Quantifiying Coherent Structures in Large Eddy Simulation

Similar documents
Engineering. Spring Department of Fluid Mechanics, Budapest University of Technology and Economics. Large-Eddy Simulation in Mechanical

Chapter 5 Phenomena of laminar-turbulent boundary layer transition (including free shear layers)

Before we consider two canonical turbulent flows we need a general description of turbulence.

Applied Thermal and Fluid Engineering. Energy Engineering (Thermal Engineering Laboratory)

What is Turbulence? Fabian Waleffe. Depts of Mathematics and Engineering Physics University of Wisconsin, Madison

Module 3: Velocity Measurement Lecture 15: Processing velocity vectors. The Lecture Contains: Data Analysis from Velocity Vectors

Turbulence and its modelling. Outline. Department of Fluid Mechanics, Budapest University of Technology and Economics.

Turbulence Modeling I!

Colloquium FLUID DYNAMICS 2013 Institute of Thermomechanics AS CR, v.v.i., Prague, October 23-25, 2013 p.1

58:160 Intermediate Fluid Mechanics Bluff Body Professor Fred Stern Fall 2014

Nonequilibrium Dynamics in Astrophysics and Material Science YITP, Kyoto

Simulation of Flow around a Surface-mounted Square-section Cylinder of Aspect Ratio Four

arxiv: v1 [physics.flu-dyn] 11 Oct 2012

INTRODUCTION OBJECTIVES

RECONSTRUCTION OF TURBULENT FLUCTUATIONS FOR HYBRID RANS/LES SIMULATIONS USING A SYNTHETIC-EDDY METHOD

Numerical Studies of Supersonic Jet Impingement on a Flat Plate

PIV study for the analysis of planar jets in cross-flow at low Reynolds number

Computational Fluid Dynamics Analysis of Jets with Internal Forced Mixers

Velocity Fluctuations in a Particle-Laden Turbulent Flow over a Backward-Facing Step

A dynamic global-coefficient subgrid-scale eddy-viscosity model for large-eddy simulation in complex geometries

SECONDARY MOTION IN TURBULENT FLOWS OVER SUPERHYDROPHOBIC SURFACES

Turbulent Rankine Vortices

Engineering. Spring Department of Fluid Mechanics, Budapest University of Technology and Economics. Large-Eddy Simulation in Mechanical

+ = + t x x x x u. The standard Smagorinsky model has been used in the work to provide the closure for the subgridscale eddy viscosity in (2):

Day 24: Flow around objects

1. Introduction, tensors, kinematics

ON TURBULENCE AND TRANSPORT IN SHALLOW WAKE FLOWS

DIRECT NUMERICAL SIMULATIONS OF HIGH SPEED FLOW OVER CAVITY. Abstract

Table of Contents. Foreword... xiii. Preface... xv

17th International Conference on Harmonisation within Atmospheric Dispersion Modelling for Regulatory Purposes 9-12 May 2016, Budapest, Hungary

NUMERICAL INVESTIGATION OF THE FLOW OVER A GOLF BALL IN THE SUBCRITICAL AND SUPERCRITICAL REGIMES

Basic Concepts: Drag. Education Community

Numerical and Experimental Study on the Effect of Guide Vane Insertion on the Flow Characteristics in a 90º Rectangular Elbow

(U c. t)/b (U t)/b

COURSE ON VEHICLE AERODYNAMICS Prof. Tamás Lajos University of Rome La Sapienza 1999

superdiffusion blocking Lagrangian Coh. Structures ocean currents internal waves and climate Coriolis force leads to barriers to transport (KAM torus)

Introduction to Turbulence AEEM Why study turbulent flows?

2.2 The Turbulent Round Jet

CCC Annual Report. UIUC, August 14, Effect of Double-Ruler EMBr on Transient Mold Flow with LES Modeling and Scaling Laws

arxiv: v1 [physics.flu-dyn] 10 Dec 2018

LES of turbulent shear flow and pressure driven flow on shallow continental shelves.

Boundary-Layer Theory

arxiv:physics/ v1 [physics.flu-dyn] 14 Mar 2000 Wavelet Cross-Correlation Analysis of Turbulent Mixing from Large-Eddy-Simulations

A Detached-Eddy-Simulation study

Concentration and segregation of particles and bubbles by turbulence : a numerical investigation

Turbulent boundary layer

FLOW-NORDITA Spring School on Turbulent Boundary Layers1

WALL PRESSURE FLUCTUATIONS IN A TURBULENT BOUNDARY LAYER AFTER BLOWING OR SUCTION

An evaluation of LES for jet noise prediction

Lagrangian Coherent Structures: applications to living systems. Bradly Alicea

Chuichi Arakawa Graduate School of Interdisciplinary Information Studies, the University of Tokyo. Chuichi Arakawa

Turbulence Instability

Cavitation Inception and Dynamics in Vortical Flows

Figure 1. Schematic of experimental setup.

HISTORY EFFECTS FOR CAMBERED AND SYMMETRIC

An Overview of Impellers, Velocity Profile and Reactor Design

Divergence free synthetic eddy method for embedded LES inflow boundary condition

Generation of initial fields for channel flow investigation

Parabolized Stability Analysis of Jets Issuing from Serrated Nozzles

Periodic planes v i+1 Top wall u i. Inlet. U m y. Jet hole. Figure 2. Schematic of computational domain.

3D hot-wire measurements of a wind turbine wake

PROPERTIES OF THE FLOW AROUND TWO ROTATING CIRCULAR CYLINDERS IN SIDE-BY-SIDE ARRANGEMENT WITH DIFFERENT ROTATION TYPES

An-Najah National University Civil Engineering Department. Fluid Mechanics. Chapter 1. General Introduction

Two-dimensional model problem to explain counter-rotating vortex pair formation in a transverse jet

FINAL REPORT. Office of Naval Research. entitled. Anatol Roshko Theodore Von Karman Professor of Aeronautics

Numerical Simulation of Rotating Turbulent Channel Flow by the Vortex in Cell Method

Curriculum Vitae of Sergio Pirozzoli

Direct numerical simulation (DNS) investigation of turbulent open channel flow of a Herschel Bulkley fluid

PIV STUDY OF LONGITUDINAL VORTICES IN A TURBULENT BOUNDARY LAYER FLOW

Shear Turbulence. Fabian Waleffe. Depts. of Mathematics and Engineering Physics. Wisconsin

Lecture 7. Turbulence

Dynamics of Large Scale Motions in Bubble-Driven Turbulent Flow

Convection in Three-Dimensional Separated and Attached Flow

The near field of coaxial jets: A numerical study

CVS filtering to study turbulent mixing

TURBINE BURNERS: Engine Performance Improvements; Mixing, Ignition, and Flame-Holding in High Acceleration Flows

Secondary vortices in turbulent square duct flow

Uncertainty quantification for RANS simulation of flow over a wavy wall

Anisotropic Formulation of the Velocity Correlation Tensor

Proceedings of the 4th Joint US-European Fluids Engineering Division Summer Meeting ASME-FEDSM2014 August 3-7, 2014, Chicago, Illinois, USA

IMPLEMENTATION OF POD AND DMD METHODS IN APACHE SPARK FRAMEWORK FOR SIMULATION OF UNSTEADY TURBULENT FLOW IN THE MODEL COMBUSTOR

Disruptive shear stress measurements of fibre suspension using ultrasound Doppler techniques

Principles of Convection

CHAPTER 7 SEVERAL FORMS OF THE EQUATIONS OF MOTION

Turbulence - Theory and Modelling GROUP-STUDIES:

Estimation of Turbulent Dissipation Rate Using 2D Data in Channel Flows

On the feasibility of merging LES with RANS for the near-wall region of attached turbulent flows

FEDSM COMPUTATIONAL AEROACOUSTIC ANALYSIS OF OVEREXPANDED SUPERSONIC JET IMPINGEMENT ON A FLAT PLATE WITH/WITHOUT HOLE

Preliminary Study of the Turbulence Structure in Supersonic Boundary Layers using DNS Data

INFLUENCE OF THE BOUNDARY CONDITIONS ON A TEMPERATURE FIELD IN THE TURBULENT FLOW NEAR THE HEATED WALL

Turbulent energy density and its transport equation in scale space

arxiv: v1 [physics.flu-dyn] 15 Jun 2016

Brief Notes on Vortex Identification

MULTIDIMENSIONAL TURBULENCE SPECTRA - STATISTICAL ANALYSIS OF TURBULENT VORTICES

Turbulence Modeling Applied to Flow over a Hydraulic Ball Check Valve

3D Numerical Study on Laminar Forced Convection in V-Baffled Square Channel

DEPARTMENT OF CHEMICAL ENGINEERING University of Engineering & Technology, Lahore. Fluid Mechanics Lab

Feedback control of transient energy growth in subcritical plane Poiseuille flow

TURBULENT BOUNDARY LAYERS: CURRENT RESEARCH AND FUTURE DIRECTIONS

FLUID MECHANICS. Atmosphere, Ocean. Aerodynamics. Energy conversion. Transport of heat/other. Numerous industrial processes

Transcription:

Quantifiying Coherent Structures in Large Eddy Simulation Máté Márton LOHÁSZ László NAGY, Péter TÓTH, István KONDOR Dept. of Fluid Mechanics @ Budapest University of Technology and Economics 1/30

Table of contents The coherent structure concept Q as vortex detection criteria Investigation methods Image processing Ribbed duct Conditional averaging Channel flow Ribbed duct Vortex tracking Axisymetric jet Spinning, merging vortex pair 2/30

Coherent structure concept Coherent structure (CS) concept: Turbulent motion can be decomposed into three parts Reynolds decomposition = Triple decomposition = c b c Average Fluctuation Coherent motion b Turbulent background = c b An important part of the fluctuation can be characterised by the motion of regular fluid structure so called coherent structures 3/30

Vortices are coherent coherent structures The vortices are the coherent (does not change much in space and time) structure in fluid motion Chakraborty2005, Haller2005 gives the mathematical proof Illustration: Coherent Not coherent How to find vortices in 3D flowfields? To select quantities which are related to rotating motion 4/30

Q vortex detection criteria Q criteria: (Hunt1988) Q Regions of Q>Qth>0 with local pressure minima is defined as vortex Only a fraction of the rotating fluids is defined as a vortex Q= 1 1 Aij A ji = ij ji S ij S ji 2 2 Vorticity dominance Q>0 means vorticity dominance Charkaborty2005 showed that beside D>0, Q>0 is needed for coherence 5/30

Q vortex detection criteria Q Q is the source term in the Poisson equation for pressure Pressure equation: Δp= 2ρQ Source term p 0 n Pressure is lower in the centre of the vortex 6/30

What to do with the coherent structures? Traditional technology: Image processing 1) Create movies of the temporal evolution of the vortices with different thresholds, and different viewpoints 2) Find well known features 3) Quantify what you can 4) Compare to possibly existing theory only qualitative results Drawback: 1) Result is user dependent 2) Evolution described in a poetic way e.g. : One sees vortices passing by as a flight of big migratory birds (Lesieur2003) Methods are needed to quantify coherent structure evolution 7/30

Image processing (example) view flow (Lohász2006) 8/30

Distance between the structures above the rib Changes between 0.2 0.3h 9/30

Distance between the structures above the rib 0.3 h 10/30

Distance between the structures above the rib 11/30

Distance between the structures above the rib 0.2 h 12/30

Distance between the structures above the rib 13/30

Distance between the structures above the rib 14/30

Distance between the structures above the rib 15/30

Distance between the structures above the rib 0.3 h 16/30

Distance between the structures above the rib 17/30

Distance between the structures above the rib 18/30

Conditional averaging Indicator function: The classes: Conditional averaged variable: Deviation: (Lohász2005) 19/44

Probability of the classes More background than vortex for both cases Intense vortices are more probable for perpendicular rib 20/44

Location of the intense vortices Leading edge of the rib Shear layer of 90 rib Wake of the 45 rib 21/44

The pressure deviation Volume average of the pressure deviation for each class for the higher than 5% probability regions Size of the higher than 5% probability regions 22/44

Channel flow Reτ=180 Vortex probability LES with Dyn. Smag. 723 cells sec. ord. scheme Q class borders: 0, 0.1, 0.01 Ub2/δ2 - Q<0 is appr. 60%, i.e vortices are rare - Intense vortices have high probability in buffer zone

Channel flow Streamwise velocity Intense vortices (or vortex cores) move slower at the channel center, and faster close to the wall

Channel flow Streamwise velocity fluctuation Q strength inversely prop. to streamwise fluctuation Wall-normal velocity Vortex core tends to the center perimeter to the wall

Vortex tracking Vortices need to be identified separatly The educted region needs to be divided into disjunct sets Needed for the quantitative investigation of the interactions The complete educed region Vortices with indices Example of an axisymmetric jet (Nyers2008) 26/30

Vortex tracking Application example: Position and size of the vortices Pressure contours 27/30

Spinning, merging vortices Spinning vortex pair, different threshold Vortex path Radius of the vortex position 28/30

Correlation between noise and vortices Far field pressure Average vorticity evolution Goal: Prediction of far field sound using vortex position and strength evolution 29/30

Conclusion The combination of the two methods: A tracking based averaging could provide the best understanding of the vortex evolution Thank you for your attention! 30/30