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1 Bifurcations in a swirling flow* Thèse de doctorat présentée pour obtenir le grade de Docteur de lÉcole Polytechnique par Elena Vyazmina * Bifurcations.

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Presentation on theme: "1 Bifurcations in a swirling flow* Thèse de doctorat présentée pour obtenir le grade de Docteur de lÉcole Polytechnique par Elena Vyazmina * Bifurcations."— Presentation transcript:

1 1 Bifurcations in a swirling flow* Thèse de doctorat présentée pour obtenir le grade de Docteur de lÉcole Polytechnique par Elena Vyazmina * Bifurcations dun écoulement tournant 13 juillet 2010 Directeurs de thèse: Jean-Marc Chomaz et Peter Schmid

2 2 Swirling flow Introduction Swirling flow Vortex breakdown Applications Classification Problematic Numerical method 2D vortex breakdown 3D vortex breakdown Active open-loop control Summary and perspectives A flow is said to be swirling when its mean direction is aligned with its rotation axis, implying helical particle trajectories.

3 3 Vortex breakdown: definition Main Features: core of vorticity and axial velocity stagnation point reverse flow or recirculation bubble Vortex breakdown is defined as a dramatic change in the structure of the flow core, with the appearance of stagnation points followed by regions of reversed flow referred to as the vortex breakdown bubble. Free jet: Gallaire (2002) Rotating cylinder, fixed lid: S. Harris Introduction Swirling flow Vortex breakdown Applications Classification Problematic Numerical method 2D vortex breakdown 3D vortex breakdown Active open-loop control Summary and perspectives

4 4 Applications Combustion burner Aeronautics Tornado Introduction Swirling flow Vortex breakdown Applications Classification Problematic Numerical method 2D vortex breakdown 3D vortex breakdown Active open-loop control Summary and perspectives

5 5 Vortex breakdown: classification Bubble or axisymmetric form Faler & Leibovich (1977) Spiral form Billant et al. (1998) Cone form Faler & Leibovich (1977) Double helix form Introduction Swirling flow Vortex breakdown Applications Classification Problematic Numerical method 2D vortex breakdown 3D vortex breakdown Active open-loop control Summary and perspectives

6 6 Problematic Pipe Experiments: Sarpkaya (1971), Faler & Leibovich (1978), Leibovich (1978,1983), Althaus (1990), Escudier & Zehnder (1982)… Theoretical and numerical investigations: Squire (1960), Benjamin (1962,1965,1967), Batchelor (1967), Escudier & Keller (1983), Keller et al. (1985), Beran (1989), Beran & Culick (1992), Lopez (1994), Wang & Rusak and coll. (1996, 1997, 1998, 2000, 2001, 2004), Buntine & Saffman (1995), Derzho & Grimshaw (2002), Herrada & Fernandez-Feria (2006)… Introduction Swirling flow Vortex breakdown Applications Classification Problematic Numerical method 2D vortex breakdown 3D vortex breakdown Active open-loop control Summary and perspectives Open flow Experiments: Billant (1998) Numerical investigations: Ruith et al. (2003) – 2D; Ruith et al. (2002, 2003, 2004), Gallaire & Chomaz (2003), Gallaire et al. (2006) – 3D Theoretical investigations: not so many…

7 7 Problematic: open flow, no lateral confinement Governing parameters - the inlet axial velocity; - the azimuthal velocity; - the radius of the vortex core; Boundary condition allowing entrainment! Introduction Swirling flow Vortex breakdown Applications Classification Problematic Numerical method 2D vortex breakdown 3D vortex breakdown Active open-loop control Summary and perspectives

8 8 Overview Introduction Numerical method 2D (axisymmetric) vortex breakdown 3D vortex breakdown Active open-loop control: effect of an external axial pressure gradient on 2D vortex breakdown Summary and perspectives

9 9 Numerical method Introduction Numerical method Flow configuration DNS RPM Arc-length continuation 2D vortex breakdown 3D vortex breakdown Active open-loop control Summary and perspectives Flow configuration Direct numerical simulations (DNS) Recursive projection method (RPM) Arc-length continuation

10 10 Flow configuration The numerical simulations are based on the incompressible time-dependent axisymmetric Navier-Stokes equations in cylindrical coordinates ( x,r, q ) Introduction Numerical method Flow configuration DNS RPM Arc-length continuation 2D vortex breakdown 3D vortex breakdown Active open-loop control Summary and perspectives

11 Flow configuration Grabowski profile (matches experiments of Mager (1972)) Grabowski & Berger (1976) uniform flow

12 Flow configuration: open lateral boundary Boersma et al. (1998) Ruith et al. (2003) Traction-free

13 Flow configuration: open outlet boundary Convective outlet conditions(steady state) Ruith et al. (2003)

14 14 Direct Numerical Simulation (DNS) Code adapted from the code developed by Nichols, Nichols et al. (2007) Mesh: clustered around centreline in radial direction Hanifi et al. (1996) Discretization: sixth-order compact-difference scheme in space Timestepping method: fourth-order Runge-Kutta scheme in time computation of the predicted velocity computation of pressure from the Poisson equation correction of the new velocity Introduction Numerical method Flow configuration DNS RPM Arc-length continuation 2D vortex breakdown 3D vortex breakdown Active open-loop control Summary and perspectives

15 Recursive Projection Method (RPM) Steady solutions with b.c.can be found by the iterative procedure: u n+1 =F(u n ), where F(u n ) is the Runge-Kutta integrator over one time-step The dominant eigenvalue of the Jacobian determines the asymptotic rate of the convergence of the fixed point iteration RPM: method implemented around existing DNS alternative to Newton! Identifies the low-dimensional unstable subspace of a few slow eigenvalues Stabilizes (and speeds-up) convergence of DNS even onto unstable steady-states. Efficient bifurcation analysis by computing only the few eigenvalues of the small subspace. Even when the Jacobian matrix is not explicitly available (!)

16 Recursive Projection Method (RPM) Newton iterations Initial state u n DNS u n+1 =F(u n ) Convergence? Subspace P of few slow & unstable eigenmodes Subspace Q = I - P Reconstruct solution: u n+1 = p+q=PN(p,q)+QF Steady state u s Picard iterations no yes n n +1 F(un)F(un) Treats timestepping routine as a black-box DNS evaluates u n+1 =F(u n ) Recursively identifies subspace of slow eigenmodes, P Substitutes pure Picard iteration with Newton method in P Picard iteration in Q = I - P Reconstructs solution u from sum of the projectors P and Q onto subspace P and its orthogonal complement Q, respectively: u = PN(p,q) + QF Shroff et al. (1993)

17 Arc-length continuation Continuation of a branch of steady solution with respect to the parameter l : F(u,l) =0, where in our case We assume that the solution curve u( l) is a multi-valued function of l At l= l c Pseudo – arc length condition Full system Newton iterations RPM procedure: –Picard iteration in Q –Newton in other

18 18 Introduction Numerical method Axisymmetric vortex breakdown Transcritical bifurcation (inviscid) Viscous effect Resolution test 3D vortex breakdown Active open-loop control Summary and perspectives 2D (axisymmetric) vortex breakdown Transcritical bifurcation (inviscid) Viscous effects Resolution test J. Kostas

19 Axisymmetric vortex breakdown: review Pipe flow Non uniqueness of the solution on the parameter Hysteretic behavior Theory of Wang and Rusak for a finite domain Critical swirl Stability of the inviscid solution Viscous effect Beran & Culick (1992) Open flow ?

20 Transcritical bifurcation (inviscid) open flow Base flow : Grabowski inlet profile q 0 (r)=(u x0 (r),u r0 (r),u q 0 (r)) Small disturbance analysis q(x,r)=q 0 (r) + e q 1 (x,r)+…, q 1 (x,r)=(u x1 (x,r),u r0 (x,r),u q 0 (x,r)) of Euler equations equation for the radial velocity u r1 : Analytical solution: separation of variables u r1 (x,r)=sin (p x/2x 0 )F (r) ODE for F = F (r) and W =S 2 Eigen value problem on W W 1 =S the critical swirl. Solution q 1 determined up to a multiplicative constant q 1 = Aq 1 Vyazmina et al. (2009)

21 21 Viscous effects: asymptotics of an open flow Wang & Rusak (1997) showed in a pipe: regular expansion is invalid near W 1 = S 1 2 Vyazmina et al. (2009): non-homogeneous expansion for open flow Introduction Numerical method Axisymmetric vortex breakdown Transcritical bifurcation (inviscid) Viscous effect Resolution test Three-dimensional vortex breakdown Active open-loop control Summary and perspectives W=W 1 + eDW, n=e 2 n, with DW =O(1), n =O(1) q(x,r)=q 0 (r)+ e q 1 (x,r)+ e 2 q 2 (x,r) + … q 1 = Aq 1 e : L u r1 =0 e 2 : L u r2 = s (q 1,q 0 ), Fredholm alternative Amplitude equation: A 2 M 1 +A DW M 2 + n W 1 M 3 =0, with Linearization of Navier-Stokes

22 22 Viscous effect: asymptotics of an open flow A 2 M 1 +A DW M 2 + n W 1 M 3 =0, Introduction Numerical method Axisymmetric vortex breakdown Transcritical bifurcation (inviscid) Viscous effect Resolution test 3D vortex breakdown Active open-loop control Summary and perspectives Obtain solution q 1 = Aq 1

23 Viscous effects: numerical simulations Re=1000

24 Importance of the resolution for high Re Resolution N 1 : N R =127; N x =257 Other resolutions: N 2 =2N 1 ; N 3 =3N 1 ; N 4 =4N 1 Point C: comparison N 1 and N 4 ? Point A: N 1 error 4 % N 2 error 0.7 % N 3 error 0.2 % Point B: N 1 error 2.5 % N 2 error 0.4 % N 3 error 0.1 % Point C: N 1 error 8 % N 2 error 1 % N 3 error 0.2 %

25 Importance of the resolution for high Re: point A Point A: N 1 error 3.8 % N 2 error 0.69 % N 3 error % Point B: N 1 error 2.47 % N 2 error 0.36 % N 3 error 0.07 % Point C: N 1 error 8.1 % N 2 error 0.9 % N 3 error 0.17 %

26 26 Viscous effect, Re=1000: second bifurcation ? Introduction Numerical method Axisymmetric vortex breakdown Transcritical bifurcation (inviscid) Viscous effect Resolution test 3D vortex breakdown Active open-loop control Summary and perspectives

27 27 Introduction Numerical method 2D vortex breakdown Three-dimensional vortex breakdown Mathematical formulation Spiral vortex breakdown Active open-loop control Summary and perspectives Three-dimensional vortex breakdown Mathematical formulation Spiral vortex breakdown Lim & Cui (2005)

28 28 3D vortex breakdown: short review Spiral vortex breakdown has been observed Experimentally: Sarpkaya (1971), Faler & Leibovich (1977), Escudier & Zehnder (1982), Lambourne & Bryer (1967) DNS: Ruith et al. (2002, 2003) Transition to helical breakdown: sufficiently large pocket of absolute instability in the wake of the bubble, giving rise to a self-excited global mode Gallaire et al. (2003, 2006) Introduction Numerical method 2D vortex breakdown Three-dimensional vortex breakdown Mathematical formulation Spiral vortex breakdown Active open-loop control Summary and perspectives

29 29 3D vortex breakdown: mathematical formulation 2D axisymmetric state is stable to axisymmetric perturbations 3D perturbations? Introduction Numerical method 2D vortex breakdown Three-dimensional vortex breakdown Mathematical formulation Spiral vortex breakdown Active open-loop control Summary and perspectives Base flow is axisymmetric and stable to 2D perturbations Since the base flow is independent of time and azimuthal angle, the perturbations are where m – azimuthal wavenumber, w - complex frequency; the growth rate s = Re(-i w ) the frequency n = Re(-i w )

30 Spiral vortex breakdown: non-axisymmetric mode m=-1 S=1.3 growth rate vs Re Re=150, S=1.3, m=-1 Ruith et al. (2003) solved fully nonlinear 3D equations

31 31 Introduction Numerical method 2D vortex breakdown 3D vortex breakdown Active open-loop control Theoretical expectations Numerical results Summary and perspectives Effect of the external pressure gradient Theoretical expectations Numerical results

32 32 An imposed pressure gradient: review for a pipe Batchelor (1967): in a diverging pipe solution families have a fold as the swirl increased. Numerically Buntine & Saffman (1995) showed the existence of bifurcation where two equilibrium solutions exist in a certain range of swirl below this limit level. Asymptotic analysis of Rusak et al. (1997) of inviscid flow due to the pipe convergence or divergence. Converging tube Leclaire (2006) Introduction Numerical method 2D vortex breakdown 3D vortex breakdown Active open-loop control Theoretical expectations Numerical results Summary and perspectives Rusak et al. (1997) Leclaire (2010)

33 33 External axial pressure gradient Introduction Numerical method 2D vortex breakdown 3D vortex breakdown Active open-loop control Theoretical expectations Numerical results Summary and perspectives Idea: An application of the external axial pressure gradient works as the tube convergence help to achieve a viscous columnar solution at at S >S c n 2

34 Pressure gradient: Theoretical expectations Carrying out the similar non-homogeneous asymptotic analysis with two competitive small parameters: n and b using dominant balance ( n=e 2 n, b = e 2 b ) we obtain the amplitude equation in the form A 2 M 1 -A DW M 2 + n W 1 M 3 - b M 4 =0, M 4 did not calculated, since there is not analytical solution for the adjoint problem. Schematic bifurcation surface

35 35 Pressure gradient: bridging the gap Introduction Numerical method 2D vortex breakdown 3D vortex breakdown Active open-loop control Theoretical expectations Numerical results Summary and perspectives Schematic bifurcation surface

36 Pressure gradient: numerical results Re=1000 N1N1 N1N1 N2N2 N2N2 N2N2 N3N3 N3N3 N3N3 N3N3 N3N3 Does the steady solution exist down to b =0? No, in the case Re=1000 Favorable pressure gradient delays vortex breakdown N3N3 N3N3

37 37 Introduction Numerical method 2D vortex breakdown 3D vortex breakdown Active open-loop control Summary and perspectives Summary Perspectives Summary and perspectives

38 Summary 2D: Bifurcation due the viscosity: numerical and theoretical analysis. 3D: 2D stable solution is unstable to 3D perturbations. Spiral vortex breakdown, m = -1. 2D: external negative pressure gradient b can delay or even prevent vortex breakdown; –Bifurcation with respect to S and b is more complex than a double fold

39 39 Perspectives Computations at higher Reynolds numbers to find vortex breakdown-free state at S >S c n 2 Asymptotic analysis with two competitive parameters n and b, determine the adjoint mode numerically Compute 3D global modes of the adjoint Navier-Stokes linearized around the axisymmetric vortex breakdown state. Proceed sensitivity analysis The slow convergence along the vortex breakdown branch Introduction Numerical method 2D vortex breakdown 3D vortex breakdown Active open-loop control Summary and perspectives Summary Perspectives Investigation of the stability of the solution

40 40 Perspectives: Supercritical Hopf bifurcation Introduction Numerical method 2D vortex breakdown 3D vortex breakdown Active open-loop control Summary and perspectives Summary Perspectives

41 Hopf bifurcation and period doublings perspectives Chaotic dynamics ?

42 42 Merci pour votre attention!


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