Routes to transition in shear flows · 2004-10-21 · STILL TODAY, TRANSITION IN SHEAR FLOWS IS...

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ROUTES TO TRANSITION IN SHEAR FLOWS ROUTES TO TRANSITION IN SHEAR FLOWS Alessandro Bottaro with contributions from: D. Biau, B. Galletti, I. Gavarini and F.T.M. Nieuwstadt

Transcript of Routes to transition in shear flows · 2004-10-21 · STILL TODAY, TRANSITION IN SHEAR FLOWS IS...

Page 1: Routes to transition in shear flows · 2004-10-21 · STILL TODAY, TRANSITION IN SHEAR FLOWS IS STILL NOT FULLY UNDERSTOOD. For the simplest parallel flows there is poor agreement

ROUTES TO TRANSITION IN SHEAR FLOWS

ROUTES TO TRANSITION IN SHEAR FLOWS

Alessandro Bottaro

with contributions from:D. Biau, B. Galletti, I. Gavarini and F.T.M. Nieuwstadt

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Osborne Reynolds, 1842-1912

“An experimental investigation of the circumstances which determinewhether motion of water shall be direct or sinuous and of the law ofresistance in parallel channels”, Royal Society, Phil. Trans. 1883

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`the colour band would all at once mix up with the surrounding water, and fill the rest of the tube with a mass of coloured water ... On viewing the tube by the light of an electric spark, the mass of colour resolved itself into a mass of more or less distinct curls, showing eddies.'

Retrans ≈ 13000

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Hydrodynamic stability theory followed a few years later:

W. M’F.Orr, ‘The stability or instability of the steady motions of a perfect liquid and of a viscous liquid’, Proc. Roy. Irish Academy, 1907

A. Sommerfeld, ‘Ein Beitrag zur hydrodynamischen Erklaerungder turbulenten Fluessigkeitsbewegungen’, Proc. 4th International Congress of Mathematicians, Rome, 1908

Hints on the solution of the stability equations for the flow in a pipe

arrived only much later (C.L. Pekeris, 1948), just to show that

(!!)Recrit → ∞

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STILL TODAY, TRANSITION IN SHEAR FLOWS IS STILL NOT FULLY UNDERSTOOD. For the simplest parallel flows there is poor agreement between predictions from the classical linear stability theory (Recrit) and experimentals results (Retrans)

Poiseuille Couette Hagen-Poiseuille Square ductRecrit 5772 ∞ ∞ ∞

Retrans ~2000 ~400 ~2000 ~2000

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THE TRANSITION PROCESS

Receptivity phase: the flow filters environmental disturbances

Initial phaseROUTE 1: TRANSIENT GROWTHROUTE 2: EXPONENTIAL GROWTH

Late, nonlinear stages of transition

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SMALL AMPLITUDE DISTURBANCESLinearized Navier-Stokes equations[to make things simple: cartesian coordinates, U=U(y)]

with homogeneous boundary conditions for (u, v, w) at y=±h

Goal: SPATIAL EVOLUTION OF DISTURBANCES

wp1Uww

vp1Uvv

up1'vUUuu

0wvu

zxt

yxt

xxt

zyx

∆ν+ρ

−=+

∆ν+ρ

−=+

∆ν+ρ

−=++

=++

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ROUTE 1: TRANSIENT GROWTH

ROUTE 1: TRANSIENT GROWTH

THE MECHANISM: a stationary algebraic instability exists in the inviscid system (“lift-up” effect). In the viscous case the growth of the disturbance energy is hampered by diffusion ⇒ transient growth

P.H. Alfredsson and M. Matsubara (1996); streaky structures in a boundarylayer. Free-stream speed: 2 [m/s], free-stream turbulence level: 6%

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INVISCID ANALYSIS: the physics suggests to employ different length and velocity scales along different directions (introducing a parameter ε << 1)

so that the steady inviscid equations to leading order are:

x → h/ε y, z → h

U, u → Umax v, w → ε Umax

p → ρ (ε Umax)2

ROUTE 1: TRANSIENT GROWTH

zx

yx

x

zyx

pUw

pUv

0'vUUu

0wvu

−=

−=

=+

=++

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Look for similarity solutions of the form:

By substituting into the equations it is easy to find thatλ = 1 is a solution, so that:

_

.c.ce)y(px)z,y,x(p

.c.ce)y(wx)z,y,x(w

.c.ce)y(vx)z,y,x(v

.c.ce)y(ux)z,y,x(u

zi2

zi1

zi1

zi

+=

+=

+=

+=

β−λ

β−λ

β−λ

βλ

zi0y0

zi0

zi0

eU

'Uvvi)z,y,x(w

e)y(v)z,y,x(v

e)y(vU

'Ux)z,y,x(u

β

β

β

β=

=

−= ALGEBRAIC GROWTH

ROUTE 1: TRANSIENT GROWTH

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ROUTE 1: TRANSIENT GROWTH

VISCOUS ANALYSIS

maxUh

ε

• Classical approach: use ( )

as scales and find the Orr-Sommerfeld/Squire

system, with and

• Two-scale approach: use ( ) as time scale

and find a reduced Os/Squire system

2max

maxmax U,

Uh,h,U ρ

ν=

hURe max

( )[ ]( ) v'UReU

0v''UReU

z1

xt

x1

xt

∂−=η∆−∂+∂

=∂−∆∆−∂+∂−

wu xz ∂−∂=η

( )[ ]( ) v'UU

0v''UU

z2xt

x22xt

∂−=η∆−∂+∂=∂−∆∆−∂+∂

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ROUTE 1: TRANSIENT GROWTH

[ ] [ ] .c.ce)y(ˆ,v,v )tzx(i )p()p( +η=η ω−β+α β,Normal modes: ℜ∈ω,

Poiseuille flow: eigenmodes full system vs parabolic model

Re = 2000, ω = 0, β = 1.91 Re = 2000, ω = 0.3, β = 1.91

Parabolic: αp = α Re, ωp = ω Re Full: α, ω

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ROUTE 1: TRANSIENT GROWTH

“Optimal” disturbances: most dangerous initial conditions at x = 0, i.e. those that maximize the output disturbance energy

dzdy)wwvvuu(

dzdywwvvuu

)0(E)x(E)x(G

000S 000

xS

++

++==

∫∫∫∫

In boundary layer scalings it is obvious that, sinceu = ❡ (Umax) and (v,w) = ❡ (Umax/Re), G is rendered maximum when u0 = 0. Then:

∫∫∫∫

+≈

S 0000

S x2

dzdy)wwvv(dzdyuu

ReG

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ROUTE 1: TRANSIENT GROWTH

Decompose the generic disturbance vector q as a sum of normal modes:

Then:

)tzx(inn

nnne)y(ˆ)t,z,y,x( ω−β+α= qq κ

mnmn

mnmn21

1mmnmnn

1

1mm

xixinn

2

B)x(A

Redy]wwvv[

dyueuRe)x(G

mn

κκκκ

κκ

κκ=

+≈

α+α−

Rayleigh quotient. The largest gain at each x is the

largest eigenvalue solution of2Reλ

mnm2mnm BReλ)x(A κκ =

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ROUTE 1: TRANSIENT GROWTH

Optimal growth, Re = 1000, ω = 0, β = 1.91 (Poiseuille flow)Re = 500, ω = 0, β = 1.58 (Couette flow)

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ROUTE 1: TRANSIENT GROWTH

Iso-G, Poiseuille flow, Re = 2000

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ROUTE 1: TRANSIENT GROWTH

Optimal growth, Poiseuille flow, Re = 2000 & 5000, ω = 0, β = 1.91

Viscous

Inviscid

Viscous

Analytical

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ROUTE 1: TRANSIENT GROWTH

Optimal symmetric disturbance and optimal streak at xopt,Poiseuille flow, Re = 2000, ω = 0, β = 1.91

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ROUTE 1: TRANSIENT GROWTH

Optimal antisymmetric disturbance and optimal streak at xopt,Poiseuille flow, Re = 2000

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ROUTE 1: TRANSIENT GROWTH

The accuracy of the parabolic system degrades with ω

Percentage error, , Poiseuille flow, Re = 2000elliptparab GG −

elliptG

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ROUTE 1: TRANSIENT GROWTH

Optimal disturbances, spatial results ...

… vs corresponding temporal results

t

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ROUTE 1: TRANSIENT GROWTH

Square duct, exit result, no optimization

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ROUTE 1: TRANSIENT GROWTH

Square duct

Optimal inlet flow Outlet streaks

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ROUTE 1: TRANSIENT GROWTH

Square duct

E

x/Re

x2

Eu

Evw

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ROUTE 1: TRANSIENT GROWTH

Optimal perturbations

Gmax/Re2 xopt/Re

Poiseuille 2.41*10-4 0.057 βopt = 1.91

Couette 3.39*10-4 0.073 βopt = 1.58

Pipe 1.03*10-4 0.033 mopt = 1

Square duct 1.12*10-4 0.039

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ROUTE 2: EXPONENTIAL GROWTH

ROUTE 2: EXPONENTIAL GROWTH

Preliminary observation: eigenvalues of the OS/Squire system are very sensitive to operator perturbations E

{ }ε≤+Λ∈α∈α=Λε EthatsuchEwith),EL(:C)L(

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ROUTE 2: EXPONENTIAL GROWTH

Consider a very particular operator perturbation, a distortion of the mean flow U(y) (induced by whatever environmental forcing) →

OS equation: L (U, α; ω, β, Re) v = 0

With a base flow variation δU(y):

δL v + L δv = 0

0vLvLvULU =δ+

α∂∂

δα+∂∂

δ

{ }ε≤δδ+Λ∈α∈α=Λδ Uwith)],UU(L[:C)L( refU

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ROUTE 2: EXPONENTIAL GROWTH

Projecting on a, eigenfunction of the adjoint system (L*a=0) we find

and hence,

In practice, for each eigenvalue αn we can tie the base flow variation δU to the ensuing variation δα via a sensitivity function GU

0vLavLavULUa =δ⋅+

α∂∂

⋅δα+∂∂

δ⋅

∫−

δ==

α∂∂⋅

∂∂δ⋅

−=δα1

1U dyUG...

vLa

vULUa

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ROUTE 2: EXPONENTIAL GROWTH

HAGEN-POISEUILLE FLOW

Spectrum of eigenvalues at Re = 3000, m = 1, ω = 0.5. The circle includes the two most receptive eigenvalues

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ROUTE 2: EXPONENTIAL GROWTH

drUGr U

1

0δ=δα ∫

Corresponding ∞ norm of rGu. Modes arranged in order of increasing |αi|

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ROUTE 2: EXPONENTIAL GROWTH

SENSITIVITY FUNCTIONS

Mode 22 (solid); mode 24 (dashed);103*mode 1 (dash-dotted)

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ROUTE 2: EXPONENTIAL GROWTH

“Optimization”

Look for optimal base flow distortion of given norm ε, so that the growth rate of the instability (-αi) is maximized:

Necessary condition is that:

ε−−γ+α=α ∫

1

1

2refii dy)UU(Min)(Min

0dyU)UU(21

1refi =

δ−γ+δα ∫

Page 33: Routes to transition in shear flows · 2004-10-21 · STILL TODAY, TRANSITION IN SHEAR FLOWS IS STILL NOT FULLY UNDERSTOOD. For the simplest parallel flows there is poor agreement

ROUTE 2: EXPONENTIAL GROWTH

Employing the previous result:

A simple gradient algorithm can be used to find the new base flow that maximizes the growth rate, for any αn and for any given base flow distortion norm ε:

with

[ ] 0dyU)UU(2)GIm(1

1refU =δ−γ+∫

[ ] 21

1

1

2)i(U

)i(

4

)GIm(

ε=γ

∫−µ

[ ])UU(2)GIm(UU ref)i()i()i(

U)i()1i( −γ+ϑ+=+

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ROUTE 2: EXPONENTIAL GROWTH

Re = 3000, m = 1, ω = 0.5. HP flow (circles), OD flow (triangles) with ε = 2.5*10-5 which minimizes αi of mode 22.

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ROUTE 2: EXPONENTIAL GROWTH

U

Optimally distorted base flow vs Hagen-Poiseuille flow.The curve of (U’/r)’/20 indicates an inflectional instability

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ROUTE 2: EXPONENTIAL GROWTH

Re=3000

Re=2300Re=1800

Re=1760

Growth rate as function of ω for m = 1 and ε = 10-5

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ROUTE 2: EXPONENTIAL GROWTH

ε=5*10-5

ε=10-5ε=5*10-6

ε=2*10-6

Neutral curves for m = 1 and ε = 10-5. Symbols give Recrit

Page 38: Routes to transition in shear flows · 2004-10-21 · STILL TODAY, TRANSITION IN SHEAR FLOWS IS STILL NOT FULLY UNDERSTOOD. For the simplest parallel flows there is poor agreement

FULL NONLINEAR SIMULATIONS

Page 39: Routes to transition in shear flows · 2004-10-21 · STILL TODAY, TRANSITION IN SHEAR FLOWS IS STILL NOT FULLY UNDERSTOOD. For the simplest parallel flows there is poor agreement

dtrdrdeˆT21)x(E

2T 2

0

1

0

)tkj(i

mj nk

)n,m(dis ϑ= ∫ ∫ ∫∑ ∑

τ

πω−ϑ

±= ±=u

Spatial evolution of the disturbance energy for the Fourier modes(m, n), with ω = 0.5. Initial amplitude of the (1,1) eigenmode (shown with thick blue line) is 0.002. Re = 3000, m = 1, n = 1, ε = 2.5*10-5.

Page 40: Routes to transition in shear flows · 2004-10-21 · STILL TODAY, TRANSITION IN SHEAR FLOWS IS STILL NOT FULLY UNDERSTOOD. For the simplest parallel flows there is poor agreement

CONCLUSIONS

Transient growth in space can be described by a parabolic systemTransient growth is related to the non-normality of OS-Squire eigenmodes (L. N. Trefethen et al., 1993)OS eigenmodes are very sensitive to base flow variations (δU-pseudospectrum, the growth is less than for the ε-pseudospectrum since two-way (possibly unphysical?) coupling between OS and Squire equations is not allowed)

Page 41: Routes to transition in shear flows · 2004-10-21 · STILL TODAY, TRANSITION IN SHEAR FLOWS IS STILL NOT FULLY UNDERSTOOD. For the simplest parallel flows there is poor agreement

CONCLUSIONS

Exponential growth can take place even in nominally subcritical conditions for mild distortions of the base flow

Poiseuille flow, Re = 3000, ω = 0.5 Optimal distortion

Page 42: Routes to transition in shear flows · 2004-10-21 · STILL TODAY, TRANSITION IN SHEAR FLOWS IS STILL NOT FULLY UNDERSTOOD. For the simplest parallel flows there is poor agreement

CONCLUSIONS

Transition is likely to be provoked by the combined effect of algebraic and exponentially growing disturbances, the ultimate fate of the flow being decided by the prevailing receptivity conditions of the flow

Page 43: Routes to transition in shear flows · 2004-10-21 · STILL TODAY, TRANSITION IN SHEAR FLOWS IS STILL NOT FULLY UNDERSTOOD. For the simplest parallel flows there is poor agreement

x

R1θ