessary to obtain sufficiently converged statistics, and also find that optimum convergence rates are achieved when the spacing in time between individual realizations is below \(\Delta t^{+}=17\). The in-plane structure of the flow in turbulent ducts is also assessed by analyzing square ducts at \(Re_{\tau ,c} \simeq 180\) and 360 and rectangular ducts with aspect ratios 3 and 10 at \(Re_{\tau ,c} \simeq 180\). Identification of coherent vortices shows that near-wall streaks are located in all the duct cases at a wall-normal distance of \(y^{+} \simeq 40\) as in Pinelli et al. (J Fluid Mech 644:107–122, 2010). We also find that large-scale motions play a crucial role in the streamline pattern of the secondary flow, whereas near-wall structures highly influence the streamwise vorticity pattern. These conclusions extend the findings by Pinelli et al. to other kinds of large-scale motions in the flow through the consideration of wider ducts. They also highlight the complex and multiscale nature of the secondary flow of second kind in turbulent duct flows.

## Keywords

Wall-bounded turbulence Direct numerical simulation Convergence Secondary flow Turbulent structures## 1 Introduction

Numerical simulations have become, together with new experimental techniques, the key to understanding some of the most intriguing aspects of wall-bounded turbulence. Since the well-known work on channel flows by Kim et al. [1] in the late 1980s, the increase of computational power and the development of highly scalable numerical algorithms has allowed the computation of increasingly higher Reynolds numbers, as well as more complicated geometries. Some of the most relevant direct numerical simulations (DNSs) of wall-bounded turbulence are the channel flows computed by del Álamo et al. [2], Lozano-Durán and Jiménez [3] and Lee and Moser [4] (up to friction Reynolds numbers of \(Re_{\tau } \simeq 2000, \simeq 4200\) and \(\simeq 5200\) respectively), the ZPG boundary layers by Schlatter and Örlü [5] and Sillero et al. [6] (up to \(Re_{\tau }\) values of \(\simeq 1000\) and \(\simeq 2000\) respectively), as well as the pipe flows by Wu and Moin [7] and El Khoury et al. [8] (with a maximum \(Re_{\tau }\) of \(\simeq 1000\) in both cases). Note that the friction Reynolds number is defined in terms of the length scale *h* (which is the channel half-height, the pipe radius or the boundary-layer thickness) and the friction velocity \(u_{\tau }=\sqrt{\tau _{w} / \rho }\) (where \(\tau _{w}\) is the wall-shear stress and \(\rho\) is the fluid density). These numerical experiments have helped to understand the buffer sublayer, and now start to shed light on the dynamics of the log layer and the outer-layer structures.

Most experimental studies of wall-bounded turbulence provide detailed descriptions of the measurement techniques and the experimental setup employed during their research. For example, Österlund [9] elaborates on the design of the wind tunnel used in his work (the MTL wind tunnel at KTH), he provides extensive descriptions of the instrumentation he used (probe calibration, sampling time\(\ldots\)) and he describes the different trip designs considered for tripping the flow under study. Despite the wealth of descriptions of experimental setups available in the literature, physical experiments are thoroughly scrutinized before they are employed to validate scaling laws or theories. As discussed by Nagib et al. [10] and Chauhan et al. [11], the tripping device employed to trigger transition to turbulence may play an important role in the development of a boundary layer, leading to underdeveloped flows if not done properly. This was also observed recently by Vinuesa et al. [12] after carefully assessing the inflow conditions of numerical simulations and comparing with experimental data. Other factors that highly influence experimental studies of wall-bounded turbulence are the necessity of adequate corrections to the probe measurements, discussed in detail in Ref. [13], or the relation between the probe size and the smallest turbulent scales, which may lead to a contamination of the near-wall measurements if the probe is not small enough [14]. The latter aspect has motivated the construction of the experimental facility CICLoPE at the University of Bologna (Italy), in which the size of the smallest turbulent scales is increased by developing a larger experimental facility [15]. The issue of the averaging time required to obtain converged turbulence statistics in turbulent-boundary-layer experiments was addressed by Klewicki and Falco [16]. In their study, they obtained cumulative estimates of statistics of a number of observables, including velocity and vorticity components, double products and time derivatives. They also assessed the necessary averaging times in different parts of the boundary layer, considering the effects of shear, intermittency and near-wall dynamics. They concluded that in order to obtain converged turbulence statistics up to the fourth moment it is necessary to average for at least 6000 convective time units (defined as the ratio of the boundary-layer thickness \(\delta\) and the freestream velocity \(U_{\infty }\)). Antonia et al. [17] provided a compilation of empirical relations to estimate the required averaging time for a particular level of convergence in turbulent jets. More recent experimental studies [18] have reported longer averaging periods of around 25,000 convective time units used to obtain converged turbulence statistics.

On the other hand, and as discussed by Schlatter and Örlü [5], the DNS data available in the literature are hardly scrutinized. Interestingly, these data show dispersions of up to 5 % in the shape factor \(H=\delta ^{*}/\theta\) (where \(\delta ^{*}\) and \(\theta\) are the displacement and momentum thicknesses respectively), and up to 20 % in skin friction. Aspects which are barely mentioned in most numerical studies, such as the numerical mechanism used to trigger transition to turbulence, can produce important differences in the computed results. Schlatter and Örlü [19] analyzed the downstream evolution of several integral, mean and fluctuating properties of simulated ZPG turbulent boundary layers, and showed that different inflow conditions and tripping mechanisms explain most of the discrepancies between the various low-*Re* DNS databases. Another characteristic that is not described in detail in the literature and significantly influences the results of a numerical simulation is convergence. Most numerical studies devote, at most, one or two lines to explain how the convergence of their statistics was assessed. A notable exception is the work by Oliver et al. [20], where the authors address the problem of statistical convergence of DNS in a systematic way. The article points out that the traditional mesh size sensitivity study using Richardson extrapolation should not be performed for the DNS analyses of turbulent flows, because of the presence of sampling errors. This may result in the discretization error not decreasing exponentially with progressively finer mesh sizes. To overcome this obstacle the authors propose a new approach which takes into account the inaccuracies in both sampling and discretization: the so-called Bayesian Richardson extrapolation. An auto-regressive model is then fitted to the obtained results in order to describe the sampling error (taking into account the autocorrelation of sampled data), which is then used to estimate the common influence of discretization and statistical errors. Other studies addressing the issue of statistical convergence in DNS data of turbulent channel flows are the work by Hoyas and Jiménez [21] and the recent work by Thompson et al. [22], in this case considering the momentum-balance equation. However, due to the lack of consensus in the community, we see the need of developing a systematic approach to assess convergence in order to minimize discrepancies between simulations, and ensure maximum accuracy of the results. One desirable feature of such a criterion would be a direct relation with the physics of the flow instead of using a purely statistical investigation. The characteristics of the convergence criterion proposed here are discussed in detail below.

Another aspect widely discussed in the area of turbulence research is the presence of coherent structures and their role in turbulent momentum transfer across different scales. For instance, del Álamo et al. [23] assessed the role of vortex clusters in wall-bounded turbulent flows, Lozano-Durán et al. [24] the impact of three-dimensional sweeps and ejections, and Lozano-Durán and Jiménez [3] tracked both types of structures in time and developed a new approach to the study of the dynamics of turbulent flows based on them. In the present study the \(\lambda _2\) method developed by Jeong and Hussain [25] is used to identify vortex clusters in turbulent rectangular ducts of different aspect ratios, at \(Re_{\tau ,c} \simeq\) 180 and 360 (note that \(Re_{\tau ,c}\) is defined in terms of the centerplane friction velocity \(u_{\tau ,c}\)). A sequence of instantaneous velocity fields is used to obtain probability density functions of the locations of the vortex clusters, and their connection with the mean secondary flow is assessed in detail.

The present article is structured as follows: convergence criteria for channels and ducts are proposed and compared with other indicators available in the literature in Sect. 2; numerical simulations performed in the present study and convergence results for channels and ducts are presented in Sect. 3; in Sect. 4 several criteria for vortex identification are described and the cross-flow of turbulent ducts is characterized; and the conclusions of this study are summarized in Sect. 5.

## 2 Convergence in numerical simulations of wall-bounded turbulence

The first step to study convergence is the identification of initial transients, i.e., what is the time \(T_{S}\) when averaging should start. During the transient period, the flow has to evolve from the initial conditions (whether they are defined by a laminar field with superimposed disturbances, or a turbulent field extracted from a previous simulation) to a state which is representative of turbulence. This period is usually shorter if the initial conditions are already turbulent than if they are laminar. Even in the first case the flow needs some time to adjust from the initial field, so \(T_{S}\) will not be zero. In the second case, \(T_{S}\) depends on the kind of disturbance used to trigger transition to turbulence. For instance, a duct flow with aspect ratio 3 (where the aspect ratio AR is defined as the duct width \(W_{d}\) divided by its total height 2*h*) and \(Re_{\tau ,c} \simeq 180\) will relaminarize if a laminar profile with superimposed high-frequency Gaussian noise is used as starting field. However, if a low-frequency tripping mechanism similar to the one described by Schlatter and Örlü [19] is used with the initial laminar profile, then the flow transitions to turbulence as discussed by Vinuesa et al. [26]. In any case, it is important to identify \(T_{S}\) properly, since the initial transient is not representative of the flow being simulated, and thus averaging times required for convergence may increase if included in the statistics.

After identifying and discarding the initial transients, we need to determine the averaging time \(T_{A}\) required to obtain sufficiently converged statistics. It is important to note the difference between \(T_{S}\) and \(T_{A}\), and especially the relevance of \(T_{S}\): longer averaging times \(T_{A}\) may be required to ensure proper convergence if the considered \(T_{S}\) is too small, i.e., if part of the initial transients are included in the statistics. All the instantaneous fields computed at times \(t>T_{S}\) are physical (represent a turbulent field at a given instant), so in principle if these fields are averaged over sufficiently high values of \(T_{A}\) it will be possible to achieve convergence.

### 2.1 Literature review of convergence criteria

Summary of convergence guidelines available in the literature for channel flows

DNS database | Scheme | \(T_{S}\) criterion | \(T_{A}\) criterion |
---|---|---|---|

Kim et al. [1] | Spectral | Linear profile of total shear stress and quasi-periodic total kinetic energy | Not specified |

Moser et al. [27] | Spectral | Linear profile of total shear stress and quasi-periodic total kinetic energy | Stationary behavior of statistics. From their experience: \(T_{A} \ge 10 L_{x}/U_{b}\) |

Iwamoto et al. [29] | Spectral | Linear profile of total shear stress, stationary behavior of mean velocity and second-order moments at some \(y_{\rm ref}\) | Not specified |

del Álamo [28] | Spectral | Linear profile of total shear stress and quasi-periodic total kinetic energy | Stationary behavior of statistics. From their experience: \(T_{A} \ge 10 L_{x}/U_{b}\) |

Tuerke [30] | Spectral | Linear profile of total shear stress and deviatoric Reynolds stress \(\overline{vw}=0\) | Not specified |

Summary of convergence guidelines available in the literature for duct flows

DNS database | Scheme | \(T_{S}\) criterion | \(T_{A}\) criterion |
---|---|---|---|

Kim et al. [1] | Spectral | Linear profile of total shear stress and quasi-periodic total kinetic energy | Not specified |

Gavrilakis [31] | 2nd order finite-differences | Not specified (2 low-res. precursor runs) | Variation of \(U_{b}<0.2\,\%\) and of total kinetic energy \(<5\,\%\) |

Huser and Biringen [32] | 4th order fin.-diff. and spectral | Linear profile of total shear stress and constant total kinetic energy | Not specified |

Spectral | Not specified | \(T_{A} > 2000 h/U_{b}\), based on critical channel conditions [35] | |

Krasnov et al. [36] | 2nd order finite-differences | Steady \(Re_{\tau }\) and other integral quantities | Not specified |

### 2.2 Definition of converged state

*P*is the pressure, \(\nu\) is the kinematic viscosity of the fluid,

*x*and

*y*the streamwise and wall-normal coordinates,

*U*the streamwise mean velocity and \(\overline{uv}\) the Reynolds shear stress. To allow comparisons between simulations, Eq. (1) can be expressed in wall units (denoted by the superscript “\(+\)”), where the velocity scale is the friction velocity \(u_{\tau }\) and the length scale is the viscous length \(\ell ^{*}=\nu /u_{\tau }\). Doing so, and integrating the RHS with respect to \(y^{+}\), one realizes that the total shear stress \(\tau _{xy}^{+}=Re^{-1}\partial U^{+}/\partial y^{+}-\overline{uv^{+}}\) has to be linear. It is important to note that this is a direct consequence of the momentum balance (1), valid only for fully-developed channel and pipe flows, and therefore not true for low aspect ratio duct flows as will be shown below. Then, the equation characterizing the converged state of the channel flow is:

*h*(outer scaling). In the case of duct flows, the converged state can be established from a streamwise momentum balance at the duct centerplane:

*V*is the mean wall-normal velocity and

*z*the spanwise coordinate. If the aspect ratio is low the side walls impact the flow at the duct centerplane, and therefore the convective term \(V^{+} \partial U^{+}/\partial y^{+}\) and the spanwise viscous diffusion \(Re^{-1} \partial ^{2} U^{+}/\partial z^{+2}\) are not zero at the centerplane. This means that we cannot proceed with direct integration as in the channel, and therefore the total shear \(\tau _{xy}^{+}\) is not linear. As a consequence, the converged state for a duct is defined through Eq. (3), and not through Eq. (2) which is only valid for spanwise-periodic channels (or possibly rectangular ducts of sufficiently high aspect ratio).

### 2.3 Convergence indicator and normalized eddy turnover time

*t*. However, although this definition accounts for the differences in friction velocities among simulations, it does not take into account the different computational box sizes. We define the following “normalized eddy turnover times”:

*x*is the only homogeneous direction. With these definitions, we consider the fact that boxes with longer periodic dimensions effectively contain larger number of turbulent structures, and thus require shorter averaging times to reach the same level of convergence as a smaller box (as also observed by del Álamo [28]).

### 2.4 Summary of convergence results available in the literature

*Re*case has an averaging period of more than 10 times the one with the larger

*Re*. In addition, the second case exhibits a lower \(\varepsilon\) value, which means that it is more converged according to the already discussed criterion. The idea is that the higher

*Re*case was computed in a larger box, which despite the fact of being more computationally expensive, allowed averaging a larger number of turbulent structures than the smaller one. Therefore, each ETT computed in the higher

*Re*case contains more information towards calculating statistics. This example highlights the interest of using the normalized \(\mathrm{ETT}^{*}\) definitions (5) and (6). This also helps to compare, in a more objective way, statistics from different databases performed in various computational boxes.

Convergence features of channel flows in the literature

DNS database | \(Re_{\tau }\) | \(\mathrm{ETT}_{S}\) | \(\mathrm{ETT}_{A}\) | \(\mathrm{ETT}^{*}_{S}\) | \(\mathrm{ETT}_{A}^{*}\) | \(\varepsilon _{\rm channel}\) |
---|---|---|---|---|---|---|

Kim et al. [1] | 180 | – | 10 | – | 43.9 | \(1.88 \times 10^{-3}\) |

Moser et al. [27] | 392 | – | – | – | – | \(4.80 \times 10^{-3}\) |

587 | – | – | – | – | \(8.50 \times 10^{-3}\) | |

Iwamoto et al. [29] | 109 | – | 2559 | – | 14,031 | \(1.03 \times 10 ^{-5}\) |

150 | – | 2061 | – | 11,300 | \(2.91 \times 10 ^{-5}\) | |

298 | – | 277 | – | 379.7 | \(6.61 \times 10 ^{-5}\) | |

396 | – | 129 | – | 176.8 | \(9.38 \times 10 ^{-4}\) | |

643 | – | 40 | – | 54.8 | \(1.67 \times 10 ^{-3}\) | |

del Álamo et al. [39] | 186 | – | 52.8 | – | 922.4 | \(1.27 \times 10 ^{-3}\) |

547 | – | 13.7 | – | 239.7 | \(1.11 \times 10 ^{-3}\) | |

del Álamo et al. [2] | 934 | – | 11.7 | – | 153.5 | \(1.08 \times 10 ^{-3}\) |

Hoyas and Jiménez [38] | 2004 | – | 10.3 | – | 135.5 | \(7.73 \times 10 ^{-4}\) |

Tuerke [30] | 550 | 5 | – | 5.5 | – | – |

950 | 5 | – | 5.5 | – | – |

The results summarized in Table 3 are presented graphically in Fig. 1. The first interesting conclusion that can be drawn is the fact that, although Moser et al. [27] and del Álamo [28] in principle used the same criterion for convergence, they reach very different convergence levels. The database from Jiménez’s research group [2, 38, 39] shows a consistent level of convergence throughout the whole Reynolds number range, on the order of \(\varepsilon \simeq 10^{-3}\), which can be considered to be sufficiently converged. However, the runs by Moser et al. [27] exhibit convergence indicators on the order of 4–10 times larger than the ones by Jiménez. This indicates the need for an objective convergence criterion that allows for comparisons between simulations. It is also interesting to note that Kim et al. [1] actually reach a convergence level very similar to the one from Jiménez, and the database from Iwamoto et al. [29] exceeds their convergence level by several orders of magnitude at low *Re*.

*Re*case by Krasnov et al. [36], which will be discussed later. The duct cases require very long averaging times for convergence due to the interaction between the secondary motions produced at the duct corners and the mean flow. This interaction has been extensively studied experimentally by Gessner et al. [41] and Gessner and Jones [42], and numerically by Vinuesa et al. [43]. Despite this, in Table 4 only Pinelli et al. [33] averaged for long periods of time. This is in part due to the lack of a consistent convergence criterion for ducts (the linear total shear profile criterion is not valid as we discussed above), and partly because duct cases are much more expensive than the periodic channel. The presence of two inhomogeneous directions does not allow the use of periodic boundary conditions in the spanwise direction, a fact that significantly increases computational cost. Another detail must be highlighted when comparing Tables 3 and 4: the convergence indicators \(\varepsilon _{\mathrm{channel}}\) and \(\varepsilon _{\mathrm{duct}}\) are not defined in terms of the same physical magnitude (shear stress for the former, and momentum in the latter), although both are expressed in nondimensional form.

Convergence features of duct flows in the literature

DNS database | \(\overline{Re_{\tau }}\) | \(\mathrm{ETT}_{S}\) | \(\mathrm{ETT}_{A}\) | \(\mathrm{ETT}^{*}_{S}\) | \(\mathrm{ETT}_{A}^{*}\) | \(\varepsilon _{\rm duct}\) |
---|---|---|---|---|---|---|

Gavrilakis [31] | 150 | 6 | 5 | 62.8 | 52.3 | \(3.27 \times 10^{-3}\) |

Huser and Biringen [32] | 300 | 120 | 30 | 256 | 64 | \(2.97 \times 10^{-3}\) |

Uhlmann et al. [34] | 78 | – | 60.8 | – | 127.4 | \(1.30 \times 10^{-2}\) |

100 | – | 108.8 | – | 113.9 | \(2.02 \times 10^{-2}\) | |

Pinelli et al. [33] | 150 | – | 544.2 | – | 1,139.8 | \(2.02 \times 10^{-3}\) |

230 | – | 377.4 | – | 790.4 | \(1.77 \times 10^{-3}\) | |

Ohlsson et al. [40] | 310 (\(\mathrm{AR}=3.33\)) | 12.1 | 17.5 | – | – | – |

Krasnov et al. [36] | 4253 | – | 1.3 | – | 2.7 | – |

*Re*computation by Krasnov et al. [36], presents a very short averaging time (around 30 times shorter than Pinelli’s values extrapolated to such a high Reynolds number). We did not have access to their database, so we were unable to calculate their convergence indicator, although they mention in their study [36] some problems in their statistics which they attribute to short averaging periods. In addition, their second-order finite-difference code may not provide as much accuracy as the spectral or fourth order finite-difference codes proposed by other research groups, especially at such high

*Re*.

## 3 Direct numerical simulations of turbulent channel and ducts flows

After carefully reviewing previously proposed convergence criteria, and assessing the level of convergence from available DNSs, we performed our own direct numerical simulations of one channel flow, and analyzed existing duct flow data with aspect ratios 1, 3 and 5 [26]. All the cases were computed at \(Re_{\tau }\) values around 180 (in the case of the ducts, the flow was adapted as discussed below to maintain the same conditions at the centerplane for the various aspect ratios). The results of these computations are shown on Figs. 1 and 2 using filled symbols. The characteristics of the numerical codes and the computations are presented next.

### 3.1 DNS of turbulent channel flow

Direct numerical simulations require computing all the spatial and temporal scales of the flow, including the largest energy-containing and the smallest dissipative ones. To that end, the computational mesh needs to be very fine close to the walls (in order to properly capture the smallest scales, which reside in the near-wall region), and it is coarsened as the core of the flow is approached, where the larger scales reside. For adequate simulation reliability, the numerical discretization has to allow an accurate representation of all the flow scales. Thus, high-order numerical schemes are the preferred methods for turbulence.

The numerical computation of turbulent channel flow was carried out using the numerical code SIMSON [44], based on a pseudo-spectral discretization to solve the three-dimensional, time-dependent, incompressible Navier–Stokes equations. Periodic boundary conditions are used in the streamwise and spanwise directions, where Fourier expansions with dealiasing represent the velocity field, and Chebyshev polynomials were used in the wall-normal direction. The streamwise pressure gradient was recalculated after each time-step to maintain a constant mass flux through the channel cross-section. The kinematic viscosity \(\nu\) was set so that a Reynolds number based on channel half-height *h* and bulk veloctiy \(U_{b}\) of \(Re_{b} \simeq 2800\) was obtained; this led to a friction Reynolds number of \(Re_{\tau } \simeq 180\). In this code, time is advanced by means of a standard mixed four-step Crank–Nicolson/Runge–Kutta scheme.

The computational box was the same as in Kim et al. [1], i.e., streamwise and spanwise lengths of \(L_{x}=4 \pi\) and \(L_{z}=2 \pi\), with wall-normal length \(L_{y}=2\). Uniform grid spacings of \(\Delta x^{+}=12\) and \(\Delta z^{+}=7\) were kept in the homogeneous directions, whereas the Chebyshev distribution in the wall-normal direction led to a minimum grid spacing of \(\Delta y^{+}_{\mathrm{min}}=0.05\) at the wall, and a maximum \(\Delta y^{+}_{\mathrm{max}}=4.4\) at the channel core. A total of \(192 \times 129 \times 160\) grid-points in the *x*, *y* and *z* directions were considered to discretize the computational domain. The simulation is initiated with random noise at \(t=0\).

In order to identify adequate values of \(T_{S}\) and \(T_{A}\), we generate a contour map with a wide range of (\(T_{S}, T_{A}\)) combinations obtained from the channel simulation, and plot the value of \(\varepsilon _{\mathrm{channel}}\), which should ideally decay to zero as statistical convergence is approached. However, only few of the runs by Iwamoto et al. [29] exhibit converge indicators below \(10^{-3}\), and most of the runs from Jiménez’s group are close to this value. Since for practical purposes, statistics obtained with \(\varepsilon _{\mathrm{channel}} = 10^{-3}\) can be considered to be sufficiently converged, we will take this as our convergence criterion for channel flows. The contour plot of \(\varepsilon _{\mathrm{channel}}\) versus the starting and averaging times \(T_{S}\) and \(T_{A}\) in convective time units (nondimensionalized using \(U_{b}\) and *h*) is shown in Fig. 3 for our channel flow simulation. This figure shows how, for starting times lower than approximately 200 convective time units, the value of \(\varepsilon\) decays very slowly, even for increasingly longer averaging times. This is due to the fact that, for \(T_{S}<200\), the instantaneous flow is not representative of a physical turbulent field, and therefore should not be accounted for in the flow statistics. Interestingly, for starting times larger than 200 convective time units (equivalent to \(\mathrm{ETT_{S}^{*}}=50\)), the value of the convergence indicator starts to decay more quickly with averaging time.

### 3.2 DNSs of turbulent duct flows

Like in the channel flow case, a direct numerical simulation technique was used to compute turbulent duct flows at three different aspect ratios. These simulations were carried out using the code Nek5000, developed by Fischer et al. [45] at Argonne National Laboratory (nek5000.mcs.anl.gov), and based on the spectral element method (SEM), originally proposed by Patera [46]. In this code, the incompressible Navier–Stokes equations are cast in weak form, so they are multiplied by a test function and integrated over the domain. The Galerkin approximation is considered for spatial discretization following the \(\mathbb {P}_{N}-\mathbb {P}_{N-2}\) formulation by Maday and Patera [47], that associates the pressure with polynomials two degrees lower than the velocity. The three-dimensional velocity vector is expressed in terms of tensor-products of Lagrange polynomials of order *N* within a spectral element, and the solution is represented at the Gauss-Lobatto-Legendre (GLL) quadrature points. The nonlinear terms are treated explicitly by third order extrapolation (EXT3), whereas the viscous terms are treated implicitly by a third-order backward differentiation scheme (BDF3) leading to a linear symmetric Stokes system to be solved at every time step.

These computations were carried out on a Cray XE6 machine at the PDC Center of KTH in Stockholm (Sweden). They required from 2048 to 4096 cores, and the MPI (message-passing interface) was employed for parallelization. In all the cases, the computational box was 25 duct half-heights long (\(L_{x}=25h\)). This is large enough to capture the longest turbulent structures in the streamwise direction according to experimental measurements in pipe flow (Guala et al. [48]) and DNSs of turbulent channel (Jiménez and Hoyas [49]) and pipe flows (Chin et al. [50]). The box length in the wall-normal direction is \(L_{y}=2h\) for all cases, and the spanwise length is adjusted depending on the aspect ratio, so for \(\mathrm{AR}=5\) we have \(L_{z}=10h\). The mesh is designed so that \(\Delta x^{+}<10, \Delta y^{+}_{\mathrm{max}}<5\), and we have at least 4 points below \(y^{+}=1\) (the guidelines for *y* also apply to *z*). Although the nodes within spectral elements are the GLL quadrature points, one has freedom to choose the element distribution, so we blended Chebyshev (close to the wall) with uniform (at the duct core) distributions, satisfying the various mesh quality requirements. Also, in an approach similar the one considered for the channel, here we adjust the input Reynolds number \(Re_{b}\) through an iterative process, in order to keep the centerplane bulk Reynolds number \(Re_{b,c}=U_{b,c} h/\nu\) (where \(U_{b,c}\) is the bulk velocity at the centerplane of the duct) constant for the different aspect ratios. This allows easier comparisons among aspect ratio cases and with available channel data. Therefore, the nominal \(Re_{\tau }\) values are just a reference, since the actual \(Re_{\tau ,c}\) will change with AR. Note that the flow is allowed to approach fully-developed turbulence via consecutively more refined runs, and the initial profile was a laminar duct flow expansion [51] with a wall-normal volume force tripping (which is activated only during the initial low-resolution runs) similar to the one used by Schlatter and Örlü [19].

#### 3.2.1 Results from the square duct case

*xy*centerplane (note that the

*xz*plot looks qualitatively very similar). In this figure we represent data up to 1680 convective time units only, which is enough to identify the initial transients: in the

*xy*centerplane the region of lowest \(\varepsilon\) can be found for \(T_{S} \simeq 100\), and averaging times of around 1580. This would not be the lowest possible \(\varepsilon\) value, and it is necessary to look at the complete time history (starting from \(T_{S}=100\)) to identify the minimum \(T_{A}\) to ensure convergence. This is done in Fig. 6, where \(\varepsilon _{xy}\) and \(\varepsilon _{xz}\) are shown as a function of averaging time. Note that in the present turbulent duct simulations \(\Delta t\) was kept below 0.2 in all cases. It can be observed how after an initial averaging period of 1000 convective time units, the decay in \(\varepsilon\) is very slow. This is related to the interaction between the secondary flow with the mean flow, and it can be argued that stationary behavior will require really long averaging times in this flow. However, reasonable levels of convergence should be sufficient for reliable conclusions. The minimum \(\varepsilon\) is around \(10^{-3}\) in both centerplanes. From Fig. 6, this value is not reached by the average \(\varepsilon\) curve until around \(T_{A}=5400\) convective time units. As a consequence, we can argue that, in order to reach sufficient statistical convergence (\(\varepsilon _{\mathrm{duct}} \simeq 10^{-3}\)), we need to discard 100 convective time units of initial transients (equivalent to \(\mathrm{ETT}_{S}=7.12\) and \(\mathrm{ETT}_{S}^{*}=30\) in our simulation), and then average for at least 5400 convective time units (equal to \(\mathrm{ETT_{A}}=385\) and \(\mathrm{ETT}_{A}^{*}=1602\)).

#### 3.2.2 Results from the \({ AR=3}\) duct case

*xy*centerplane, as a function of starting and averaging times. This figure shows that transient effects are present until \(T_{S}=200\), which is equivalent to \(\mathrm{ETT_{S}}=13.8\), or \(\mathrm{ETT_{S}^{*}}=57.5\)) if the box size correction is considered. The minimum \(\varepsilon\) value is obtained at approximately \(T_{A}=1600\), which corresponds to \(\mathrm{ETT}_{A}=110\) and \(\mathrm{ETT}_{A}^{*}=460\). Although the minimum \(\varepsilon _{\mathrm{duct}}\) is \(2.95 \times 10^{-4}\), a more moderate convergence value of \(\varepsilon _{\mathrm{duct}}=10^{-3}\) can be obtained with \(T_{A}=1000\) or \(\mathrm{ETT}_{A}^{*}=287.5\). It is also interesting to note that the convergence indicator on the

*xz*centerplane reaches a value of \(\varepsilon =1.5 \times 10^{-3}\) rather quickly (\(T_{A}\) of around 200), but then this indicator does not get significantly smaller. This is associated with the fact that the most significant physical mechanisms take place on the

*xy*centerplane instead of the spanwise direction.

#### 3.2.3 Results from the \({ AR=5}\) duct case

The convergence and averaging time results from the previous sections are also summarized in Fig. 2, where a comparison with the available data in the literature is also shown. Note that for the aspect ratio 3 and 5 cases we present two scenarios: the short \(T_{A}\) (which should be considered as a minimum requirement for convergence) and the long \(T_{A}\) (corresponding to our longest runs, with the lowest possible convergence indicators).

## 4 Characterization of the mean cross-flow structure in turbulent rectangular ducts

### 4.1 Vortex identification methods

*Q*criterion by Hunt et al. [52], the \(\Delta\) criterion proposed by Chong et al. [53], the swirling strength condition by Zhou et al. [54], the approach by Kida and Miura [55] and the \(\lambda _{2}\) method by Jeong and Hussain [25]. We have extensively tested all these methodologies and found that all of them yield very similar results. The analysis presented in Sect. 4.2 was performed by considering the \(\lambda _{2}\) method [25], which as most vortex identification methods, is based on the analysis of the properties of the velocity gradient tensor:

*S*and \(\varOmega\)) one can find the regions of local pressure minimum associated with vortex centers. Jeong and Hussain [25] define a vortex core as a region where \(S^{2}+\varOmega ^{2}\) has two negative eigenvalues. Therefore, it is sufficient to sort the eigenvalues in increasing order and check the sign of the second one (which gives the \(\lambda _{2}\) name to the method).

### 4.2 Characterization of the secondary flow

In this section we analyze the in-plane structure of the flow in turbulent square ducts at \(Re_{\tau ,c} \simeq 180\) and 360, and of rectangular ducts with aspect ratios 3 and 10 at \(Re_{\tau ,c} \simeq 180\). The databases considered for these analyses are described in detail in Refs. [26, 43]. In Fig. 9 we assess the Reynolds-number effects on the flow by analyzing streamwise velocity *U*, streamlines of the mean secondary flow \(\psi\), probability density function (pdf) of coherent vortex locations obtained with the \(\lambda _{2}\) method [25] and mean streamwise vorticity \(\varOmega _{x}\). The first interesting feature of the flow at the two Reynolds numbers is the fact that the typical secondary flow pattern with one pair of counter-rotating vortex on each corner can be observed. This type of cross-flow is denoted as secondary flow of second kind [56], and it is formed by the cross-stream Reynolds stress difference \(\overline{v^{2}}-\overline{w^{2}}\) and the deviatoric Reynolds shear stress \(\overline{vw}\). It is clear from both parts of the figure that the secondary flow basically convects momentum from the duct centerplane towards the duct bisector, and the iso-contours of the streamwise velocity reflect this effect: the flow is lifted at \(z/h \simeq 0\) (with the corresponding local reduction of wall shear stress), and pushed towards the corner along the duct bisector. It is also interesting to note that the pdf of vortex locations follows the distribution of iso-contours of the mean flow as well, which further supports the connection between the individual vortical structures and the averaged flow features. The two thick black lines indicate the separation between regions with probability above and below 60 % of the maximum probability of occurrence, and as expected the probability decreases as the core of the flow and the wall are approached. The corner region also exhibits a very low probability of vortex occurrence due to the inhibiting effect of the side wall on the turbulent cycle taking place on the horizontal wall (and viceversa), which leads locally to very low *Re* conditions. With respect to the regions of high probability of finding vortices, in both cases the maximum probability is obtained at a wall-normal distance of around \(40^{+}\), which is in agreement with the square duct simulations by Pinelli et al. [33] up to \(Re_{\tau } \simeq 300\) (based on friction velocity averaged over the four walls). Note that in the study by Pinelli et al. [33] the pdf of streak locations was evaluated by means of the wall shear stress time history, whereas here we reach the same conclusion based on the analysis of individual vortical structures. Although the location of maximum pdf is fixed in inner units, in outer units this location is \(y/h \simeq 0.22\) and \(\simeq 0.11\) in the low and high-*Re* cases respectively, which shows the effect of a wider scale separation as consequence of the increasing Reynolds number. This is also manifested in the vortex distributions, where the region of low pdf remains bounded to a narrower region close to the wall in the higher *Re* case. Another interesting effect of the Reynolds number is the fact that the inner-scaled duct widths are \(\simeq 360\) and 720 respectively, which limits the number of streaks present in each case since the spanwise separation between two adjacent streaks is approximately \(50^{+}\).

*Re*cases exhibit similar features although the pattern in the \(Re_{\tau ,c} \simeq 360\) case appears to be more stretched towards the core, as also observed by Pinelli et al. [33]. Interestingly, the centers of the vortices also move farther away from the wall as

*Re*increases, which suggests that large-scale structures in the flow play an important role in the formation of the secondary flow. The opposite effect is observed in the streamwise vorticity pattern: although qualitatively the \(\varOmega _{x}\) fields share some features with the \(\psi\) one (namely the sense of rotation from the duct centerplane towards the bisectors). On the other hand as

*Re*increases, in the case of the wall vorticity component of opposite sign, the vorticity field contracts and becomes limited to a progressively smaller region closer to the wall. The centers of the \(\varOmega _{x}\) regions also move towards the wall for increasing Reynolds numbers, which indicates that the near-wall structures are more relevant to the streamwise vorticity field than the large-scale motions. This is further corroborated when analyzing the difference between the pdf of occurrence of vortices with positive and negative streamwise vorticity, which was also analyzed by Pinelli et al. [33], and strongly resembles the \(\varOmega _{x}\) field. Note that a total of 100 instantaneous fields of streamwise length \(L_{x}=25h\) were analyzed to obtain these results, and a larger number of fields would allow one to detect more individual structures, which would likely lead to better agreement with the \(\varOmega _{x}\) field. These results demonstrate that there is a strong connection between the individual vortical structures preferentially located close to the corner and the streamwise vorticity field, which explains why \(\varOmega _{x}\) contracts for increasing

*Re*. It can therefore be argued that the streamline field scales in outer units whereas the streamwise vorticity one does it in inner units, hence highlighting the complex and multiscale nature of the secondary flow of second kind.

*z*, all the way to the centerplane. Its center also moves slightly away from the corner, from a distance of around 0.5

*h*in the square duct to around 0.8

*h*. Further increase of the aspect ratio produces a progressive development of the vortex on the horizontal wall, up to a spanwise distance of around 5

*h*from the corner, although its center appears to remain at a distance of 0.8

*h*from the corner. This is another manifestation of the relevance of large-scale motions in the flow on the streamline pattern: in this case larger scales are allowed by the physical increase of the spanwise dimension, instead of the larger scale disparity produced by a higher

*Re*. A very interesting observation can be drawn from the \(\varOmega _{x}\) fields: the region closer to the corner does not get constrained as the aspect ratio is increased, and the region next to it expands to a much lower extent than the streamline pattern in the \(\mathrm{AR}=3\) and 10 cases. In this regard, the vorticity component along the horizontal wall shows more development in

*z*, but still not as much as the streamlines. Note that the center of the vorticity region closer to the corer remains constant at a distance of around 0.1

*h*as AR increases, and it is quite remarkable that the region next to it, unlike the streamline pattern, also has a fixed center located at a distance of around 0.3

*h*. Therefore, the larger scales resulting from a physically wider duct do not significantly affect the fundamental behavior of the streamwise vorticity field, since its relevant physics are associated with the near-wall structures. The difference between the pdf of occurrence of vortices with positive and negative streamwise vorticity, which also in these cases shows strong resemblance with the \(\varOmega _{x}\) field, further reinforces this conclusion. The analysis of coherent structures was based on 334 instantaneous fields in the \(\mathrm{AR}=3\) case and 536 in the \(\mathrm{AR}=10\) one.

## 5 Conclusions and discussion

Despite the impact of convergence level on the final statistics of direct numerical simulations of wall-bounded turbulence, there is not a consistent criterion in the literature to allow appropriate convergence assessments. In this study a wide range of databases of turbulent channel and duct flows is analyzed, comparing numerical algorithms, starting and averaging times and achieved level of convergence. To this end, a convergence indicator for channel flows \(\varepsilon _{\mathrm{channel}}\) based on the deviation of the total shear stress from a linear profile is defined. An extension of this criterion for duct flows (\(\varepsilon _{\mathrm{duct}}\)) is also proposed, and since the total shear stress does not have to be linear in ducts, we measure the deviation with respect to the streamwise momentum balance at the duct centerplane. Note that this criterion applies to convergence of the duct at the centerplane section, and not to other cross-flow effects taking place in the spanwise direction. In order to allow appropriate comparisons of starting and averaging times among simulations, we express both in eddy turnover times and then apply a correction based on the box size. The motivation of this correction is to acknowledge the fact that simulations run on larger boxes effectively contain more turbulent structures (in the homogeneous directions), thus are approximately equivalent to longer runs in smaller boxes. Comparisons of the indicator and corrected averaging time for available data in the literature lead to consistent trends in the results, thus proving the validity of the proposed approach.

We also present results from DNSs of a turbulent channel flow, and three duct flows with aspect ratios 1, 3 and 5, all of them at \(Re_{\tau ,c} \simeq 180\). The aim of these simulations was to find optimum values of starting and averaging times (\(T_{S}\) and \(T_{A}\) respectively, when expressed in convective time units) for various flow cases. We also find a maximum value of the spacing in time between individual realizations, which in inner scaling takes the value \(\Delta t^{+}=17\). For both channel and duct we identified the converged state as that where the corresponding convergence indicator \(\varepsilon\) took a value of \(10^{-3}\) or lower. Under this criterion, most of the available channel-flow data in the literature can be considered as converged, except the database by Moser et al. [27] which is however close to convergence. With respect to the duct data, none of the literature data can be considered to be sufficiently converged. This is in part due to the lack of an appropriate definition of convergence for the duct, and also due to the extremely long averaging times required for square ducts at low Reynolds numbers. The methodology proposed here can serve as a baseline to design new simulations, assess the quality of already existing ones, and more importantly can help to interpret and scrutinize available DNS data in the literature, in the same way as experimentalists take into account details of the experimental setup when interpreting a particular dataset.

It is important to note that the proposed criteria are meant to provide a baseline comparison between databases, and an idea of the convergence level achieved in channel and duct-flow simulations. However, these criteria are focused on the mean momentum balance, and therefore do not provide a comprehensive assessment of convergence. For instance, convergence in terms of \(\varepsilon\) does not guarantee convergence in other quantities of interest such as spectra, two-point correlations or Reynolds-stress transport equations. Therefore, the present work should be considered as an initial effort towards defining more general convergence criteria. Moreover, we also acknowledge that many research groups assess statistical convergence in a number of ways that are not necessarily reported in their publications: for instance, they assess the evolution of quantities that should be statistically zero when convergence has been achieved (such as the mean spanwise velocity in turbulent channel flows), or they confirm that statistics computed from the second half of the averaging time are consistent with those calculated in terms of the first half (which prevents from statistics polluted by inadequately stationary data). Other remarkable efforts toward establishing good practices in statistical convergence are the statistical error analyses by Oliver et al. [20] and Hoyas and Jiménez [21], or the documentation of residuals in the mean momentum balance and the Reynolds-stress transport equations in the simulations by Lee and Moser [4].

In a second part of the study, the in-plane structure of the flow in turbulent ducts is assessed by analyzing square ducts at \(Re_{\tau ,c} \simeq 180\) and 360 and rectangular ducts with aspect ratios 3 and 10 at \(Re_{\tau ,c} \simeq 180\) [26, 43]. The effect of the secondary flow of second kind on the mean flow, i.e., convection of momentum from the duct centerplane to the bisectors, is observed in the iso-contours of streamwise velocity. Identification of coherent vortices using the \(\lambda _{2}\) criterion [25] shows that near-wall streaks are located in all the duct cases at a wall-normal distance of \(y^{+} \simeq 40\) as in Pinelli et al. [33], and the probability of occurrence of a vortex at the corner is very low due to the inhibiting effect of the side wall. Moreover, we find that the streamline pattern becomes stretched towards the duct core at higher *Re* and towards the duct centerplane at higher AR; the centers of the vortices also move away from the wall in both cases, which highlights the relevant role of large-scale motions on the streamline pattern of the secondary flow. On the other hand, the streamwise vorticity field becomes compressed towards the duct corners as *Re* increases, and its changes are comparatively small for increasing AR. The connection between the \(\varOmega _{x}\) field and the near-wall structures is further illustrated by comparing vorticity contours with the difference between the pdf of occurrence of vortices with positive and negative streamwise vorticity. These conclusions, i.e., outer-scale scaling of \(\psi\) and inner-scale scaling of \(\varOmega _{x}\), extend the findings by Pinelli et al. [33] to higher Reynolds numbers, and more importantly to another kind of large-scale motions in the flow through the consideration of wider ducts. They also highlight the complex and multiscale nature of the secondary flow of second kind in turbulent duct flows.

## Notes

### Acknowledgements

RV and PS acknowledge financial support from the Knut and Alice Wallenberg Foundation and the Swedish Research Council (Vetenskapsrådet). The simulations were performed on resources provided by the Swedish National Infrastructure for Computing (SNIC) at PDC in Stockholm. We are also grateful to the various research groups who made their databases publicly available online.

### Compliance with ethical standards

### Conflict of interest

The authors declare that they have no conflict of interest.

## References

- 1.Kim J, Moin P, Moser RD (1987) Turbulence statistics in fully developed channel flow at low reynolds number. J Fluid Mech 177:133ADSCrossRefMATHGoogle Scholar
- 2.del Álamo JC, Jiménez J, Zandonade P, Moser RD (2004) Scaling of the energy spectra of turbulent channels. J Fluid Mech 500:135ADSCrossRefMATHGoogle Scholar
- 3.Lozano-Durán A, Jiménez J (2014) Time-resolved evolution of coherent structures in turbulent channels: characterization of eddies and cascades. J Fluid Mech 759:432ADSCrossRefGoogle Scholar
- 4.Lee M, Moser RD (2015) Direct numerical simulation of turbulent channel flow up to \(re_{\tau }= 5200\). J Fluid Mech 774:395ADSCrossRefGoogle Scholar
- 5.Schlatter P, Örlü R (2010) Assessment of direct numerical simulation data of turbulent boundary layers. J Fluid Mech 659:116CrossRefMATHGoogle Scholar
- 6.Sillero JA, Jiménez J, Moser RD (2013) One-point statistics for turbulent wall-bounded flows at reynolds numbers up to \(\delta ^{+} \simeq 2000\). Phys Fluids 25:105102ADSCrossRefGoogle Scholar
- 7.Wu X, Moin P (2008) A direct numerical simulation study on the mean velocity characteristics in turbulent pipe flow. J Fluid Mech 608:81ADSCrossRefMATHGoogle Scholar
- 8.El Khoury GK, Schlatter P, Noorani A, Fischer PF, Brethouwer G, Johansson AV (2013) Direct numerical simulation of turbulent pipe flow at moderately high reynolds numbers. Flow Turbul Combust 91:475CrossRefGoogle Scholar
- 9.Österlund JM (1999) Experimental studies of zero pressure-gradient turbulent boundary layer flow. PhD Thesis, Royal Institute of Technology (KTH), Stockholm, SwedenGoogle Scholar
- 10.Nagib HM, Chauhan KA, Monkewitz PA (2007) Approach to an asymptotic state for zero pressure gradient turbulent boundary layers. Phil Trans R Soc A 365:755ADSCrossRefMATHGoogle Scholar
- 11.Chauhan KA, Monkewitz PA, Nagib HM (2009) Criteria for assessing experiments in zero pressure gradient boundary layers. Fluid Dyn Res 41:021404ADSCrossRefMATHGoogle Scholar
- 12.Vinuesa R, Schlatter P, Malm J, Mavriplis C, Henningson DS (2015) Direct numerical simulation of the flow around a wall-mounted square cylinder under various inflow conditions. J Turbul 16:555ADSCrossRefGoogle Scholar
- 13.Vinuesa R, Nagib HM (2016) Enhancing the accuracy of measurement techniques in high Reynolds number turbulent boundary layers for more representative comparison to their canonical representations. Eur J Mech B Fluids 55:300MathSciNetCrossRefGoogle Scholar
- 14.Vinuesa R, Duncan RD, Nagib HM (2016) Alternative interpretation of the Superpipe data and motivation for CICLoPE: the effect of a decreasing viscous length scale. Eur J Mech B Fluids 58:109CrossRefGoogle Scholar
- 15.Talamelli A, Bellani G, Rossetti A (2014) The “long pipe” in CICLoPE: A design for detailed turbulence measurements. In: Progress in Turbulence V, Proceedings in Physics. Springer, vol 149, p 127Google Scholar
- 16.Klewicki JC, Falco RE (1990) On accurately measuring statistics associated with small-scale structure in turbulent boundary layers using hot-wire probes. J Fluid Mech 219:119ADSCrossRefGoogle Scholar
- 17.Antonia RA, Satyaprakash BR, Hussain AKMF (1982) Statistics of fine-scale velocity in turbulent plane and circular jets. J Fluid Mech 119:55ADSCrossRefGoogle Scholar
- 18.Örlü R, Schlatter P (2013) Comparison of experiments and simulations for zero pressure gradient turbulent boundary layers at moderate Reynolds numbers. Exp Fluids 54:1547CrossRefGoogle Scholar
- 19.Schlatter P, Örlü R (2012) Turbulent boundary layers at moderate reynolds numbers: inflow length and tripping effects. J Fluid Mech 710:5ADSCrossRefMATHGoogle Scholar
- 20.Oliver TA, Malaya N, Ulerich R, Moser RD (2014) Estimating uncertainties in statistics computed from direct numerical simulation. Phys Fluids 26:035101ADSCrossRefGoogle Scholar
- 21.Hoyas S, Jiménez J (2008) Reynolds number effects on the reynolds-stress budgets in turbulent channels. Phys Fluids 20:101511ADSCrossRefMATHGoogle Scholar
- 22.Thompson RL, Sampaio LEB, Bragança Alves FAV, Thais L, Mompean G (2016) A methodology to evaluate statistical errors in DNS data of plane channel flows. Comp Fluids 130:1MathSciNetCrossRefGoogle Scholar
- 23.del Álamo JC, Jiménez J, Zandonade P, Moser RD (2006) Self-similar vortex clusters in the turbulent logarithmic region. J Fluid Mech 561:329ADSCrossRefMATHGoogle Scholar
- 24.Lozano-Durán A, Flores O, Jiménez J (2011) The three-dimensional structure of momentum transfer in turbulent channels. J Fluid Mech 694:100ADSCrossRefMATHGoogle Scholar
- 25.Jeong J, Hussain F (1995) On identification of a vortex. J Fluid Mech 285:69ADSMathSciNetCrossRefMATHGoogle Scholar
- 26.Vinuesa R, Noorani A, Lozano-Durán A, El Khoury GK, Schlatter P, Fischer PF, Nagib HM (2014) Aspect ratio effects in turbulent duct flows studied through direct numerical simulation. J Turbul 15:677ADSCrossRefGoogle Scholar
- 27.Moser RD, Kim J, Mansour NN (1999) Direct numerical simulation of turbulent channel flow up to \({R}e_{\tau }=590\). Phys Fluids 11:943ADSCrossRefMATHGoogle Scholar
- 28.del Álamo JC (2005) La organización a gran escala de canales turbulentos. PhD Thesis, Polytechnic University of Madrid, SpainGoogle Scholar
- 29.Iwamoto K, Suzuki Y, Kasagi N (2002) Reynolds number effect on wall turbulence: toward effective feedback control. Int J Heat Fluid Flow 23:678MathSciNetCrossRefGoogle Scholar
- 30.Tuerke F (2011) An inverse rans simulation of a turbulent channel flow at moderate reynolds numbers. Final Project Report, Polytechnic University of Madrid (Spain) and Technische Universität Berlin (Germany)Google Scholar
- 31.Gavrilakis S (1992) Numerical simulation of low-reynolds-number turbulent flow through a straight square duct. J Fluid Mech 244:101ADSCrossRefGoogle Scholar
- 32.Huser A, Biringen S (1993) Direct numerical simulation of turbulent flow in a square duct. J Fluid Mech 257:65ADSCrossRefMATHGoogle Scholar
- 33.Pinelli A, Uhlmann M, Sekimoto A, Kawahara G (2010) Reynolds number dependence of mean flow structure in square duct turbulence. J Fluid Mech 644:107ADSCrossRefMATHGoogle Scholar
- 34.Uhlmann M, Pinelli A, Kawahara G, Sekimoto A (2007) Marginally turbulent flow in a square duct. J Fluid Mech 588:153ADSCrossRefMATHGoogle Scholar
- 35.Jiménez J, Moin P (1991) The minimal flow unit in near-wall turbulence. J Fluid Mech 225:213ADSCrossRefMATHGoogle Scholar
- 36.Krasnov D, Zikanov O, Boeck T (2012) Numerical study of magnetohydrodynamic duct flow at high reynolds and hartmann numbers. J Fluid Mech 704:421ADSMathSciNetCrossRefMATHGoogle Scholar
- 37.Flores O, Jiménez J (2010) Hierarchy of minimal flow units in the logarithmic layer. Phys Fluids 22:071704ADSCrossRefGoogle Scholar
- 38.Hoyas S, Jiménez J (2006) Scaling of the velocity fluctuations in turbulent channels up to \({R}e_{\tau } = 2003\). Phys Fluids 18:011702ADSCrossRefGoogle Scholar
- 39.del Álamo JC, Jiménez J (2003) Spectra of the very large anisotropic scales in turbulent channels. Phys Fluids 15:41CrossRefMATHGoogle Scholar
- 40.Ohlsson J, Schlatter P, Fischer PF, Henningson D (2010) Direct numerical simulation of separated flow in a three-dimensional diffuser. J Fluid Mech 650:307ADSCrossRefMATHGoogle Scholar
- 41.Gessner FB, Eppich HM, Lund EG (1993) Reynolds number effects on the near-wall structure of turbulent flow along a streamwise corner. In: So RMC, Speziale CG, Launder BE (eds) Near wall turbulent flows. Elsevier, Amsterdam, pp 965–975Google Scholar
- 42.Gessner FB, Jones JB (1965) On some aspects of fully-developed turbulent flow in rectangular channels. J Fluid Mech 23:689ADSCrossRefGoogle Scholar
- 43.Vinuesa R, Schlatter P, Nagib HM (2015) On minimum aspect ratio for duct flow facilities and the role of side walls in generating secondary flows. J Turbul 16:588ADSCrossRefGoogle Scholar
- 44.Chevalier M, Schlatter P, Lundbladh A, Henningson DS (2007) A pseudo-spectral solver for incompressible boundary layer flows. Tech. Rep. TRITA-MEK 2007:07, Royal Institute of Technology, Stockholm, SwedenGoogle Scholar
- 45.Fischer P.F., Lottes J.W., Kerkemeier S.G. (2008) Nek5000: Open source spectral element CFD solver. http://nek5000.mcs.anl.gov
- 46.Patera AT (1984) A spectral element method for fluid dynamics: laminar flow in a channel expansion. J Comput Phys 54:468ADSCrossRefMATHGoogle Scholar
- 47.Maday Y, Patera AT (1989) Spectral element methods for the Navier–Stokes equations. In: Noor AK (ed) State of the art surveys in computational mechanics. ASME, New York, pp 71–143Google Scholar
- 48.Guala M, Hommema SE, Adrian RJ (2006) Large-scale and very-large-scale motions in turbulent pipe flow. J Fluid Mech 554:521ADSCrossRefMATHGoogle Scholar
- 49.Jiménez J, Hoyas S (2010) Turbulent fluctuations above the buffer layer of wall-bounded flows. J Fluid Mech 611:215MATHGoogle Scholar
- 50.Chin C, Ooi ASH, Marusic I, Blackburn M (2010) The influence of pipe length on turbulence statistics computed from direct numerical simulation data. Phys Fluids 22:115107ADSCrossRefGoogle Scholar
- 51.Panton RL (1996) Incompressible flow, 2nd edn. Wiley, ColoradoMATHGoogle Scholar
- 52.Hunt JCR, Wray AA, Moin P (1998) Eddies, streams, and convergence zones in turbulent flows. Center for Turbulence Research (CTR) Proceedings of Summer ProgramGoogle Scholar
- 53.Chong MS, Perry AE, Cantwell BJ (1990) A general classification of three-dimensional flow fields. Phys Fluids 5:765ADSMathSciNetCrossRefGoogle Scholar
- 54.Zhou J, Adrian RJ, Balachandar S, Kendali TM (1990) Mechanisms for generating coherent packets of hairpin vortices. J Fluid Mech 387:353ADSCrossRefMATHGoogle Scholar
- 55.Kida S, Miura H (1998) Identification and analysis of vortical structures. Eur J Mech B Fluids 17:471CrossRefMATHGoogle Scholar
- 56.Prandtl L (1926) Über die ausgebildete Turbulenz [turbulent flow]. Verh. 2nd Intl Kong. NACA Tech. Memo 62, 2nd Intl Kong. für Tech. Mech., Zürich. p. 435Google Scholar

## Copyright information

**Open Access**This article is distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution, and reproduction in any medium, provided you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons license, and indicate if changes were made.