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Publications (10 of 234) Show all publications
Dogan, E., Örlü, R., Gatti, D., Vinuesa, R. & Schlatter, P. (2019). Quantification of amplitude modulation in wall-bounded turbulence. Paper presented at Inernational Camp-Style Seminar on Dynamics of Wall-Bounded Shear Flows, AUG 31-SEP 02, 2016, Kyoto, JAPAN. Fluid Dynamics Research, 51(1), Article ID 011408.
Open this publication in new window or tab >>Quantification of amplitude modulation in wall-bounded turbulence
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2019 (English)In: Fluid Dynamics Research, ISSN 0169-5983, E-ISSN 1873-7005, Vol. 51, no 1, article id 011408Article in journal (Refereed) Published
Abstract [en]

Many recent investigations on the scale interactions in wall-bounded turbulent flows focus on describing so-called amplitude modulation, the phenomenon that deals with the influence of large scales in the outer region on the amplitude of the small-scale fluctuations in the near-wall region. The present study revisits this phenomenon regarding two aspects, namely the method for decomposing the scales and the quantification of the modulation. First, the paper presents a summary of the literature that has dealt with either or both aspects. Second, for decomposing the scales, different spectral filters (temporal, spatial or both) and empirical mode decomposition (EMD) are evaluated and compared. The common data set is a well-resolved large-eddy simulation that offers a wide range of Reynolds numbers spanning Re-theta = 880-8200. The quantification of the amplitude modulation is discussed for the resulting scale components. Particular focus is given to evaluate the efficacy of the various filters to separate scales for the range of Reynolds numbers of interest. Different to previous studies, the different methods have been evaluated using the same data set, thereby allowing a fair comparison between the various approaches. It is observed that using a spectral filter in the spanwise direction is an effective approach to separate the small and large scales in the flow, even at comparably low Reynolds numbers, whereas filtering in time should be approached with caution in the low-to-moderate Re range. Additionally, using filters in both spanwise and time directions, which would separate both wide and long-living structures from the small and fast scales, gives a cleaner image for the small-scales although the contribution to the scales interaction from that filter implementation has been found negligible. Applying EMD to decompose the scales gives similar results to Fourier filters for the energy content of the scales and thereby for the quantification of the amplitude modulation using the decomposed scales. No direct advantage of EMD over classical Fourier filters could be seen. Potential issues regarding different decomposition methods and different definitions of the amplitude modulation are also discussed.

Place, publisher, year, edition, pages
IOP PUBLISHING LTD, 2019
Keywords
amplitude modulation, turbulent boundary layer, scale interaction
National Category
Fluid Mechanics and Acoustics
Identifiers
urn:nbn:se:kth:diva-243936 (URN)10.1088/1873-7005/aaca81 (DOI)000456203700009 ()2-s2.0-85061429605 (Scopus ID)
Conference
Inernational Camp-Style Seminar on Dynamics of Wall-Bounded Shear Flows, AUG 31-SEP 02, 2016, Kyoto, JAPAN
Note

QC 20190306

Available from: 2019-03-06 Created: 2019-03-06 Last updated: 2019-03-18Bibliographically approved
Sasaki, K., Vinuesa, R., Cavalieri, A. V. G., Schlatter, P. & Henningson, D. S. (2019). Transfer functions for flow predictions in wall-bounded turbulence. Journal of Fluid Mechanics, 864, 708-745
Open this publication in new window or tab >>Transfer functions for flow predictions in wall-bounded turbulence
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2019 (English)In: Journal of Fluid Mechanics, ISSN 0022-1120, E-ISSN 1469-7645, Vol. 864, p. 708-745Article in journal (Refereed) Published
Abstract [en]

Three methods are evaluated to estimate the streamwise velocity fluctuations of a zero-pressure-gradient turbulent boundary layer of momentum-thickness-based Reynolds number up to using as input velocity fluctuations at different wall-normal positions. A system identification approach is considered where large-eddy simulation data are used to build single and multiple-input linear and nonlinear transfer functions. Such transfer functions are then treated as convolution kernels and may be used as models for the prediction of the fluctuations. Good agreement between predicted and reference data is observed when the streamwise velocity in the near-wall region is estimated from fluctuations in the outer region. Both the unsteady behaviour of the fluctuations and the spectral content of the data are properly predicted. It is shown that approximately 45 % of the energy in the near-wall peak is linearly correlated with the outer-layer structures, for the reference case. These identified transfer functions allow insight into the causality between the different wall-normal locations in a turbulent boundary layer along with an estimation of the tilting angle of the large-scale structures. Differences in accuracy of the methods (single- and multiple-input linear and nonlinear) are assessed by evaluating the coherence of the structures between wall-normally separated positions. It is shown that the large-scale fluctuations are coherent between the outer and inner layers, by means of an interactions which strengthens with increasing Reynolds number, whereas the finer-scale fluctuations are only coherent within the near-wall region. This enables the possibility of considering the wall-shear stress as an input measurement, which would more easily allow the implementation of these methods in experimental applications. A parametric study was also performed by evaluating the effect of the Reynolds number, wall-normal positions and input quantities considered in the model. Since the methods vary in terms of their complexity for implementation, computational expense and accuracy, the technique of choice will depend on the application under consideration. We also assessed the possibility of designing and testing the models at different Reynolds numbers, where it is shown that the prediction of the near-wall peak from wall-shear-stress measurements is practically unaffected even for a one order of magnitude change in the corresponding Reynolds number of the design and test, indicating that the interaction between the near-wall peak fluctuations and the wall is approximately Reynolds-number independent. Furthermore, given the performance of such methods in the prediction of flow features in turbulent boundary layers, they have a good potential for implementation in experiments and realistic flow control applications, where the prediction of the near-wall peak led to correlations above 0.80 when wall-shear stress was used in a multiple-input or nonlinear scheme. Errors of the order of 20 % were also observed in the determination of the near-wall spectral peak, depending on the employed method.

Place, publisher, year, edition, pages
CAMBRIDGE UNIV PRESS, 2019
Keywords
turbulence modelling, turbulent boundary layers
National Category
Fluid Mechanics and Acoustics
Identifiers
urn:nbn:se:kth:diva-245119 (URN)10.1017/jfm.2019.27 (DOI)000458488900001 ()2-s2.0-85061456245 (Scopus ID)
Note

QC 20190315

Available from: 2019-03-15 Created: 2019-03-15 Last updated: 2019-03-15Bibliographically approved
Rezaeiravesh, S., Vinuesa, R., Liefvendahl, M. & Schlatter, P. (2018). Assessment of uncertainties in hot-wire anemometry and oil-film interferometry measurements for wall-bounded turbulent flows. European journal of mechanics. B, Fluids, 72, 57-73
Open this publication in new window or tab >>Assessment of uncertainties in hot-wire anemometry and oil-film interferometry measurements for wall-bounded turbulent flows
2018 (English)In: European journal of mechanics. B, Fluids, ISSN 0997-7546, E-ISSN 1873-7390, Vol. 72, p. 57-73Article in journal (Refereed) Published
Abstract [en]

In this study, the sources of uncertainty of hot-wire anemometry (HWA) and oil-film interferometry (OFI) measurements are assessed. Both statistical and classical methods are used for the forward and inverse problems, so that the contributions to the overall uncertainty of the measured quantities can be evaluated. The correlations between the parameters are taken into account through the Bayesian inference with error-in-variable (EiV) model. In the forward problem, very small differences were found when using Monte Carlo (MC), Polynomial Chaos Expansion (PCE) and linear perturbation methods. In flow velocity measurements with HWA, the results indicate that the estimated uncertainty is lower when the correlations among parameters are considered, than when they are not taken into account. Moreover, global sensitivity analyses with Sobol indices showed that the HWA measurements are most sensitive to the wire voltage, and in the case of OFI the most sensitive factor is the calculation of fringe velocity. The relative errors in wall-shear stress, friction velocity and viscous length are 0.44%, 0.23% and0.22%, respectively. Note that these values are lower than the ones reported in other wall-bounded turbulence studies. Note that in most studies of wall-bounded turbulence the correlations among parameters are not considered, and the uncertainties from the various parameters are directly added when determining the overall uncertainty of the measured quantity. In the present analysis we account for these correlations, which may lead to a lower overall uncertainty estimate due to error cancellation Furthermore, our results also indicate that the crucial aspect when obtaining accurate inner-scaled velocity measurements is the wind-tunnel flow quality, which is more critical than the accuracy in wall-shear stress measurements.

Place, publisher, year, edition, pages
Elsevier, 2018
Keywords
Hot-wire anemometry, Oil-film interferometry, Uncertainty quantification, Wall-bounded turbulence
National Category
Applied Mechanics
Identifiers
urn:nbn:se:kth:diva-228692 (URN)10.1016/j.euromechflu.2018.04.012 (DOI)000447570200005 ()2-s2.0-85047057608 (Scopus ID)
Funder
Swedish Research CouncilKnut and Alice Wallenberg Foundation
Note

QC 20180530

Available from: 2018-05-30 Created: 2018-05-30 Last updated: 2018-11-06Bibliographically approved
Wang, Z., Örlü, R., Schlatter, P. & Chung, Y. M. (2018). Direct numerical simulation of a turbulent 90° bend pipe flow. International Journal of Heat and Fluid Flow, 73, 199-208
Open this publication in new window or tab >>Direct numerical simulation of a turbulent 90° bend pipe flow
2018 (English)In: International Journal of Heat and Fluid Flow, ISSN 0142-727X, E-ISSN 1879-2278, Vol. 73, p. 199-208Article in journal (Refereed) Published
Abstract [en]

Direct numerical simulation (DNS) has been performed for a spatially developing 90° bend pipe flow to investigate the unsteady flow motions downstream of the bend. A recycling method is implemented to generate a fully-developed turbulent inflow condition. The Reynolds number of the pipe flow is ReD=5300 and the bend curvature is γ=0.4. A long straight pipe section (40D) is attached in the downstream of the bend to allow the flow to develop. Flow oscillations downstream of the bend are measured using several methods, and the corresponding oscillation frequencies are estimated. It is found that different characteristic frequencies are obtained from various flow measurements. The stagnation point movement and single-point velocity measurements may not be good measures to determine the swirl-switching frequency. The oscillations of the lateral pressure force on the pipe wall and half-sided mass flow rate are proposed to be a more unambiguous measure of the unsteady flow motions downstream of the bend. 

Place, publisher, year, edition, pages
Elsevier B.V., 2018
Keywords
90 degrees bend, Conditional averaging, Curved pipe, DNS, Swirl switching, Turbulent pipe flow, Direct numerical simulation, Flow rate, Numerical models, Pipe flow, Reynolds number, Turbulent flow, Characteristic frequencies, Curved pipes, Oscillation frequency, Stagnation points, Turbulent inflow conditions, Oscillating flow
National Category
Mechanical Engineering
Identifiers
urn:nbn:se:kth:diva-236662 (URN)10.1016/j.ijheatfluidflow.2018.08.003 (DOI)2-s2.0-85052536769 (Scopus ID)
Note

Export Date: 22 October 2018; Article; CODEN: IJHFD; Correspondence Address: Chung, Y.M.; School of Engineering and Centre for Scientific Computing, University of WarwickUnited Kingdom; email: y.m.chung@warwick.ac.uk; Funding details: University of Warwick; Funding details: EP/L000261/1, EPSRC, Engineering and Physical Sciences Research Council; Funding text: This work has been supported by the Engineering and Physical Sciences Research Council grant no EP/L000261/1 . The authors would like to thank Professor Paul Fischer for the help in using Nek5000 . Simulations were performed on ARCHER, the UK National Supercomputing Service. This work also used the HPC facilities (Tinis) at the Centre for Scientific Computing, University of Warwick. QC 20181113

Available from: 2018-11-13 Created: 2018-11-13 Last updated: 2018-11-13Bibliographically approved
Rinaldi, E., Schlatter, P. & Bagheri, S. (2018). Edge state modulation by mean viscosity gradients. Journal of Fluid Mechanics, 838, 379-403
Open this publication in new window or tab >>Edge state modulation by mean viscosity gradients
2018 (English)In: Journal of Fluid Mechanics, ISSN 0022-1120, E-ISSN 1469-7645, Vol. 838, p. 379-403Article in journal (Refereed) Published
Abstract [en]

Motivated by the relevance of edge state solutions as mediators of transition, we use direct numerical simulations to study the effect of spatially non-uniform viscosity on their energy and stability in minimal channel flows. What we seek is a theoretical support rooted in a fully nonlinear framework that explains the modified threshold for transition to turbulence in flows with temperature-dependent viscosity. Consistently over a range of subcritical Reynolds numbers, we find that decreasing viscosity away from the walls weakens the streamwise streaks and the vortical structures responsible for their regeneration. The entire self-sustained cycle of the edge state is maintained on a lower kinetic energy level with a smaller driving force, compared to a flow with constant viscosity. Increasing viscosity away from the walls has the opposite effect. In both cases, the effect is proportional to the strength of the viscosity gradient. The results presented highlight a local shift in the state space of the position of the edge state relative to the laminar attractor with the consequent modulation of its basin of attraction in the proximity of the edge state and of the surrounding manifold. The implication is that the threshold for transition is reduced for perturbations evolving in the neighbourhood of the edge state in the case that viscosity decreases away from the walls, and vice versa.

Place, publisher, year, edition, pages
Cambridge University Press, 2018
Keywords
nonlinear dynamical systems, nonlinear instability, transition to turbulence
National Category
Fluid Mechanics and Acoustics
Identifiers
urn:nbn:se:kth:diva-222027 (URN)10.1017/jfm.2017.921 (DOI)2-s2.0-85040834445 (Scopus ID)
Funder
Swedish e‐Science Research Center
Note

QC 20180131

Available from: 2018-01-31 Created: 2018-01-31 Last updated: 2018-11-14Bibliographically approved
Chin, C., Vinuesa, R., Örlü, R., Cardesa, J. I., Noorani, A., Schlatter, P. & Chong, M. S. (2018). Flow topology of rare back flow events and critical points in turbulent channels and toroidal pipes. In: Journal of Physics: Conference Series. Paper presented at 3rd Madrid Summer School on Turbulence, School of Aeronautics of the Universidad Politecnica de MadridMadrid, Spain, 29 May 2017 through 30 June 2017. Institute of Physics Publishing (IOPP), 1001(1), Article ID 012002.
Open this publication in new window or tab >>Flow topology of rare back flow events and critical points in turbulent channels and toroidal pipes
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2018 (English)In: Journal of Physics: Conference Series, Institute of Physics Publishing (IOPP), 2018, Vol. 1001, no 1, article id 012002Conference paper, Published paper (Refereed)
Abstract [en]

A study of the back flow events and critical points in the flow through a toroidal pipe at friction Reynolds number Reτ ≈ 650 is performed and compared with the results in a turbulent channel flow at Reτ ≈ 934. The statistics and topological properties of the back flow events are analysed and discussed. Conditionally-averaged flow fields in the vicinity of the back flow event are obtained, and the results for the torus show a similar streamwise wall-shear stress topology which varies considerably for the spanwise wall-shear stress when compared to the channel flow. The comparison between the toroidal pipe and channel flows also shows fewer back flow events and critical points in the torus. This cannot be solely attributed to differences in Reynolds number, but is a clear effect of the secondary flow present in the toroidal pipe. A possible mechanism is the effect of the secondary flow present in the torus, which convects momentum from the inner to the outer bend through the core of the pipe, and back from the outer to the inner bend through the pipe walls. In the region around the critical points, the skin-friction streamlines and vorticity lines exhibit similar flow characteristics with a node and saddle pair for both flows. These results indicate that back flow events and critical points are genuine features of wall-bounded turbulence, and are not artifacts of specific boundary or inflow conditions in simulations and/or measurement uncertainties in experiments.

Place, publisher, year, edition, pages
Institute of Physics Publishing (IOPP), 2018
Series
Journal of Physics: Conference Series, ISSN 1742-6588 ; 1001
National Category
Fluid Mechanics and Acoustics
Identifiers
urn:nbn:se:kth:diva-238246 (URN)10.1088/1742-6596/1001/1/012002 (DOI)000454926900002 ()2-s2.0-85046100946 (Scopus ID)
Conference
3rd Madrid Summer School on Turbulence, School of Aeronautics of the Universidad Politecnica de MadridMadrid, Spain, 29 May 2017 through 30 June 2017
Note

QC 20181101

Available from: 2018-11-01 Created: 2018-11-01 Last updated: 2019-01-18Bibliographically approved
Otero, E., Vinuesa, R., Marin, O., Laure, E. & Schlatter, P. (2018). Lossy Data Compression Effects on Wall-bounded Turbulence: Bounds on Data Reduction. Flow Turbulence and Combustion, 101(2), 365-387
Open this publication in new window or tab >>Lossy Data Compression Effects on Wall-bounded Turbulence: Bounds on Data Reduction
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2018 (English)In: Flow Turbulence and Combustion, ISSN 1386-6184, E-ISSN 1573-1987, Vol. 101, no 2, p. 365-387Article in journal (Refereed) Published
Abstract [en]

Postprocessing and storage of large data sets represent one of the main computational bottlenecks in computational fluid dynamics. We assume that the accuracy necessary for computation is higher than needed for postprocessing. Therefore, in the current work we assess thresholds for data reduction as required by the most common data analysis tools used in the study of fluid flow phenomena, specifically wall-bounded turbulence. These thresholds are imposed a priori by the user in L (2)-norm, and we assess a set of parameters to identify the minimum accuracy requirements. The method considered in the present work is the discrete Legendre transform (DLT), which we evaluate in the computation of turbulence statistics, spectral analysis and resilience for cases highly-sensitive to the initial conditions. Maximum acceptable compression ratios of the original data have been found to be around 97%, depending on the application purpose. The new method outperforms downsampling, as well as the previously explored data truncation method based on discrete Chebyshev transform (DCT).

Place, publisher, year, edition, pages
Springer, 2018
Keywords
Lossy data compression, Data reduction, Turbulence statistics, Orthogonal polynomials, Resilience
National Category
Bioinformatics (Computational Biology)
Identifiers
urn:nbn:se:kth:diva-237136 (URN)10.1007/s10494-018-9923-5 (DOI)000446583900006 ()2-s2.0-85047423287 (Scopus ID)
Funder
Swedish Foundation for Strategic Research Knut and Alice Wallenberg FoundationSwedish Research Council
Note

QC 20181025

Available from: 2018-10-25 Created: 2018-10-25 Last updated: 2018-10-25Bibliographically approved
Otero, E., Gong, J., Min, M., Fischer, P., Schlatter, P. & Laure, E. (2018). OpenACC accelerator for the Pn-Pn-2 algorithm in Nek5000. In: Proceedings of the 5th International Conference on Exascale Applications and Software: . Paper presented at The 5th International Conference on Exascale Applications and Software, 17th to 19th April 2018 in Edinburgh, Scotland.
Open this publication in new window or tab >>OpenACC accelerator for the Pn-Pn-2 algorithm in Nek5000
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2018 (English)In: Proceedings of the 5th International Conference on Exascale Applications and Software, 2018Conference paper, Oral presentation with published abstract (Refereed)
National Category
Computer and Information Sciences
Identifiers
urn:nbn:se:kth:diva-232362 (URN)978-0-9926615-3-3 (ISBN)
Conference
The 5th International Conference on Exascale Applications and Software, 17th to 19th April 2018 in Edinburgh, Scotland
Note

QC 20180725

Available from: 2018-07-20 Created: 2018-07-20 Last updated: 2018-07-25Bibliographically approved
Vidal, A., Nagib, H. M., Schlatter, P. & Vinuesa, R. (2018). Secondary flow in spanwise-periodic in-phase sinusoidal channels. Journal of Fluid Mechanics, 851, 288-316
Open this publication in new window or tab >>Secondary flow in spanwise-periodic in-phase sinusoidal channels
2018 (English)In: Journal of Fluid Mechanics, ISSN 0022-1120, E-ISSN 1469-7645, Vol. 851, p. 288-316Article in journal (Refereed) Published
Abstract [en]

Direct numerical simulations (DNSs) are performed to analyse the secondary flow of Prandtl's second kind in fully developed spanwise-periodic channels with in-plane sinusoidal walls. The secondary flow is characterized for different combinations of wave parameters defining the wall geometry at Re-h = 2500 and 5000, where h is the half-height of the channel. The total cross-flow rate in the channel Q(yz) is defined along with a theoretical model to predict its behaviour. Interaction between the secondary flows from opposite walls is observed if lambda similar or equal to h similar or equal to A, where A and lambda are the amplitude and wavelength of the sinusoidal function defining the wall geometry. As the outer-scaled wavelength (lambda/h) is reduced, the secondary vortices become smaller and faster, increasing the total cross-flow rate per wall. However, if the inner-scaled wavelength (lambda(+)) is below 130 viscous units, the cross-flow decays for smaller wavelengths. By analysing cases in which the wavelength of the wall is much smaller than the half-height of the channel lambda << h, we show that the cross-flow distribution depends almost entirely on the separation between the scales of the instantaneous vortices, where the upper and lower bounds are determined by lambda/h and lambda(+), respectively. Therefore, the distribution of the secondary flow relative to the size of the wave at a given Re-h can be replicated at higher Re-h by decreasing lambda/h and keeping lambda(+) constant. The mechanisms that contribute to the mean cross-flow are analysed in terms of the Reynolds stresses and using quadrant analysis to evaluate the probability density function of the bursting events. These events are further classified with respect to the sign of their instantaneous spanwise velocities. Sweeping events and ejections are preferentially located in the valleys and peaks of the wall, respectively. The sweeps direct the instantaneous cross-flow from the core of the channel towards the wall, turning in the wall-tangent direction towards the peaks. The ejections drive the instantaneous cross-flow from the near-wall region towards the core. This preferential behaviour is identified as one of the main contributors to the secondary flow.

Place, publisher, year, edition, pages
Cambridge University Press, 2018
Keywords
turbulence simulation, turbulent flows
National Category
Fluid Mechanics and Acoustics
Identifiers
urn:nbn:se:kth:diva-232762 (URN)10.1017/jfm.2018.498 (DOI)000439307100010 ()2-s2.0-85050633237 (Scopus ID)
Funder
Swedish Research CouncilKnut and Alice Wallenberg FoundationSwedish e‐Science Research Center
Note

QC 20180803

Available from: 2018-08-03 Created: 2018-08-03 Last updated: 2018-08-06Bibliographically approved
Vinuesa, R., Schlatter, P. & Nagib, H. M. (2018). Secondary flow in turbulent ducts with increasing aspect ratio. PHYSICAL REVIEW FLUIDS, 3(5), Article ID 054606.
Open this publication in new window or tab >>Secondary flow in turbulent ducts with increasing aspect ratio
2018 (English)In: PHYSICAL REVIEW FLUIDS, ISSN 2469-990X, Vol. 3, no 5, article id 054606Article in journal (Refereed) Published
Abstract [en]

Direct numerical simulations of turbulent duct flows with aspect ratios 1, 3, 5, 7, 10, and 14.4 at a center-plane friction Reynolds number Re-tau,Re- c similar or equal to 180, and aspect ratios 1 and 3 at Re-tau,Re- c similar or equal to 360, were carried out with the spectral-element code NEK5000. The aim of these simulations is to gain insight into the kinematics and dynamics of Prandtl's secondary flow of the second kind and its impact on the flow physics of wall-bounded turbulence. The secondary flow is characterized in terms of the cross-plane component of the mean kinetic energy, and its variation in the spanwise direction of the flow. Our results show that averaging times of around 3000 convective time units (based on duct half-height h) are required to reach a converged state of the secondary flow, which extends up to a spanwise distance of around similar or equal to 5h measured from the side walls. We also show that if the duct is not wide enough to accommodate the whole extent of the secondary flow, then its structure is modified as reflected through a different spanwise distribution of energy. Another confirmation of the extent of the secondary flow is the decay rate of kinetic energy of any remnant secondary motions for z(c)/h > 5 (where z(c) is the spanwise distance from the corner) in aspect ratios 7, 10, and 14.4, which exhibits a decreasing level of energy with increasing averaging time t(a), and in its rapid rate of decay given by similar to t(a)(-1). This is the same rate of decay observed in a spanwise-periodic channel simulation, which suggests that at the core, the kinetic energy of the secondary flow integrated over the cross-sectional area, < K >(yz), behaves as a random variable with zero mean, with rate of decay consistent with central limit theorem. Long-time averages of statistics in a region of rectangular ducts extending about the width of a well-designed channel simulation (i.e., extending about similar or equal to 3h on each side of the center plane) indicate that ducts or experimental facilities with aspect ratios larger than 10 may, if properly designed, exhibit good agreement with results obtained from spanwise-periodic channel computations.

Place, publisher, year, edition, pages
American Physical Society, 2018
Keywords
Direct Numerical-Simulation, Straight Square Duct, Boundary-Layers, Rectangular Ducts, Reynolds-Numbers, Shear, Wall
National Category
Fluid Mechanics and Acoustics
Identifiers
urn:nbn:se:kth:diva-230444 (URN)10.1103/PhysRevFluids.3.054606 (DOI)000433036100004 ()2-s2.0-85049037220 (Scopus ID)
Funder
Knut and Alice Wallenberg FoundationSwedish Research CouncilSwedish e‐Science Research Center
Note

QC 20180614

Available from: 2018-06-14 Created: 2018-06-14 Last updated: 2018-10-16Bibliographically approved
Organisations
Identifiers
ORCID iD: ORCID iD iconorcid.org/0000-0001-9627-5903

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