Hydrodynamics. Class 11. Laurette TUCKERMAN

Similar documents
Course: Nonlinear Dynamics. Laurette TUCKERMAN Maps, Period Doubling and Floquet Theory

Nonlinear Dynamics. Laurette TUCKERMAN Maps, Period Doubling and Floquet Theory

Laurette TUCKERMAN Rayleigh-Bénard Convection and Lorenz Model

Chapter 5. The Differential Forms of the Fundamental Laws

2 The incompressible Kelvin-Helmholtz instability

Kelvin Helmholtz Instability

9 Fluid Instabilities

Can weakly nonlinear theory explain Faraday wave patterns near onset?

Math 211. Substitute Lecture. November 20, 2000

Sound Waves Sound Waves:

General introduction to Hydrodynamic Instabilities

PAPER 331 HYDRODYNAMIC STABILITY

CHAPTER 5. RUDIMENTS OF HYDRODYNAMIC INSTABILITY

Lecture 7. Please note. Additional tutorial. Please note that there is no lecture on Tuesday, 15 November 2011.

On the displacement of two immiscible Stokes fluids in a 3D Hele-Shaw cell

Quasipatterns in surface wave experiments

6 Linear Equation. 6.1 Equation with constant coefficients

1. Comparison of stability analysis to previous work

Modelling Rayleigh Taylor instability of a sedimenting suspension of several thousand circular particles in a direct numerical simulation

Three-dimensional Floquet stability analysis of the wake in cylinder arrays

A Model of Evolutionary Dynamics with Quasiperiodic Forcing

Stability of flow past a confined cylinder

Poincaré Map, Floquet Theory, and Stability of Periodic Orbits

Second Order Systems

The Whitham Equation. John D. Carter April 2, Based upon work supported by the NSF under grant DMS

Math Ordinary Differential Equations

Investigation of the effect of external periodic flow. pulsation on a cylinder wake using linear stability. analysis

03. Simple Dynamical Systems

6 Parametric oscillator

3 2 6 Solve the initial value problem u ( t) 3. a- If A has eigenvalues λ =, λ = 1 and corresponding eigenvectors 1

Euler equation and Navier-Stokes equation

Relativistic Electrodynamics

is conserved, calculating E both at θ = 0 and θ = π/2 we find that this happens for a value ω = ω given by: 2g

Chapter 1 Fluid Characteristics

Theoretical considerations on ultrasound assisted atomization of fluid sheets

MAE210C: Fluid Mechanics III Spring Quarter sgls/mae210c 2013/ Solution II

Stability of Shear Flow

Journal of Applied Nonlinear Dynamics

CH.3. COMPATIBILITY EQUATIONS. Multimedia Course on Continuum Mechanics

V (r,t) = i ˆ u( x, y,z,t) + ˆ j v( x, y,z,t) + k ˆ w( x, y, z,t)

g(t) = f(x 1 (t),..., x n (t)).

1 POTENTIAL FLOW THEORY Formulation of the seakeeping problem

Linear Hydrodynamic Stability Analysis Summary and Review. Example of Stability Problems. Start with Base Velocity Profile

Consider a particle in 1D at position x(t), subject to a force F (x), so that mẍ = F (x). Define the kinetic energy to be.

If the symmetry axes of a uniform symmetric body coincide with the coordinate axes, the products of inertia (Ixy etc.

Stability of the splay state in pulse-coupled networks

Magnetohydrodynamics Stability of a Compressible Fluid Layer Below a Vacuum Medium

Numerics and Control of PDEs Lecture 1. IFCAM IISc Bangalore

Solutions for homework 5

Available online at ScienceDirect. Procedia IUTAM 14 (2015 ) IUTAM ABCM Symposium on Laminar Turbulent Transition

Irrotational Faraday Waves on a Viscous Fluid

Available online at ScienceDirect. Procedia IUTAM 19 (2016 ) IUTAM Symposium Analytical Methods in Nonlinear Dynamics

Plateau-Rayleigh Instability of a Cylinder of Viscous Liquid (Rayleigh vs. Chandrasekhar) L. Pekker FujiFilm Dimatix Inc., Lebanon NH USA

approach to Laplacian Growth Problems in 2-D

10.52 Mechanics of Fluids Spring 2006 Problem Set 3

PEAT SEISMOLOGY Lecture 2: Continuum mechanics

Introduction to Fluid Dynamics

Vortex wake and energy transitions of an oscillating cylinder at low Reynolds number

Prof. Krstic Nonlinear Systems MAE281A Homework set 1 Linearization & phase portrait

Wave and Elasticity Equations

Observation of Star-Shaped Surface Gravity Waves

Array Research: A Research Example

Putzer s Algorithm. Norman Lebovitz. September 8, 2016

Governing Equations of Fluid Dynamics

(Nearly) Scale invariant fluid dynamics for the dilute Fermi gas in two and three dimensions. Thomas Schaefer North Carolina State University

To link to this article : DOI: /S URL :

Numerical Simulation of the Hagemann Entrainment Experiments

INHOMOGENEOUS LINEAR SYSTEMS OF DIFFERENTIAL EQUATIONS

Faraday Instability on Elastic Interfaces

6.6 Rayleigh-Darcy (or Horton-Rogers-Lapwood) instability

Time-periodic forcing of Turing patterns in the Brusselator model

Scale invariant fluid dynamics for the dilute Fermi gas at unitarity

Numerical simulation of Faraday waves

Stability, cyclone-anticyclone asymmetry and frequency selection in rotating shallow-water wakes

Dynamics of Structures: Theory and Analysis

C. Show your answer in part B agrees with your answer in part A in the limit that the constant c 0.

Dynamics of Strongly Nonlinear Internal Solitary Waves in Shallow Water

Capillary-gravity waves: The effect of viscosity on the wave resistance

Mathematics for Engineers II. lectures. Differential Equations

Axisymmetric Hopf bifurcation in a free surface rotating cylinder flow

Hydrodynamic Forces on Floating Bodies

The Shallow Water Equations

Vortex structures in the wake of a buoyant tethered cylinder at moderate to high reduced velocities

1+t 2 (l) y = 2xy 3 (m) x = 2tx + 1 (n) x = 2tx + t (o) y = 1 + y (p) y = ty (q) y =

Laurette TUCKERMAN Numerical Methods for Differential Equations in Physics

Lecture 4: Numerical solution of ordinary differential equations

Review of Fundamental Equations Supplementary notes on Section 1.2 and 1.3

Chapter 9: Differential Analysis

Transient Phenomena in Quantum Bound States Subjected to a Sudden Perturbation

Thursday, August 4, 2011

Exercise 5: Exact Solutions to the Navier-Stokes Equations I

Notes 4: Differential Form of the Conservation Equations

(Super) Fluid Dynamics. Thomas Schaefer, North Carolina State University

PUTNAM PROBLEMS DIFFERENTIAL EQUATIONS. First Order Equations. p(x)dx)) = q(x) exp(

- Marine Hydrodynamics. Lecture 4. Knowns Equations # Unknowns # (conservation of mass) (conservation of momentum)

Waves in Linear Optical Media

ARTICLE IN PRESS. Available online at Mathematics and Computers in Simulation xxx (2011) xxx xxx

Chapter 9: Differential Analysis of Fluid Flow

Contents. I Introduction 1. Preface. xiii

Math 54. Selected Solutions for Week 10

Transcription:

Hydrodynamics Class 11 Laurette TUCKERMAN laurette@pmmh.espci.fr

Faraday instability Faraday (1831): Vertical vibration of fluid layer = stripes, squares, hexagons

In 1990s: first fluid-dynamical quasicrystals: Edwards & Fauve Kudrolli, Pier & Gollub J. Fluid Mech. (1994) Physica D (1998)

Effect of horizontal motion ζ(x+u t,t+ t) = ζ(x,t) ζ(x,t)+ ζ ζ t+ u t = ζ(x,t) t x ζ t = ζ x u Effect of vertical motion ζ(x,t+ t) = ζ(x,t)+w t ζ(x,t)+ ζ t = ζ(x,t)+w t t ζ t = w Combined effect foru = φ: ζ t +u ζ x +v ζ y = w ζ t + φ ζ x x + φ ζ y y = φ z

Surface Tension Tangential force along surface= normal force if slope varies. ζ xx < 0 = F z < 0 to be counterbalanced by p > p 0 : p 0 p = σ 2 ζ x 2 Bernouilli equation (ideal fluid) satisfied at surface: φ dt + 1 2 φ 2 = p 0 p gζ ρ becomes: φ dt + 1 2 φ 2 = σ 2 ζ ρ x gζ 2

Bernouilli s equation at interface: t φ+ 1 2 φ 2 = σ ρ ( 2 x + 2 y)ζ Φ Oscillating frame of reference= oscillating gravity G(t) = g acos(ωt) Gravitational potential energy at interface: Bernouilli s equation at interface: [ t φ+ 12 φ 2 ] Φ = G(t)z = G(t)ζ (x,y,z=ζ(x,y)) Interface z = ζ(x, y, t) moves according to: = t ζ +u ζ = w [ ] σ ρ ( 2 x + y)ζ 2 G(t)ζ (x,y) Incompressibility: u = φ = 0

Base state: For small perturbations: u = 0 ζ = 0 t ζ (x,y) + u ζ = z φ (x,y,z=0+ ζ(x,y)) [ ] 1 t φ+ 2 φ 2 = (x,y,z=0+ ζ(x,y)) [ σ ρ ( 2 x + 2 y)ζ G(t)ζ Consider domain to be horizontally infinite (homogeneous) = solutions exponential/trigonometric in x = (x,y) Seek bounded solutions= trigonometric: exp(ik x) = exp(i(k x x+k y y)) ] (x,y) Height ζ(x,y,t) = k e ik xˆζk (t) Velocity φ(x,y,z,t) = k e ik xˆφk (z,t) 0 = φ = ( 2 z k 2 )ˆφ k = ˆφ k e ±kz Assume infinite depth(z ) = ˆφ k = e kzˆφk (t)

Drop hats and subscriptk t ζ = z φ z=0 = kφ z=0 = φ z=0 = t ζ/k t φ z=0 = σ ρ ( 2 x + 2 y)ζ G(t)ζ t t ζ/k = σ ρ ( k2 )ζ G(t)ζ tζ 2 = k 3σ ζ k(g acos(ωt))ζ ρ Defineω 2 0 = σ ρ k3 +gk â = ak ω 2 0 2 tζ = ω 2 0(1 âcos(ωt))ζ a = 0 = Gravity-capillary waves = ζ e ±iω 0t a 0 = Linear equation forζ whose coefficients are periodic

Floquet theory Linear equations with constant coefficients: aẍ+bẋ+cx = 0 = x(t) = α 1 e λ1t +α 2 e λ 2t where aλ 2 +bλ+c = 0 ẋ = cx = x(t) = e ct x(0) N N c n x (n) = 0 = x(t) = α n e λ nt n=0 where n=1 N c n λ n = 0 Generalize to linear equations with periodic coefficients: a(t)ẍ+b(t)ẋ+c(t)x = 0 = x(t) = α 1 (t)e λ1t +α 2 (t)e λ 2t a(t),b(t),c(t) have period T = α 1 (t),α 2 (t) have period T n=0

Floquet theory continued a(t)ẍ+b(t)ẋ+c(t)x = 0 = x(t) = α 1 (t)e λ1t +α 2 (t)e λ 2t α 1 (t),α 2 (t) Floquet functions λ 1,λ 2 Floquet exponents growing solution if Real(λ j ) > 0 µ 1 e λ1t,µ 2 e λ 2T Floquet multipliers growing solution if µ j > 1 λ 1, λ 2 not roots of polynomial = calculate numerically or asymptotically ẋ = c(t)x = x(t) = e λt α(t) N N c n (t)x (n) = 0 = x(t) = e λnt α n (t) n=0 n=1

for exponent λ Region of stability for multipliere λt Imaginary part non-unique = choose Im(λ) ( πi/t, πi/t] = ( iω/2, iω/2]

2 tζ = ω 2 0(1 acos(ωt))ζ Temporal Floquet problem, witht = 2π/ω ζ(t) = c 1 e λ 1t f 1 (t mod T)+c 2 e λ 2t f 2 (t mod T) Two Floquet exponentsλ j and Floquet functions f j (t) for each k Real(λ) 0 for some j, k = flat surface unstable = Faraday waves with spatial wavenumberk and temporal frequency Im(λ) Im(λ) e λt waves period 0 1 harmonic T = 2π/ω (same as forcing) ω/2 1 subharmonic 2T = 4π/ω (twice forcing period)

Instability Tongues

Floquet functions λ (ζ-< ζ >)/ 0.003 0.002 0.001 0 0 1 t / T 2 3-0.001-0.002-0.003 λ (ζ-< ζ >)/ 0.006 0.004 0.002 0 1 2 3 0 t / T -0.002 (ζ-< ζ >)/ 0.03 0.02 0.01 0 0 1 t / T 2 3-0.01-0.02 within tongue 1 /2 within tongue 2 /2 within tongue 3 /2 subharmonic harmonic subharmonic µ = 1 µ = +1 µ = 1 λ -0.03

Inclusion of viscosity ρ t u = p+µ u u = 0 ê z ρ t u = ê z p+ê z µ u Assuming v = 0, then ρ t w = µ 2 w τ ij = pδ ij +µ( xj U i + xi U j ) As before, for linear stability analysis, evaluate atz = 0 using flat interface with normal in z direction. Continuity of tangential stress = 0 = τ xz = µ( x w + z u) 0 = τ yz = µ( y w + z v) 0 = x τ xz + y τ yz = µ( 2 xw + 2 yw + xz u+ yz v) = µ( 2 x + 2 y 2 z)w Normal stress is not zero at interface: counterbalanced by surface tension σ( 2 x + 2 z)ζ = τ zz = (p ρg(t)ζ)+2µ z w z=0

Instability tongues for viscous fluids Thresholds are finite instead of zero. Tongues are rounded Minima of tongues rise with frequency (1/2, 2/2, 3/2,... tongues)

Square patterns in Faraday instability

Hexagonal patterns in Faraday instability

Ideal flow Cylinder wake with downstream recirculation zone Von Kármán vortex street (Re 46) Laboratory experiment (Taneda, 1982) Off Chilean coast past Juan Fernandez islands

Stability analysis of von Kármán vortex street 2D limit cycleu 2D (x,y,tmod T) obeys: Add 3D perturbation t U 2D = (U 2D )U 2D P 2D + 1 Re U 2D t ( U 2D +u 3D ) = (U 2D (t) )u 2D (U 2D (t) )u 3D (u 3D )U 2D (t) (u 3D )u 3D ( P 2D +p 3D )+ 1 Re ( U 2D +u 3D ) Subtract 2D equation from 3D equation and neglect quadratic terms to obtain equation governing perturbation u 3D : t u 3D = (U 2D (t) )u 3D (u 3D )U 2D (t) p 3D + 1 Re u 3D Linear equation which is homogeneous in z and periodic in t

von Kárman vortex street: Re = U d/ν 46 spatially: two-dimensional (x,y) (homogeneous in z) temporally: periodic,st = fd/u appears spontaneously U 2D (x,y,t mod T)

Infinitesimal perturbation u 3D obeys linear equation: t u 3D = (U 2D (t) )u 3D (u 3D )U 2D (t) p 3D + 1 Re u 3D Equation is linear and homogeneous in z. Seek solutions which are bounded in z, hence periodic u 3D (x,y,z,t) e iβz with coefficients which are periodic in t with period T : Floquet form u 3D (x,y,z,t) e λt f(t mod T) Therefore u 3D (x,y,z,t) e iβz e λ βt f β (x,y,t mod T) Fix β, calculateλ β and µ β e λ βt. Real part ofλ β > 0 µ β > 1 (For each β value, there are actually many eigenvalues λ β. Selectλ β with largest real part.)

From Barkley & Henderson, J. Fluid Mech. (1996) mode A:Re c = 188.5 β c = 1.585 = 2π/β c 4 mode B:Re c = 259 β c = 7.64 = 2π/β c 1

mode A atre = 210 mode B atre = 250 From M.C. Thompson, Monash University, Australia (http://mec-mail.eng.monash.edu.au/ mct/mct/docs/cylinder.html)