60th Annual Meeting Division of Fluid Dynamics A multiscale approach to study the stability of long waves in near-parallel flows S. Scarsoglio #, D.Tordella.

Slides:



Advertisements
Similar presentations
Potential Flow Theory : Incompressible Flow
Advertisements

LARGE-EDDY SIMULATION and LAGRANGIAN TRACKING of a DIFFUSER PRECEDED BY A TURBULENT PIPE Sep 07, 2006 Fabio Sbrizzai a, Roberto Verzicco b and Alfredo.
1 Linné Flow Centre KTH Mechanics 7th European Fluid Mechanics Conference, Manchester, September, Dan Henningson collaborators Shervin Bagheri,
Space & Atmosphere Research Center University of Sheffield Róbert Erdélyi and Michael Ruderman SPARC, Department of Applied Mathematics, University of.
Results It was found that variations in wettability disturb the flow of adjacent liquid (Fig. 3). Our results suggest that for a given liquid the normal.
Modeling Generation and Nonlinear Evolution of Plasma Turbulence for Radiation Belt Remediation Center for Space Science & Engineering Research Virginia.
Quantification of Laminar flow weakness … P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Instability Analysis of Laminar Flows.
Chapter 2 Reynolds Transport Theorem (RTT) 2.1 The Reynolds Transport Theorem 2.2 Continuity Equation 2.3 The Linear Momentum Equation 2.4 Conservation.
1 Linné Flow Centre KTH Mechanics ERCOFTAC SIG 33 Workshop, Santa Margherita Ligure, October 16-18, 2008 Dan Henningson collaborators Shervin Bagheri,
Modelling Flow Distributed Oscillations In The CDIMA Reaction Jonathan R Bamforth, Serafim Kalliadasis, John H Merkin, Stephen K Scott School of Chemistry,
23-28 September 2003 Basic Processes in Turbulent Plasmas Forecasting asymptotic states of a Galerkin approximation of 2D MHD equations Forecasting asymptotic.
Dissipation of Alfvén Waves in Coronal Structures Coronal Heating Problem T corona ~10 6 K M.F. De Franceschis, F. Malara, P. Veltri Dipartimento di Fisica.
6/29/20151 Stability of Parallel Flows. 6/29/20152 Analysis by LINEAR STABILITY ANALYSIS. l Transitions as Re increases 0 < Re < 47: Steady 2D wake Re.
Neeraj Jain1, Surja Sharma2
Analysis of Physical Intuition … P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Two-dimensional Boundary Layer Flows.
An Ultimate Combination of Physical Intuition with Experiments… P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Boundary Layer.
Lectures 11-12: Gravity waves Linear equations Plane waves on deep water Waves at an interface Waves on shallower water.
Intermittent Transport and Relaxation Oscillations of Nonlinear Reduced Models for Fusion Plasmas S. Hamaguchi, 1 K. Takeda, 2 A. Bierwage, 2 S. Tsurimaki,
Large-amplitude oscillations in a Townsend discharge in low- current limit Vladimir Khudik, Alex Shvydky (Plasma Dynamics Corp., MI) Abstract We have developed.
The sliding Couette flow problem T. Ichikawa and M. Nagata Department of Aeronautics and Astronautics Graduate School of Engineering Kyoto University The.
Contact Line Instability in Driven Films
Numerical Simulation on Flow Generated Resistive Wall Mode Shaoyan Cui (1,2), Xiaogang Wang (1), Yue Liu (1), Bo Yu (2) 1.State Key Laboratory of Materials.
VISCOUS MEANS FLOWS IN NEARLY INVISCID FARADAY WAVES Elena Martín Universidad de Vigo, Spain - Drift instabilities of spatially uniform Faraday waves.
Recent advances in wave kinetics
Unione Industriale Torino
TOWER SHADOW MODELIZATION WITH HELICOIDAL VORTEX METHOD Jean-Jacques Chattot University of California Davis OUTLINE Motivations Review of Vortex Model.
Computing Internal and External Flows Undergoing Instability and Bifurcations V. V. S. N. Vijay, Neelu Singh and T. K. Sengupta High Performance Computing.
59th Annual Meeting Division of Fluid Dynamics Initial-value problem for the two-dimensional growing wake S. Scarsoglio #, D.Tordella # and W. O. Criminale*
Properties of Filter (Transfer Function) Real part of a Transfer Function for different order periodic filters.
Electron behaviour in three-dimensional collisionless magnetic reconnection A. Perona 1, D. Borgogno 2, D. Grasso 2,3 1 CFSA, Department of Physics, University.
Numerical simulations of thermal counterflow in the presence of solid boundaries Andrew Baggaley Jason Laurie Weizmann Institute Sylvain Laizet Imperial.
HELICOIDAL VORTEX MODEL FOR WIND TURBINE AEROELASTIC SIMULATION Jean-Jacques Chattot University of California Davis OUTLINE Challenges in Wind Turbine.
Rotating D’Arcy Convection Manel Naspreda Martí Departament de Física Fonamental Universitat de Barcelona Group of Statistical Physics Revisor: Michael.
22 nd IFIP TC 7 Conference on System Modeling and Optimization Analysis of the convective instability of the two- dimensional wake D.Tordella #, S.Scarsoglio.
M. Onofri, F. Malara, P. Veltri Compressible magnetohydrodynamics simulations of the RFP with anisotropic thermal conductivity Dipartimento di Fisica,
12th European Turbulence Conference Linear generation of multiple time scales by three-dimensional unstable perturbations S. Scarsoglio #, D.Tordella #
The Stability of Laminar Flows - 2
Numerical study of flow instability between two cylinders in 2D case V. V. Denisenko Institute for Aided Design RAS.
Challenges in Wind Turbine Flows
On the nature of bend instability Stefano Lanzoni University of Padua, Italy Bianca Federici and Giovanni Seminara University of Genua, Italy.
Requirements of High Accuracy Computing 1) Adopted numerical scheme must resolve all physical time and length scales. 2) Numerical scheme must be neutrally.
Chernoshtanov I.S., Tsidulko Yu.A.
Chapter 3. Instability of the free plane and near – wall plane jet
The Stability of Laminar Flows
1 Espen Åkervik 7 th ERCOFTAC SIG33 WORKSHOP Low dimensional model for control of the Blasius boundary layer by balanced truncation Espen Åkervik in collaboration.
The Rayleigh-Taylor Instability By: Paul Canepa and Mike Cromer Team Leftovers.
Multimedia files -3/13 Instability of plane parallel flows Contents: 1.Canonical basic velocity profiles 2.Critical Reynolds numbers for the canonical.
Transition to Tubulence in the Hartmann Layer A. Thess 1, D.Krasnov 1, E. Zienicke 1, O. Zikanov 2, T. Boeck 3 1-Ilmenau University of Technology 2-University.
11th European Turbulence Conference Temporal dynamics of small perturbations for a two-dimensional growing wake S. Scarsoglio #, D.Tordella # and W. O.
P. Meunier Institut de Recherche sur les Phénomènes Hors-Equilibre, Marseille, France Collaborators: X. Riedinger, N. Boulanger, S. Le Dizès, P. Billant.
An experimental study of bypass transition in plane Couette flow S. AMALFI, F. LAADHARI & J. F. SCOTT Laboratoire de Mécanique des Fluides et d’Acoustique.
Arthur Straube PATTERNS IN CHAOTICALLY MIXING FLUID FLOWS Department of Physics, University of Potsdam, Germany COLLABORATION: A. Pikovsky, M. Abel URL:
Spatial Evolution of Resonant Harmonic Mode Triads in a Blasius Boundary Layer 37th AIAA Fluid Dynamics Conference and Exhibit José B. Dávila Department.
Combined Local and Global Stability Analyses (work in progress) Matthew Juniper, Ubaid Qadri, Dhiren Mistry, Benoît Pier, Outi Tammisola, Fredrik Lundell.
Turbulent Fluid Flow daVinci [1510].
A new feature of nonlinear processes in smooth shear flows: Angular redistribution of Nonlinear perturbations G. D. Chagelishvili M. Nodia institute of.
Date of download: 7/7/2016 Copyright © ASME. All rights reserved. From: Modal Stability TheoryLecture notes from the FLOW-NORDITA Summer School on Advanced.
Date of download: 9/27/2017 Copyright © ASME. All rights reserved.
Identifying the “wavemaker” of fluid/structure instabilities
WHAT CONTROLS BAR MIGRATION IN TIDAL CHANNELS?
A rotating hairy BH in AdS_3
An Analytical Model for A Wind Turbine Wake
Unione Industriale Torino
Stability of subcritical electrohydrodynamics in dielectric fluids
Absolute and convective instability of the two-dimensional wake
CPHT-Ecole polytechnique
Stability and Dynamics in Fabry-Perot cavities due to combined photothermal and radiation-pressure effects Francesco Marino1,4, Maurizio De Rosa2, Francesco.
Karl Schindler, Bochum, Germany
Experimental and Numerical Investigation of Controlled, Small-Scale Motions in a Turbulent Shear Layer Bojan Vukasinovic, Ari Glezer Woodruff School of.
Critical Timing without a Timer for Embryonic Development
Presentation transcript:

60th Annual Meeting Division of Fluid Dynamics A multiscale approach to study the stability of long waves in near-parallel flows S. Scarsoglio #, D.Tordella # and W. O. Criminale* # Dipartimento di Ingegneria Aeronautica e Spaziale, Politecnico di Torino, Torino, Italy * Department of Applied Mathematics, University of Washington, Seattle, Washington, Usa EFMC7, Manchester, September 14-18, 2008

Outline  Physical problem  Initial-value problem  Multiscale analysis for the stability of long waves  Conclusions

 Flow behind a circular cylinder steady, incompressible and viscous;  Approximation of 2D asymptotic Navier-Stokes expansions (Belan & Tordella, 2003), 20 ≤ Re ≤ 100. Physical Problem

Initial-value problem  Linear, three-dimensional perturbative equations in terms of vorticity and velocity (Criminale & Drazin, 1990);  Base flow parametric in x and Re U(y; x 0, Re)  Laplace-Fourier transform in x and z directions for perturbation quantities:

α r = k cos( Φ ) wavenumber in x-direction γ = k sin( Φ ) wavenumber in z-direction Φ = tan -1 ( γ / α r ) angle of obliquity k = ( α r 2 + γ 2 ) 1/2 polar wavenumber α i 0 spatial damping rate

 Periodic initial conditions for  Velocity field vanishing in the free stream. symmetric asymmetric and

 The growth function G is the normalized kinetic energy density and measures the growth of the perturbation energy at time t. Early transient and asymptotic behaviour of perturbations  The temporal growth rate r (Lasseigne et al., 1999) and the angular frequency ω (Whitham, 1974) perturbation phase

(a): R=100, y 0 =0, x 0 =6.50, α i =0.01, n 0 =1, asymmetric, Φ =3/8 π, k=0.5,1,1.5,2,2.5. (b): R=50, y 0 =0, x 0 =7, k=0.5, Φ =0, asymmetric, n 0 =1, α i = 0,0.01,0.05,0.1. Exploratory analysis of the transient dynamics (c): Wave spatial evolution in the x direction for k= α r =0.5, α i = 0,0.01,0.05,0.1.

(d): R=100, y 0 =0, x 0 =11.50, k=0.7, asymmetric, α i =0.02, n 0 =1, Φ =0, π /2. (e): R=100 x 0 =12, k=1.2, α i =0.01, symmetric, n 0 =1, Φ = π /2, y 0 =0,2,4,6. (f): R=50 x 0 =14, k=0.9, α i =0.15, asymmetric, y 0 =0, Φ = π /2, n 0 =1,3,5,7.

(a)-(b)-(c)-(d): R=100, y 0 =0, k=0.6, α i =0.02, n 0 =1, Φ = π /4, x 0 =11 and 50, symmetric and asymmetric. ……..

(a): R=100, y 0 =0, x 0 =9, k=1.7, α i =0.05, n 0 =1, symmetric, Φ = π /8. >>

(a)-(b): Re=50, α i =0.05, Ф =0, x 0 =11, n 0 =1, y 0 =0. Initial-value problem (triangles: symmetric, circles: asymmetric), normal mode analysis (black curves), experimental data (Williamson 1989, red symbols). Asymptotic fate and comparison with modal analysis  Asymptotic state: the temporal growth rate r asymptotes to a constant value (dr/dt < ε ~ ).

Multiscale analysis for the stability of long waves  Different scales in the stability analysis:  Slow scales (base flow evolution);  Fast scales (disturbance dynamics); Small parameter is the polar wavenumber of the perturbation: k<<1  In some flow configurations, long waves can be destabilizing (for example Blasius boundary layer and 3D cross flow boundary layer);  In such instances the perturbation wavenumber of the unstable wave is much less than O(1).

Full linear system base flow (U(x,y:Re), V(x,y;Re))  Regular perturbation scheme, k<<1:  Temporal scales:  Spatial scales: Multiple scales hypothesis

Order O(1) Order O(k)

(a)-(b): Re=100, k=0.01, Ф = π /4, x 0 =10, n 0 =1, y 0 =0. Full linear problem (black circles: symmetric, black triangles: asymmetric), multiscale O(1) (red circles: symmetric, red triangles: asymmetric). Comparison with the full linear problem

(a): R=50, y 0 =0, k=0.03, n 0 =1, x 0 =12, Φ = π /4, asymmetric, α i =0.04, 0.4. (b): R=100, y 0 =0, n 0 =1, x 0 =27, Φ =0, symmetric, α i =0.2, k=0.1, 0.01, (c): R=100, y 0 =0, k=0.02, x 0 =13.50, n 0 =1, Φ = π /2, α i =0.08, sym and asym. -> <-

(a)-(b): R=50, y 0 =0, k=0.04, n 0 =1, x 0 =12, Φ = π /2, asymmetric, α i =0.005, 0.01, 0.05 (multiscale O(1)), α i =0 (full problem).

Conclusions  Synthetic perturbation hypothesis (saddle point sequence);  Absolute instability pockets (Re=50,100) found in the intermediate wake;  Good agreement, in terms of frequency, with numerical and experimental data;  No information on the early time history of the perturbation;  Different transient growths of energy;  Asymptotic good agreement with modal analysis and with experimental data (in terms of frequency and wavelength);  Multiscaling O(1) for long waves well approximates full linear problem.

where and