Transitjon in subcritjcal shear fmows Invariant solutjons and the - - PowerPoint PPT Presentation

transitjon in subcritjcal shear fmows invariant solutjons
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Transitjon in subcritjcal shear fmows Invariant solutjons and the - - PowerPoint PPT Presentation

Transitjon in subcritjcal shear fmows Invariant solutjons and the edge of chaos. Ashley P. Willis 1 , Rich Kerswell 2 , Predrag Cvitanovi 3 , Yohann Duguet 4 1 School of Mathematjcs and Statjstjcs, University of Sheffjeld. 2 DAMTP,


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Transitjon in subcritjcal shear fmows – Invariant solutjons and the edge of chaos.

Ashley P. Willis 1, Rich Kerswell 2, Predrag Cvitanović 3, Yohann Duguet 4

1 School of Mathematjcs and Statjstjcs, University of Sheffjeld. 2 DAMTP, University of Cambridge. 3 School of Physics, Georgia Tech. (chaosbook.org) 4 LIMSI-CNRS, Orsay, France.

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Peixinho & Mullin, PRL Illuminated fmakes Axial vortjcity Simulatjon

Localised turbulence in a pipe

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APPROACH: TURBULENCE AS A CHAOTIC DYNAMICAL SYTSTEM

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Trajectory in phase space, structured by stable/unstable manifolds

  • f the equilibrium points.
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Jacobian-free Newton-Krylov

  • Only involves evaluatjons of F(x).
  • No preconditjoner necessary!

Knoll and Keyes (2004) Viswanath (2007)

→ GMRES

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Jacobian-free Newton-Krylov

Knoll and Keyes (2004) Viswanath (2007)

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Stabilise Newton: Don’t take too large step δx ... Knoll and Keyes (2004) Viswanath (2007)

GMRES:

Jacobian-free Newton-Krylov - Hookstep

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Code at openpipefmow.org (non-problem specifjc: black box) arxiv:1908.06730

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PROBLEMS

  • 1. Where to get startjng guess x0 !?
  • 2. Look for recurrences: ‘small’

how small? what norm!?

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Observed importance of combination Re = LU / ν L, diameter U, mean axial flow ν, kinematic viscosity

Osborne Reynolds’ Experiments, 1883

“The only idea I had formed before commencing the experiments, was that at some critical velocity the motion must become unstable, so that any disturbance from perfectly steady motion would result in eddies.”

i.e. surprised to not find critical flow rate for linear instability

“…the steady motion breaks down suddenly… for disturbances of the magnitude that cause it to break down… while it is stable for a smaller disturbance…”

i.e. finite amplitude disturbance required to trigger turbulence

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Re (fmow rate)

1

10 103 104 105 106 Turbulent frictjon / Laminar frictjon (drag).

Laminar Intermittent Turbulent

102

Adapted from Nikuradse (1950) / Blasius (1913) Turbulent frictjon Laminar frictjon

slope approx 0.75

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Subcritjcal instability, nonlinearity important

Saddle-node bifurcatjon

|| u’ || Re Re || u’ || ?

linearly stable laminar-turbulent boundary

  • r ‘edge of chaos’

‘turbulence’ Disconnected from laminar state. Q: how to fjnd states?

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Shear Flows U U 2L 2U L Couetue fmow channel fmow pipe fmow Reynolds number Re = LU /  Kinematjc viscosity 

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turbulence linear Re

  • bserved

instability Pipe fmow 1720 inf.? Channel fmow 950 5772 ASBL 367 54370 Couetue fmow 312 inf.

Stability of shear-fmows

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Travelling Waves (TWs) Flow rate laminar

Pipe fmow

Re=81

lower bound, energy stability theory

Re≈2000 Turbulence observed

(Faisst & Kerswell 2003) lowest fjnite-amplitude solutjon

m=2, m=3

Re>770 (Pringle & Kerswell 2007) lowest fjnite-amplitude solutjon

m=1

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Travelling Waves (TWs) / Vortex-Wave Interactjon (VWI) state / ‘Exact’ Coherent Structures (ECS) / Invariant Solutjons

[Boundary-layer: ] Hall & Smith (1991), via asymptotjc theory. [Plane-couetue:] Walefge (1998), via contjnuatjon from Taylor-Couetue

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S2 S3 S4 S5

Streaks near walls Slower core

Faisst & Eckhardt (2003) Wedin & Kerswell (2004)

Travelling Wave solutjons (TWs)

[Pipe:] via (painful) contjnuatjon from system with body force

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Force 2D streaks 3D instability Reduce force

Discovery of TWs. (Self sustaining cycle completed ‘by hand’!)

START: least-stable 2D eigen mode  Force

Level of forcing

END: unforced 3D state, self-sustained

Faisst & Eckhardt (2003) Wedin & Kerswell (2004)

  • A lot can go wrong!
  • State really linked to dynamics?
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Trajectory in phase space, structured by stable/unstable manifolds

  • f the equilibrium points.

Dimension of the space N → inf., In simulatjons, N = O(105-106), dimension of unstable manifolds n = O(10)

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Laminar stable point Unstable TW becomes aturactor within ‘edge’ Turbulence

Laminar turbulent boundary calculated by bisectjon: Skufca, Yorke & Eckardt (2006) for a reduced model of shear fmow Schneider, Eckhardt & Yorke (2007) for a short periodic pipe Itano & Toh (2000) for channel fmow.

IF n=1 : Timestepping + Bisectjon between ICs.

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Laminar stable point Chaotjc aturactor within ‘edge’ Turbulence

Duguet, W. & Kerswell 2008,10 JFM long pipe, localised coherent structures within laminar-turbulent boundary

Chaos within edge much milder than turbulence → good candidates for Newton search IF n>1 : Timestepping + Bisectjon between ICs.

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Discovery of many (spatially periodic) TWs solutions for pipe flow

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Pufg-like invariant solutjons Avila, Mellibovsky, Rolland & Hof 2013 Exact localised periodic orbits found in m=2 + mirror space Chantry, Willis & Kerswell 2014 Exact localised periodic orbits connected to periodic TWs via spatjal subharmonic bifurcatjon.

localised solutjon

periodic solutjons

L=2π /α

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‘Edge tracking’: Avila, Mellibovsky, Rolland & Hof 2013 Exact localised solution found in m=2 + mirror space 100s of simulations!

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TWs disconnected from laminar state. How to find them? A Re Re = const. Re A Re(t) = Re0 + ĸ.(A0 – A(t))

(Willis, Duguet, Omel’Chenko & Wolfrum, 2017, JFM)

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Pipe simulation: L = 2π /1.25 R, m = 2, no S&R etc. IC Re(t) = Re0 + ĸ.(A0 – A(t))

increasing

ĸ

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Re(t) = Re0 + ĸ.(A0 – A(t))

increasing

ĸ

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TW in ‘controlled’ and ‘uncontrolled’ system

  • const. ĸ
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unstable UPO stabilized RPO

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‘Method’:

  • 1. Find a ‘suitable’ amplitude measure A
  • 2. Link control parameter to A(t), e.g. Re(t) = Re0 + к (A0 – A(t))
  • 3. Increase slowly к = к(t) → reductjon in A(t)
  • 4. Fix к if hit a stable point / orbit!

(Willis, Duguet, Omel’Chenko & Wolfrum, 2017, JFM)

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Key points:

  • TWs (and POs) are weakly unstable solutjons of the N-S equatjons
  • Some are found in the laminar-turbulent boundary → transitjon
  • With hindsight, we could have found them yonks ago!

(Willis, Duguet, Omel’Chenko & Wolfrum, 2017, JFM)

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Recurrent cycles (periodic orbits, POs) in turbulence

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yellow, 2 = -0.3 blue, uz = -0.1

Need to go into moving frame...

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Which phase speed !?

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‘Slicing’

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‘Slicing’

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Fourier ‘Slicing’

(Dynamics of TW just goes around circle)

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Slice vs Poincaré sectjon

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Recurrence plot (sliced dynamics)

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Sliced pipe

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Recurrence plot ‘Compensatory’ norm. ‘Crap’ norm ?

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Recurrence plot DMD/Koopman analysis ? Page & Kerswell (arXiv:1906.01310) Machine learning ? Page & Kerswell CSC methods ? Marensi & Willis

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Summary

  • Jacobian-free Newton-Krylov (- Hookstep): workhorse for dynamical

systems approach. arxiv:1908.06730

  • Relatjve equilibria (TWs) and relatjve periodic orbits (RPOs) embedded in

laminar-turbulent boundary.

  • Gettjng intjtal guesses for JFNK main issue.
  • Bisectjon / ‘Surfjng’ edge.
  • ‘Slicing’ (symmetry reductjon)
  • RPOs embedded in turbulence → proxy for turbulence
  • Norm problem.