Abstract
Wallbounded shear flows transitioning to turbulence may selforganize into alternating turbulent and laminar regions forming a stripe pattern with nontrivial oblique orientation. Different experiments and flow simulations identify oblique stripe patterns as the preferred solution of the wellknown NavierStokes equations, but the origin of stripes and their oblique orientation remains unexplained. In concluding his lectures, Feynman highlights the unexplained stripe pattern hidden in the solution space of the NavierStokes equations as an example demonstrating the need for improved theoretical tools to analyze the fluid flow equations. Here we exploit dynamical systems methods and demonstrate the existence of an exact equilibrium solution of the fully nonlinear 3D NavierStokes equations that resembles oblique stripe patterns in plane Couette flow. The stripe equilibrium emerges from the wellstudied Nagata equilibrium and exists only for a limited range of pattern angles. This suggests a mechanism selecting the nontrivial oblique orientation angle of turbulentlaminar stripes.
Introduction
The complex laminarturbulent transition in wallbounded shear flows is one of the least understood phenomena in fluid mechanics. In the simple geometry of plane Couette flow (PCF), the flow in a gap between two parallel plates moving in opposite directions, the transitional flow spontaneously breaks the translational symmetries in both the streamwise and the spanwise direction causing regions of turbulent and laminar flow to coexist in space^{1,2,3,4,5}. Remarkably, the flow may further selforganize into a regular pattern of alternating turbulent and laminar stripes^{6,7,8,9,10,11,12} also observed in TaylorCouette^{6, 13,14,15,16,17} and channel flow^{18,19,20,21,22}. The wavelength of these stripes or bands is much larger than the gap size, the only characteristic scale of the system, and they are oblique with respect to the streamwise direction. Consequently, both the largescale wavelength and the oblique orientation of turbulentlaminar stripes must directly follow from the flow dynamics captured by the governing Navier–Stokes equations. Experiments and numerical flow simulations reliably generate stripe patterns but a theory explaining the origin of the pattern characteristics is still missing. This is related to the Navier–Stokes equations being highly nonlinear partial differential equations, whose theoretical analysis remains challenging.
It was the early observation that an oblique turbulentlaminar pattern can be the preferred solution of the NavierStokes equations that motivated R. Feynman to stress the lack of “mathematical power [of his time] to analyze [the Navier–Stokes equations] except for very small Reynolds numbers”^{23}. Recent advances in numerical methods not only allow the simulation of flows but also the construction of exact equilibria, traveling waves and periodic orbits of the fully nonlinear 3D Navier–Stokes equations. These exact invariant solutions are believed to be embedded in a strange invariant set generating the chaotic dynamics of turbulent flow in the system’s state space^{24}. Consequently, a picture emerges where turbulent flow is described as a chaotic walk between dynamically unstable invariant solutions which together with their entangled stable and unstable manifolds support the turbulent dynamics^{25}. Exact invariant solutions are thus “building blocks” which resemble characteristic flow structures that are observed in flow simulations and experiments, when the dynamics transiently visits the exact invariant solution. A theoretical explanation of oblique stripe patterns within this dynamical systems description requires the as yet unsuccessful identification of exact invariant solutions resembling the detailed spatial structure of turbulentlaminar stripes, including their oblique orientation and largescale periodicity.
Nagata discovered the first invariant solution of PCF^{26,27,28}. Like most invariant solutions of PCF found since then^{29}, this socalled Nagata equilibrium is periodic in the streamwise and spanwise directions, repeating on the scale of the gap height. Such periodic solutions do not capture the coexistence of turbulent and laminar flow on scales much larger than the gap height and consequently cannot underly oblique stripes. Spanwise localized invariant solutions^{30, 31} and doubly localized invariant solutions in extended periodic domains^{32} show nonlinear flow structures coexisting with laminar flow but no known invariant solution captures oblique orientation or suggests a pattern wavelength matching oblique stripe patterns.
We present a fully nonlinear equilibrium solution of PCF (Fig. 1b), resembling the oblique stripe pattern observed in direct numerical simulations (Fig. 1a). Parametric continuation demonstrates that this stripe equilibrium is connected to the wellstudied Nagata equilibrium via two successive symmetrybreaking bifurcations, and that its existence is limited to oblique orientations.
Results
Simulating stripe patterns
For direct numerical simulations (DNS) of oblique stripe patterns in PCF we use a parallelized version of the pseudospectral code CHANNELFLOW^{25, 33}. The numerical domain is periodic in two perpendicular dimensions along the plates (x and z) with periods of (L_{x}, L_{z}) = (10, 40) in units of half the gap height. Noslip boundary conditions are imposed at the moving plates located at y = ±1. Inversion symmetry with respect to the domain center is enforced. The relative plate velocity and the associated base flow are tilted against the periodic domain dimensions at an angle of θ = 24° following Barkley and Tuckerman^{7}. At Reynolds number Re = Uh/ν = 350, with the relative plate velocity 2U, gap height 2h and kinematic viscosity ν the flow organizes into selfsustained turbulentlaminar stripes, as shown in Fig. 1a, where we periodically repeat the computational domain to highlight the largescale structure of the pattern.
Equilibrium resembling stripes
An invariant equilibrium solution capturing the stripes was found by introducing a largescale amplitude modulation to a known spatially periodic equilibrium using a suitable window function, similar to ref. ^{31}. Specifically, the Nagata equilibrium was periodically extended in the spanwise direction for n = 9 periods, then sheared to align the velocity streaks with the base flow in the tilted domain and finally multiplied with a scalar window function equal to a scaled mean field of turbulent kinetic energy of the oblique stripe pattern from several DNS runs. Using the constructed velocity field as initial guess, Newton iteration yields the stripe equilibrium (Fig. 1b).
The stripe equilibrium shares the smallscale wavy modulation with the Nagata equilibrium but also shows the largescale oblique amplitude modulation of the turbulentlaminar stripe pattern. The amplitude modulation between the highamplitude turbulent region and the lowamplitude laminar region of the equilibrium on average follows a sinusoidal profile closely resembling the pattern mean flow found in DNS at identical boundary conditions^{8}. The stripe equilibrium moreover captures detailed features of the turbulentlaminar interfaces. A base flow directed into a turbulent region leads to a sharper “upstream” interface than a base flow directed out of a turbulent region at a “downstream” interface. The direction of the base flow is reversed for y → −y. An upstream interface in the upper half thus corresponds to a downstream interface in the lower one. This gives rise to socalled overhang regions^{1, 34} and an asymmetry between the left and right interface in Fig. 1 where turbulent kinetic energy is visualized at y = 0.5 above the midplane. Finally, the stripe equilibrium is symmetric under inversion σ_{i}[u, v, w](x, y, z) = [−u, −v, −w] (−x, −y, −z), a symmetry also found for the mean flow of stripe patterns^{8}. The sinusoidal amplitude modulation, the captured overhang regions and the inversion symmetry, all characteristic of the pattern’s mean flow, together with the visual comparison in Fig. 1 show that the stripe equilibrium has the spatial features of the oblique stripe pattern. We have thus identified a first exact invariant solution underlying oblique turbulentlaminar patterns.
The unstable eigenspace of the evolution operator linearized around the equilibrium is spanned by 15 directions. The remaining ~10^{6} directions are attracting. Consequently, the dynamics is attracted towards the stripe equilibrium from almost all directions. The exponential growth rates ω_{r} along the unstable directions are small compared to typical turbulent time scales in the flow, given by the oscillatory frequencies ω_{i} in the spectrum of eigenvalues (Fig. 2). The low dimensional unstable eigenspace and the small exponential growth rates suggest a weakly unstable exact invariant solution that is a dynamically relevant transiently visited “building block” of the chaotic saddle underlying the turbulent flow.
Origin of the equilibrium
At small scales, the stripe equilibrium reflects the wavy streak structure of the spatially periodic Nagata equilibrium. This suggests that the stripe equilibrium emerges from the Nagata equilibrium in a bifurcation creating oblique longwavelength modulations. To identify this patternforming bifurcation numerically, the Nagata equilibrium needs to “fit” in an extended tilted periodic domain aligned with the wavevector of the neutral mode creating the oblique longwavelength modulation. The Nagata equilibrium indeed not only satisfies the streamwise and spanwise periodic boundary conditions of the commonly studied minimal flow domain but may also be periodic with respect to selected larger tilted domains. The symmetry group of the Nagata equilibrium, including all combined discrete translations over streamwisespanwise periods (λ_{st}, λ_{sp}), intersects with the group of translations of a tilted rectangular domain, with periodicity (L_{x}, L_{z}), if
is satisfied for \((k,l,m,n)\, \in \,{\Bbb N}\) and 0° < θ < 90°. Geometrically, condition (1) describes how the x–z coordinate lines of the tilted domain wind on a torus defined by the streamwisespanwise periodic minimal domain. The condition is satisfied if the coordinate lines are closed curves (Fig. 3a). For the domain (θ, L_{x}, L_{z}) = (24°, 10, 40) considered so far, the geometric condition (1) implies wavelengths (λ_{st}, λ_{sp}) = (1.02, 4.06) at which the Nagata equilibrium does not exist. Keeping L_{z} = 40 and choosing winding numbers (k, l, m, n) = (1, 1, 1, 9) however leads to a slightly modified domain (θ, L_{x}, L_{z}) = (18.4°, 40/3, 40) in which the Nagata equilibrium with (λ_{st}, λ_{sp}) = (12.65, 4.22) exists, as displayed in Fig. 3b. On the lower branch of the Nagata equilibrium close to the saddlenode bifurcation, there is a pitchfork bifurcation at Re_{I} = 164. Its neutrally stable longwavelength eigenmode, whose eigenvalue changes sign at Re_{I}, is plotted in Fig. 3c. This is the initial patternforming bifurcation creating oblique amplitude modulations on the Nagata equilibrium.
Using parametric continuation we follow both the periodic Nagata equilibrium (named \({\cal{A}}\) hereafter) and the emerging modulated equilibrium solution \(\left( {\cal{B}} \right)\) from its primary bifurcation point at (Re, θ, L_{x})_{I} = (164, 18.4°, 40/3) to the parameters \(({\mathrm{Re}},\,\theta ,\,L_x)_{\cal{C}} = (350,\,24^ \circ,\,10)\) of the stripe equilibrium \(\left( {\cal{C}} \right)\). In the three dimensional parameter space we choose a continuation path parametrized by tilt angle θ with the Reynolds number linear in θ, such that \({\mathrm{Re}}(\theta ) = \left( {{\mathrm{Re}}_{\mathrm{I}}(\theta _{\cal{C}}  \theta ) + {\mathrm{Re}}_{\cal{C}}(\theta  \theta _{\mathrm{I}})} \right)/(\theta _{\cal{C}}  \theta _{\mathrm{I}})\) and domain length L_{x}(θ) = L_{z}/(n tan(θ)) for n = 9 and constant domain width of L_{z} = 40. The resulting bifurcation diagram demonstrates that the Nagata equilibrium \({\cal{A}}\), is connected to the stripe equilibrium \({\cal{C}}\) (Fig. 4).
The primary bifurcation is of pitchfork type, subcritical, forward in Re and breaks the streamwise–spanwise translation symmetry of \({\cal{A}}\). Along the bifurcating branch of \({\cal{B}}\) significant amplitude modulations of the smallscale periodic signal form with period L_{z}/2 along z, as indicated by the doublepulse profile of the zdependent and x–yaveraged fluctuations u(z) at Re = 225 in Fig. 4b. The modulation period reflects a discrete translation symmetry \(\sigma _{\cal{B}}\) over half the domain diagonal, \(\sigma _{\cal{B}}[u,v,w](x,y,z) = [u,v,w](x + L_x/2,y,z + L_z/2)\). Equilibrium \({\cal{B}}\) inherits this symmetry from \({\cal{A}}\) because \(\sigma _{\cal{B}}\) is not broken by the neutral mode of the primary bifurcation (Fig. 3c).
A secondary patternforming bifurcation occurs at (Re, θ, L_{x})_{II} = (332, 23.4°, 10.3) along solution branch \({\cal{B}}\) (blue line in Fig. 4). This subcritical pitchfork bifurcation breaks the translation symmetry \(\sigma _{\cal{B}}\). The spatial period of the amplitude modulation is doubled and gives rise to solution branch \({\cal{C}}\) forming a singlepulse equilibrium. Solution branch \({\cal{C}}\) (red line in Fig. 4) reaches \(Re_{\cal{C}} = 350\) after undergoing an additional saddlenode bifurcation at (Re, θ, L_{x}) = (243, 20.8°, 11.7). The amplitude profiles of singlepulse and doublepulse equilibria show that the singlepulse with period L_{z} = 40 has large modulations at Re = 350 and θ = 24°, while the modulations in the doublepulse equilibrium are reduced (Fig. 4c). This agrees with the observations that stripes tend to have pattern wavelengths λ in the range of 40 ≤ λ ≤ 60 at Re around 350^{6, 10}. In summary, two bifurcations successively break discrete translation symmetries of the Nagata equilibrium to create the stripe equilibrium solution.
Smallscale velocity streaks carry a wavy modulation which has a streamwise phase that is clearly evident when plotting the streamwise vorticity at the midplane. We illustrate streamwise wave fronts by lines connecting vorticity maxima or minima in the spanwise direction (red/blue lines in Fig. 5). Straight and strictly spanwise oriented wave fronts indicate a constant streamwise phase of all streaks of the (spanwise periodic) Nagata equilibrium \({\cal{A}}\). The primary pattern forming bifurcation from \({\cal{A}}\) to \({\cal{B}}\) introduces local phase shifts which dislocate vorticity extrema away from a straight alignment and bend the wave front. The dislocations introduced into \({\cal{B}}\) are symmetric with respect to halfdomain translations \(\sigma _{\cal{B}}\) and centered at z = 0 and z = 20. For the stripe equilibrium \({\cal{C}}\) formed from \({\cal{B}}\) in the second pattern forming bifurcation, the topology of the wave fronts is preserved but they are geometrically deformed into sigmoidal structures.
In the turbulent region of equilibrium \({\cal{C}}\), the wave fronts of the wavy streaks are skewed at θ = 24° against the spanwise direction and oriented exactly along the pattern wave vector (\({\cal{C}}\) in Fig. 5). Assuming that all exact invariant solutions underlying stripe patterns show this alignment of wave fronts in the turbulent region with the pattern orientation, we conjecture that the range of possible skewing angles Nagatatype equilibria can sustain^{35} limits the range of angles at which oblique stripe patterns can exist.
Pattern angle selection
We identified equilibrium \({\cal{C}}\) at pattern angle θ = 24°. Continuation in θ for fixed pattern wavelength λ = 40 determines the range in θ for which the stripe equilibrium exists. At Re = 350, the equilibrium exists in the range 16.5° ≤ θ ≤ 26.1° before it undergoes saddlenode bifurcations (Fig. 6). Outside this range the stripe equilibrium is not sustained. The range of orientation angles over which the stripe equilibrium exists agrees with the range over which oblique stripe patterns of wavelength λ = 40 are observed in simulations^{8}. At lower Re, the range of allowed pattern angles shrinks and shifts towards larger values (Fig. 6). This trend of allowed θ for varying Re aligns with simulations and experiments of turbulentlaminar stripes^{8}. The finite existence range of the fully nonlinear exact equilibirum solution of the 3D Navier–Stokes equations thus appears to select the nontrivial angle at which selforganized turbulentlaminar stripes emerge in transitional shear flows.
Discussion
Experimental and numerical observations of selforganized oblique turbulentlaminar stripes in wallbounded extended shear flows suggest the existence of exact invariant solutions underlying these patterns. We present the first such invariant solution of the fully nonlinear 3D Navier–Stokes equations in plane Couette flow that captures the detailed spatial structure of oblique stripe patterns. The stripe equilibrium emerges from the known Nagata equilibrium via a sequence of two patternforming bifurcations with longwavelength oblique neutral modes. The existence of the stripe equilibrium at wavelength λ = 40 is limited to oblique orientations in a finite range of pattern angles around θ = 24°. The existence range agrees with simulations and experimental observations of turbulentlaminar stripes. This suggests a selection mechanism for the pattern angle and provides a route towards explaining why turbulentlaminar stripes are oblique.
Data availability
The fully resolved velocity field of the stripe equilibrium is provided as a data file in the supplementary material. The file format is NetCDF and can be directly imported in many postprocessing and visualization tools. Below, we specify the names of grid variables in the file and how to reproduce the equilibrium using the open source software CHANNELFLOW. The velocity field is numerically resolved in a domain of size (L_{x}, H, L_{z}) = (10, 2, 40) using a grid of size (N_{x}, N_{y}, N_{z}) = (42, 33, 340). The variables of the grid dimensions are named “X”, “Y” and “Z”, where “Y” is the wallnormal dimension. The components of the velocity vectors along each dimension are called “Velocity_X”, “Velocity_Y”, and “Velocity_Z”. The equilibrium solution can be checked for convergence and further analyzed using CHANNELFLOW. The Reynolds number of Re = 350 for plane Couette flow must be set using the flag “R 350”. To define the tilt angle of θ = 24° of the laminar base flow with respect to the domain dimensions, the flag “theta 0.4182” must be specified. Numerical stability requires a CFLnumber in the range of 0.2 < CFL < 0.4. The provided data file allows to reconstruct the data supporting the findings of this study. The data is also available from the corresponding author upon reasonable request.
Code availability
All numerical algorithms used in the present study are open source and can be downloaded via https://www.channelflow.ch.
References
 1.
Lundbladh, A. & Johansson, A. V. Direct simulation of turbulent spots in plane Couette flow. J. Fluid Mech. 229, 499–516 (1991).
 2.
Tillmark, N. & Alfredsson, P. H. Experiments on transition in plane Couette flow. J. Fluid Mech. 235, 89–102 (1992).
 3.
Daviaud, F., Hegseth, J. & Berge, P. Subcritical transition to turbulence in plane Couette flow. Phys. Rev. Lett. 69, 2511–2514 (1992).
 4.
Lemoult, G. et al. Directed percolation phase transition to sustained turbulence in Couette flow. Nat. Phys. 12, 254–258 (2016).
 5.
Couliou, M. & Monchaux, R. Growth dynamics of turbulent spots in plane Couette flow. J. Fluid Mech. 819, 1–20 (2017).
 6.
Prigent, A., Grégoire, G., Chaté, H., Dauchot, O. & van Saarloos, W. Largescale finitewavelength modulation within turbulent shear flows. Phys. Rev. Lett. 89, 014501 (2002).
 7.
Barkley, D. & Tuckerman, L. S. Computational study of turbulentlaminar patterns in Couette flow. Phys. Rev. Lett. 94, 014502 (2005).
 8.
Barkley, D. & Tuckerman, L. S. Mean flow of turbulentlaminar patterns in plane Couette flow. J. Fluid Mech. 576, 109–137 (2007).
 9.
Duguet, Y., Schlatter, P. & Henningson, D. S. Formation of turbulent patterns near the onset of transition in plane Couette flow. J. Fluid Mech. 650, 119–129 (2010).
 10.
Tuckerman, L. S. & Barkley, D. Patterns and dynamics in transitional plane Couette flow. Phys. Fluids 23, 041301 (2011).
 11.
Philip, J. & Manneville, P. From temporal to spatiotemporal dynamics in transitional plane Couette flow. Phys. Rev. E 83, 036308 (2011).
 12.
Ishida, T., Brethouwer, G., Duguet, Y. & Tsukahara, T. Laminarturbulent patterns with rough walls. Phys. Rev. Fluids 2, 073901 (2017).
 13.
Coles, D. Transition in circular Couette flow. J. Fluid. Mech. 21, 385–425 (1965).
 14.
Andereck, C. D., Liu, S. S. & Swinney, H. L. Flow regimes in a circular Couette system with independently rotating cylinders. J. Fluid Mech. 164, 155–183 (1986).
 15.
Hegseth, J. J., Andereck, C. D., Hayot, F. & Pomeau, Y. Spiral turbulence and phase dynamics. Phys. Rev. Lett. 62, 257–260 (1989).
 16.
Meseguer, A., Mellibovsky, F., Avila, M. & Marques, F. Instability mechanisms and transition scenarios of spiral turbulence in TaylorCouette flow. Phys. Rev. E 80, 1–4 (2009).
 17.
Dong, S. Evidence for internal structures of spiral turbulence. Phys. Rev. E 80, 1–4 (2009).
 18.
Tsukahara, T., Seki, Y., Kawamura, H. & Tochio, D. DNS of turbulent channel flow with very low Reynolds numbers. In Proc. Fourth International Symposium on Turbulence and Shear Flow Phenomena, 935–940 (2005).
 19.
Hashimoto, S., Hasobe, A., Tsukahara, T., Kawaguchi, Y. & Kawamura, H. An experimental study on turbulentstripe structure in transitional channel flow. Proc. Sixth International Symposium on Turbulence, Heat and Mass Transfer 193–196 (2009).
 20.
Aida, H., Tsukahara, T. & Kawaguchi, Y. Development of a turbulent spot into a stripe pattern in plane Poiseuille flow. Proc. Seventh International Symposium on Turbulence and Shear Flow Phenomena 1–6 (2011).
 21.
Tuckerman, L. S., Kreilos, T., Schrobsdorff, H., Schneider, T. M. & Gibson, J. F. Turbulentlaminar patterns in plane Poiseuille flow. Phys. Fluids 26, 114103 (2014).
 22.
Xiong, X., Tao, J., Chen, S. & Brandt, L. Turbulent bands in planePoiseuille flow at moderate Reynolds numbers. Phys. Fluids 27, 041702 (2015).
 23.
Feynman, R., Leighton, R. & Sands, M. The Feynman Lectures on Physics 2 (AddisonWesley, Reading, MA, 1964).
 24.
Lanford, O. E. The strange attractor theory of turbulence. Ann. Rev. Fluid Mech. 14, 347–364 (1982).
 25.
Gibson, J. F., Halcrow, J. & Cvitanović, P. Visualizing the geometry of state space in plane Couette flow. J. Fluid Mech. 611, 107–130 (2008).
 26.
Nagata, M. Threedimensional finiteamplitude solutions in plane Couette flow: bifurcation from infinity. J. Fluid Mech. 217, 519–527 (1990).
 27.
Clever, R. M. & Busse, F. H. Threedimensional convection in a horizontal fluid layer subjected to a constant shear. J. Fluid Mech. 234, 511–527 (1992).
 28.
Waleffe, F. Threedimensional coherent states in plane shear flows. Phys. Rev. Lett. 81, 4140–4143 (1998).
 29.
Gibson, J. F., Halcrow, J. & Cvitanović, P. Equilibrium and travelingwave solutions of plane Couette flow. J. Fluid Mech. 638, 243–266 (2009).
 30.
Schneider, T. M., Gibson, J. F. & Burke, J. Snakes and ladders: localized solutions of plane Couette flow. Phys. Rev. Lett. 104, 104501 (2010).
 31.
Gibson, J. F. & Brand, E. Spanwiselocalized solutions of planar shear flows. J. Fluid Mech. 745, 25–61 (2014).
 32.
Brand, E. & Gibson, J. F. A doublylocalized equilibrium solution of plane Couette flow. J. Fluid Mech. 750, R3 (2014).
 33.
Gibson, J. F. et al. Channelflow 2.0. https://www.channelflow.ch. Accessed 10 April 2019.
 34.
Duguet, Y. & Schlatter, P. Oblique laminarturbulent interfaces in plane shear flows. Phys. Rev. Lett. 110, 034502 (2013).
 35.
Gibson, J. F. & Schneider, T. M. Homoclinic snaking in plane Couette flow: bending, skewing and finitesize effects. J. Fluid Mech. 794, 530–551 (2016).
Acknowledgements
This work was supported by the Swiss National Science Foundation (SNF) under grant no. 200021160088.
Author information
Affiliations
Contributions
T.M.S. conceived the project. F.R. carried out the research under supervision of T.M.S. and with initial input of T.K. The manuscript was prepared by F.R. and T.M.S., in correspondence with T.K.
Corresponding author
Correspondence to Tobias M. Schneider.
Ethics declarations
Competing interests
The authors declare no competing interests.
Additional information
Journal peer review information: Nature Communications thanks Takahiro Tsukahara, Genta Kawahara, and other anonymous reviewers for their contribution to the peer review of this work. Peer reviewer reports are available.
Publisher’s note: Springer Nature remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.
Supplementary information
Rights and permissions
Open Access This article is licensed under a Creative Commons Attribution 4.0 International License, which permits use, sharing, adaptation, distribution and reproduction in any medium or format, as long as 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. The images or other third party material in this article are included in the article’s Creative Commons license, unless indicated otherwise in a credit line to the material. If material is not included in the article’s Creative Commons license and your intended use is not permitted by statutory regulation or exceeds the permitted use, you will need to obtain permission directly from the copyright holder. To view a copy of this license, visit http://creativecommons.org/licenses/by/4.0/.
About this article
Cite this article
Reetz, F., Kreilos, T. & Schneider, T.M. Exact invariant solution reveals the origin of selforganized oblique turbulentlaminar stripes. Nat Commun 10, 2277 (2019). https://doi.org/10.1038/s4146701910208x
Received:
Accepted:
Published:
Further reading

Heat transfer of transitional regime with helical turbulence in annular flow
International Journal of Heat and Fluid Flow (2020)

Patterns in WallBounded Shear Flows
Annual Review of Fluid Mechanics (2020)

Origin of localized snakesandladders solutions of plane Couette flow
Physical Review E (2019)
Comments
By submitting a comment you agree to abide by our Terms and Community Guidelines. If you find something abusive or that does not comply with our terms or guidelines please flag it as inappropriate.