RaNS.1 RaNS + PDE Turbulence Closure Models

Size: px
Start display at page:

Download "RaNS.1 RaNS + PDE Turbulence Closure Models"

Transcription

1 RaNS.1 RaNS + PDE Turbulence Closure Models Time-averaged Navier-Sokes PDE closure models one-equaion: k wih l specified υ, Re ranspor wo-equaion: k, ε ranspor k,ω ranspor Turbulen kineic energy ranspor D : ( ) = k k U k 1 1 E L k + U i υ +ε+ uuu + p u 0 j x ij x x x i i j ρ = j j j j j υ ui ui dissipaion : ε δ 3/ / l jk 3 xj x k k - 1 i Re sress : δ + U U k υ S, S = ij ij ij ij + 3 xj xi 1 1 υ k closure model: uuu i i j+ pu j - ρ σ x k j j

2 RaNS. RaNS + Single Turbulence Closure Models Prandl one-equaion model selecs ε 3/ l assumed proporional o mixing lengh Baldwin-Barh Re ranspor PDE Spalar-Allmaras υ ranspor PDE = C k / l D eddy viscosiy: υ C υre DD (le Re R) μ 1 ( ) υr υr ( υr) 1/ 1 υ ( υr) ranspor: L ( υr) = + U υ+ υ σ C( RP) 0 j ε υ + = x x σ x x j j ε k k closure: 7 coeffeciens + 3 funcions ( Wilcox, pg.110 ) eddy viscosiy : υ = υf υ 1 υ υ 1 υ υ υ ranspor : L ( υ) = + U ( υ υ) C C υs C 0 j + + = x σ x x 1 x 3 d j k k k closure : 8 coeffeciens + 3 funcions (Wilcox, pg.111)

3 RaNS.3 RaNS + Two PDE Turbulence Closure Models Fundamenal variables for RaNS+ PDE closure models Kolmogorov: ω dissipaion rae, D ( -1) υ k/ ω, l k 1/ / ω, ε kω Chou: υ k/ ε, l k 3/ / ε Roa : υ k/ l, ε k3/ / l Kolmogorov, Speziale, W ilcox, Peng k-ω closure L ( k) = k k U i k + U + β kω ( υ+ σ υ ) = 0 j x ij x x x j j j j L ω ω ω U i ω j j j closure: υ = k/ ω, consans α, β, β, σ, σ, β= β f, β = β f ( ) = ω + U α ( ) 0 j ij + β ω υ + συ = x k x x x j β 0 β 1, χ k χ ΩΩ ij jk S f ω ki,,, 0, ω -3 k χ f ω = = χ χ β ω β + χ > k k k 1+80χ ω ( β 0 ω) x j x j χ k 1 1 definiions: ε = β kω, Ω Ui, j U j, i, S U ij ij i, j + U j, i

4 RaNS.4 RaNS + Two PDE Turbulence Closure Models Jones & Launder, Launder & Sharma k-ε closure L( k) and L( ε) wih momens modelled already covered u exac ( ) i L ε υ ( L ( u )) = 0 x x i j j eqn.(4.45) in Wilcox Yakho and Orzag renormalizaion group (RNG) model L ( k ) and L ( ε) remain in " sandard " form C λ 3 (1 λ / λ0 ) μ k C C +, λ S S ε ε 1 3 ji ij + βλ ε all model consans slighly alered Two PDE closure model coefficien deerminaion compaibiliy wih BL similariy resoluion, decaying homogeneous isoropic urbulence

5 RaNS.5 Similariy Soluions for RaNS + PDE Closures Uni-direcional flow primiive PDEs and similariy soluion forms

6 RaNS.6 Similariy Soluions for RaNS +PDE Closures Insering self-similar forms ino DP x (u), η y/x u 1 d j du D P ( η): L ( U) V - η N = S U x u η ηdη dη where : N( η) ransformed eddy viscosiy erm V ( η) ransverse momenum erm S ( ) sreamwise convecion erm u η Similariy form for k-ω and k-ε closure models

7 RaNS.7 Similariy Soluions for RaNS +PDE Closures Similariy closure parameers / funcions Key disincion beween k-ω and k-ε closure models is χ ω χ = f ( Ω Ω S ) Ω Ω S + Ω Ω S for -D flows ω ij jk ki U 1 U 0 U 1 U 1 U 0 x y x r 0 0 ry, 1 U V 1 U V D: S = 0 Axi: S = 0 Boh: Ω = 1 U ij ij y y 0 0 ij r r ry, V r χ ω 1 U U V 1 U U V 1 U V - + =0 χ - + ω 4 y x y 4 r x r 4 y r

8 RaNS.8 RaNS + PDE Farfield Similariy Soluions Numerical similariy soluions for farfield urbulen flows wake mixing layer

9 RaNS.9 RaNS + PDE Farfield Similariy Soluions Numerical similariy soluions for farfield urbulen flows plane je round je

10 RaNS.10 RaNS +k-ω Soluion for Turbulen Channel Flow Perurbaion mached-region soluions, k-ω model k ω closure Re = 13,750 H o DNS (Mansour) P + U = υ / u 4 xy y ε + = υε/ u4

11 RaNS.11 RaNS + PDE Closure Model Near Wall BCs PDE closure models mus address nearfield low Re region BCs recall BL similariy U+ u/ u = κ -1log( y+ E) + C y+ u y/ υ producion = dissipaion in L ( k) υ -1 = κ ε = (κ ) -1 = / μ ω = (κ ) yu y u k u C y u 3 Modificaions for pressure gradien, surface roughness dp P+ υ ρu 3 dx 5 C 8.5 in log law

12 RaNS.1 RaNS + PDE Closure Model Low Re Effecs TS applied o DM + DP x for flucuaing velociies near surface u fx( x,z,) y + O( y ) 3 v fy( x,z,) y + O( y ) as y 0 w fz( x,z,) y + O( y ) Limiing behavior for ime-averaged properies 1 k ( f + f ) y + O( y3), ε υ ( f + f ) y+ O( y), ( f f ) y3+ O( y4) x z x z xy x y Implemenaed by modificaions o PDE closure models for BLs ε = ε +ε 0 υ f k μ μ = C / ε

13 RaNS.13 RaNS +PDE Low Re Closure Modificaions Correlaion Re numbers : Re T = k /ε, R y = k 1/ y/ν, y + = u y/ν

14 RaNS.14 RaNS + PDE Low Re Closure Modificaions Examining low Re model asympoic behavior for k-ε as y 0: k y ε/ k υ / y y 3, y 4 for Lam-Bremhors xy BCs a y =0: k =0 = ε k 1/ k ε=ε +ε, ε= f, 0 0 y y k ε= υ y for Lam-Bremhors ε = 0 y ransiion o k-ω: ε= C kω = β0kω μ k + = k / u

15 RaNS.15 RaNS + Low Re k-ω Closure Model Low Re k - ω closure model idenical excep for α * υ = α k / ω T 0 α 1 Closure model consans now funcions of urbulen Re s β = 9 f β /15, σ = 1/ = σ σ =β /3, α = 1/9 R = 8 β R = 6 k R =.95 ω

16 RaNS.16 RaNS + k-ω Low Re Soluion for Channel Flow k ωlow Re closure Re = 13,750 H o DNS (Mansour) P + U = υ / xy u y ε = υε/ u + 4 4

17 RaNS.17 Summary: RaNS + PDE Turbulence Closure Time-averaged incompressible NS + PDE closure models single PDE : Prandl mixing lengh wih L ( k) Baldwin-Barh: L (Re ) closure consans, funcions Spalar-Allmaras: L ( υ ) dual PDE : Kolmogrov,...: L ( k), L (ω), υ = k /ω Jones Launder,...: L( k), L( ε ), υ = C k / ε Yakho,...,RNG: C ε modified for Uni-direcional farfield flows, similariy soluion characerizaion μ S ij L ω(, Ω ) admis vorex rollup for -D axisymmeric flow S ij ij improved agreemen for all farfield cases accepable agreemen for channel flow Uni-direcional nearfield flows, low Re modificaions low Re models address wall damping asympoically L ( S ) ij ω(,α ) provides necessary modificaions for k-ω improved agreemen for k, P, ε nearwall disribuions

Diffusion & Viscosity: Navier-Stokes Equation

Diffusion & Viscosity: Navier-Stokes Equation 4/5/018 Diffusion & Viscosiy: Navier-Sokes Equaion 1 4/5/018 Diffusion Equaion Imagine a quaniy C(x,) represening a local propery in a fluid, eg. - hermal energy densiy - concenraion of a polluan - densiy

More information

NUMERICAL SIMULATION OF A LIQUID SODIUM TURBULENT FLOW OVER A BACKWARD FACING STEP WITH A FOUR PARAMETER LOGARITHMIC TURBULENCE MODEL

NUMERICAL SIMULATION OF A LIQUID SODIUM TURBULENT FLOW OVER A BACKWARD FACING STEP WITH A FOUR PARAMETER LOGARITHMIC TURBULENCE MODEL h European Conference on Compuaional Mechanics (ECCM ) 7h European Conference on Compuaional Fluid Dynamics (ECFD 7) 11 June, Glasgow, UK NUMERICAL SIMULATION OF A LIQUID SODIUM TURBULENT FLOW OVER A BACKWARD

More information

ASSESSMENT OF BUOYANCY-CORRECTED TURBULENCE MODELS FOR THERMAL PLUMES

ASSESSMENT OF BUOYANCY-CORRECTED TURBULENCE MODELS FOR THERMAL PLUMES Engineering Applicaions of Compuaional Fluid Mechanics Vol. 7, No., pp. 9 49 (1) ASSESSMENT OF BUOYANCY-CORRECTED TURBULENCE MODELS FOR THERMAL PLUMES Raesh Kumar and Anupam Dewan * * Deparmen of Applied

More information

Turbulent Flows. Computational Modelling of Turbulent Flows. Overview. Turbulent Eddies and Scales

Turbulent Flows. Computational Modelling of Turbulent Flows. Overview. Turbulent Eddies and Scales School of Mechanical Aerospace and Civil Engineering Turbulen Flows As noed above, using he mehods described in earlier lecures, he Navier-Sokes equaions can be discreized and solved numerically on complex

More information

Verification of a CFD benchmark solution of transient low Mach number flows with Richardson extrapolation procedure 1

Verification of a CFD benchmark solution of transient low Mach number flows with Richardson extrapolation procedure 1 Verificaion of a CFD benchmark soluion of ransien low Mach number flows wih Richardson exrapolaion procedure S. Beneboula, S. Gounand, A. Beccanini and E. Suder DEN/DANS/DMS/STMF Commissaria à l Energie

More information

Heat Transfer. Revision Examples

Heat Transfer. Revision Examples Hea Transfer Revision Examples Hea ransfer: energy ranspor because of a emperaure difference. Thermal energy is ransferred from one region o anoher. Hea ranspor is he same phenomena lie mass ransfer, momenum

More information

Computer Fluid Dynamics E181107

Computer Fluid Dynamics E181107 Compuer Fluid Dynamics E181107 2181106 Turbulen flows, Remark: foils wih black background could be skipped, hey are aimed o he more advanced courses Rudolf Žiný, Úsav procesní a zpracovaelské echniky ČVUT

More information

Program: RFEM 5, RSTAB 8, RF-DYNAM Pro, DYNAM Pro. Category: Isotropic Linear Elasticity, Dynamics, Member

Program: RFEM 5, RSTAB 8, RF-DYNAM Pro, DYNAM Pro. Category: Isotropic Linear Elasticity, Dynamics, Member Verificaion Example Program: RFEM 5, RSTAB 8, RF-DYNAM Pro, DYNAM Pro Caegory: Isoropic Linear Elasiciy, Dynamics, Member Verificaion Example: 0104 Canilever Beam wih Periodic Exciaion 0104 Canilever Beam

More information

Vanishing Viscosity Method. There are another instructive and perhaps more natural discontinuous solutions of the conservation law

Vanishing Viscosity Method. There are another instructive and perhaps more natural discontinuous solutions of the conservation law Vanishing Viscosiy Mehod. There are anoher insrucive and perhaps more naural disconinuous soluions of he conservaion law (1 u +(q(u x 0, he so called vanishing viscosiy mehod. This mehod consiss in viewing

More information

Area A 0 level is h 0, assuming the pipe flow to be laminar. D, L and assuming the pipe flow to be highly turbulent.

Area A 0 level is h 0, assuming the pipe flow to be laminar. D, L and assuming the pipe flow to be highly turbulent. Pipe Flows (ecures 5 o 7). Choose he crec answer (i) While deriving an expression f loss of head due o a sudden expansion in a pipe, in addiion o he coninuiy and impulse-momenum equaions, one of he following

More information

THE EFFECT OF SUCTION AND INJECTION ON UNSTEADY COUETTE FLOW WITH VARIABLE PROPERTIES

THE EFFECT OF SUCTION AND INJECTION ON UNSTEADY COUETTE FLOW WITH VARIABLE PROPERTIES Kragujevac J. Sci. 3 () 7-4. UDC 53.5:536. 4 THE EFFECT OF SUCTION AND INJECTION ON UNSTEADY COUETTE FLOW WITH VARIABLE PROPERTIES Hazem A. Aia Dep. of Mahemaics, College of Science,King Saud Universiy

More information

where the coordinate X (t) describes the system motion. X has its origin at the system static equilibrium position (SEP).

where the coordinate X (t) describes the system motion. X has its origin at the system static equilibrium position (SEP). Appendix A: Conservaion of Mechanical Energy = Conservaion of Linear Momenum Consider he moion of a nd order mechanical sysem comprised of he fundamenal mechanical elemens: ineria or mass (M), siffness

More information

ME 391 Mechanical Engineering Analysis

ME 391 Mechanical Engineering Analysis Fall 04 ME 39 Mechanical Engineering Analsis Eam # Soluions Direcions: Open noes (including course web posings). No books, compuers, or phones. An calculaor is fair game. Problem Deermine he posiion of

More information

2 int T. is the Fourier transform of f(t) which is the inverse Fourier transform of f. i t e

2 int T. is the Fourier transform of f(t) which is the inverse Fourier transform of f. i t e PHYS67 Class 3 ourier Transforms In he limi T, he ourier series becomes an inegral ( nt f in T ce f n f f e d, has been replaced by ) where i f e d is he ourier ransform of f() which is he inverse ourier

More information

Introduction to Physical Oceanography Homework 5 - Solutions

Introduction to Physical Oceanography Homework 5 - Solutions Laure Zanna //5 Inroducion o Phsical Oceanograph Homework 5 - Soluions. Inerial oscillaions wih boom fricion non-selecive scale: The governing equaions for his problem are This ssem can be wrien as where

More information

Unsteady Mass- Transfer Models

Unsteady Mass- Transfer Models See T&K Chaper 9 Unseady Mass- Transfer Models ChEn 6603 Wednesday, April 4, Ouline Conex for he discussion Soluion for ransien binary diffusion wih consan c, N. Soluion for mulicomponen diffusion wih

More information

Theory of! Partial Differential Equations-I!

Theory of! Partial Differential Equations-I! hp://users.wpi.edu/~grear/me61.hml! Ouline! Theory o! Parial Dierenial Equaions-I! Gréar Tryggvason! Spring 010! Basic Properies o PDE!! Quasi-linear Firs Order Equaions! - Characerisics! - Linear and

More information

t 2 B F x,t n dsdt t u x,t dxdt

t 2 B F x,t n dsdt t u x,t dxdt Evoluion Equaions For 0, fixed, le U U0, where U denoes a bounded open se in R n.suppose ha U is filled wih a maerial in which a conaminan is being ranspored by various means including diffusion and convecion.

More information

Navneet Saini, Mayank Goyal, Vishal Bansal (2013); Term Project AML310; Indian Institute of Technology Delhi

Navneet Saini, Mayank Goyal, Vishal Bansal (2013); Term Project AML310; Indian Institute of Technology Delhi Creep in Viscoelasic Subsances Numerical mehods o calculae he coefficiens of he Prony equaion using creep es daa and Herediary Inegrals Mehod Navnee Saini, Mayank Goyal, Vishal Bansal (23); Term Projec

More information

Cosmic String Loop Distribution with a Gravitational Wave Cutoff

Cosmic String Loop Distribution with a Gravitational Wave Cutoff Ouline Inroducion Towards he Cosmological Aracor Cosmic Sring Loop Disribuion wih a Graviaional Wave Cuoff Larissa Lorenz Insiue of Mahemaics and Physics Cenre for Cosmology, Paricle Physics and Phenomenology

More information

IMPLEMENTATION OF AN ALGEBRAIC BYPASS TRANSITION MODEL INTO TWO-EQUATION TURBULENCE MODEL FOR A FINITE VOLUME METHOD SOLVER

IMPLEMENTATION OF AN ALGEBRAIC BYPASS TRANSITION MODEL INTO TWO-EQUATION TURBULENCE MODEL FOR A FINITE VOLUME METHOD SOLVER Colloquium FLUID DYNAMICS 2007 Insiue of Thermomechanics AS CR, v. v. i., Prague, Ocober 24-26, 2007 p.1 IMPLEMENTATION OF AN ALGEBRAIC BYPASS TRANSITION MODEL INTO TWO-EQUATION TURBULENCE MODEL FOR A

More information

APPLICATION OF SCALE ADAPTIVE SIMULATION BASED ON K-Ω SST TURBULENCE MODEL

APPLICATION OF SCALE ADAPTIVE SIMULATION BASED ON K-Ω SST TURBULENCE MODEL APPLICATION OF SCALE ADAPTIVE SIMULATION BASED ON K-Ω SST TURBULENCE MODEL XiangYu Wang, Dong Li Naional Key Laboraory of Science and Technology on Aerodynamic Design and Research, Norhwesern Polyechnical

More information

Excel-Based Solution Method For The Optimal Policy Of The Hadley And Whittin s Exact Model With Arma Demand

Excel-Based Solution Method For The Optimal Policy Of The Hadley And Whittin s Exact Model With Arma Demand Excel-Based Soluion Mehod For The Opimal Policy Of The Hadley And Whiin s Exac Model Wih Arma Demand Kal Nami School of Business and Economics Winson Salem Sae Universiy Winson Salem, NC 27110 Phone: (336)750-2338

More information

Thermal Modeling of a Honeycomb Reformer including Radiative Heat Transfer

Thermal Modeling of a Honeycomb Reformer including Radiative Heat Transfer Thermal Modeling of a Honeycomb Reformer including Radiaive Hea Transfer J Schöne *1, A Körnig 1, W Becer 1 and A Michaelis 1 1 Fraunhofer IKTS, Winerbergsraße 8, 0177 Dresden *Corresponding auhor: jaobschoene@isfraunhoferde

More information

Physics 235 Chapter 2. Chapter 2 Newtonian Mechanics Single Particle

Physics 235 Chapter 2. Chapter 2 Newtonian Mechanics Single Particle Chaper 2 Newonian Mechanics Single Paricle In his Chaper we will review wha Newon s laws of mechanics ell us abou he moion of a single paricle. Newon s laws are only valid in suiable reference frames,

More information

LES at high Re numbers: a near-wall eddy-viscosity formulation

LES at high Re numbers: a near-wall eddy-viscosity formulation a high Re numbers: a near-wall eddy-viscosiy formulaion Georgi Kalizin, Jeremy A. Templeon & Gorazd Medic Mechanical ngineering Deparmen, Sanford Universiy, Sanford, CA 943, USA Absrac A near-wall eddy-viscosiy

More information

Chapter 15: Phenomena. Chapter 15 Chemical Kinetics. Reaction Rates. Reaction Rates R P. Reaction Rates. Rate Laws

Chapter 15: Phenomena. Chapter 15 Chemical Kinetics. Reaction Rates. Reaction Rates R P. Reaction Rates. Rate Laws Chaper 5: Phenomena Phenomena: The reacion (aq) + B(aq) C(aq) was sudied a wo differen emperaures (98 K and 35 K). For each emperaure he reacion was sared by puing differen concenraions of he 3 species

More information

Comparison of Heat Transfer between a Circular and Rectangular Tube Heat Exchanger by using Ansys Fluent

Comparison of Heat Transfer between a Circular and Rectangular Tube Heat Exchanger by using Ansys Fluent Research Aricle Inernaional Journal Thermal Technologies E-ISSN 77 4114 14 INPRESSCO, All Righs Reserved Available a hp://pressco.com/caegory/ij/ Comparison Hea Transfer beween a Circular and Recangular

More information

1 Solutions to selected problems

1 Solutions to selected problems 1 Soluions o seleced problems 1. Le A B R n. Show ha in A in B bu in general bd A bd B. Soluion. Le x in A. Then here is ɛ > 0 such ha B ɛ (x) A B. This shows x in B. If A = [0, 1] and B = [0, 2], hen

More information

N. Sandeep 1 and V. Sugunamma 2

N. Sandeep 1 and V. Sugunamma 2 Journal of Applied Fluid Mechanics, Vol. 7, No., pp. 75-86, 4. Available online a www.jafmonline.ne, ISSN 735-357, EISSN 735-3645. Radiaion and Inclined Magneic Field Effecs on Unseady Hydromagneic Free

More information

Theory of! Partial Differential Equations!

Theory of! Partial Differential Equations! hp://www.nd.edu/~gryggva/cfd-course/! Ouline! Theory o! Parial Dierenial Equaions! Gréar Tryggvason! Spring 011! Basic Properies o PDE!! Quasi-linear Firs Order Equaions! - Characerisics! - Linear and

More information

TOP-QUARK MASS MEASUREMENTS AT THE LHC

TOP-QUARK MASS MEASUREMENTS AT THE LHC TOP-QUARK MASS MEASUREMENTS AT THE LHC S. Blyweer, on behalf of he ATLAS and CMS Collaboraions Vrije Universiei Brussel - Ineruniversiy Insiue for High Energies Pleinlaan 2, 1050 Brussel, Belgium The op-quark

More information

And the solution to the PDE problem must be of the form Π 1

And the solution to the PDE problem must be of the form Π 1 5. Self-Similar Soluions b Dimensional Analsis Consider he diffusion problem from las secion, wih poinwise release (Ref: Bluman & Cole, 2.3): c = D 2 c x + Q 0δ(x)δ() 2 c(x,0) = 0, c(±,) = 0 Iniial release

More information

Lecture 4 Kinetics of a particle Part 3: Impulse and Momentum

Lecture 4 Kinetics of a particle Part 3: Impulse and Momentum MEE Engineering Mechanics II Lecure 4 Lecure 4 Kineics of a paricle Par 3: Impulse and Momenum Linear impulse and momenum Saring from he equaion of moion for a paricle of mass m which is subjeced o an

More information

Flow-Induced Vibration Analysis of Supported Pipes with a Crack

Flow-Induced Vibration Analysis of Supported Pipes with a Crack Flow-Induced Vibraion Analsis of Suppored Pipes wih a Crack Jin-Huk Lee, Samer Masoud Al-Said Deparmen of Mechanical Engineering American Universi of Sharjah, UAE Ouline Inroducion and Moivaion Aeroacousicall

More information

Differential Equations

Differential Equations Mah 21 (Fall 29) Differenial Equaions Soluion #3 1. Find he paricular soluion of he following differenial equaion by variaion of parameer (a) y + y = csc (b) 2 y + y y = ln, > Soluion: (a) The corresponding

More information

Numerical investigation of Ranque-Hilsch energy separation effect A.S. Noskov 1,a, V.N. Alekhin 1,b, A.V. Khait 1,a

Numerical investigation of Ranque-Hilsch energy separation effect A.S. Noskov 1,a, V.N. Alekhin 1,b, A.V. Khait 1,a Applied Mechanics and Maerials Online: 2013-01-11 ISSN: 1662-7482, Vol. 281, pp 355-358 doi:10.4028/www.scienific.ne/amm.281.355 2013 Trans Tech Publicaions, Swizerland Numerical invesigaion of Ranque-Hilsch

More information

Unsteady Mixed Convection Heat and Mass Transfer Past an Infinite Porous Plate with Thermophoresis Effect

Unsteady Mixed Convection Heat and Mass Transfer Past an Infinite Porous Plate with Thermophoresis Effect Unseady Mixed Convecion Hea and Mass Transfer Pas an Infinie Porous Plae wih Thermophoresis Effec TARIQ AL-AZAB Mechanical Engineering Deparmen, Al-Al-Sal Communiy College Al-Balqa Applied Universiy P.O.Box

More information

Numerical Simulation of the Overall Flow Field for Underwater Vehicle with Pump Jet Thruster

Numerical Simulation of the Overall Flow Field for Underwater Vehicle with Pump Jet Thruster Available online a www.sciencedirec.com Procedia Engineering 31 (2012) 769 774 Inernaional Conference on Advances in Compuaional Modeling and Simulaion Numerical Simulaion of he Overall Flow Field for

More information

Depletion of nonlinearity in two-dimensional turbulence. Abstract

Depletion of nonlinearity in two-dimensional turbulence. Abstract Depleion of nonlineariy in wo-dimensional urbulence Andrey V. Pushkarev and Wouer J.T. Bos LMFA, CNRS, Ecole Cenrale de Lyon, Universié de Lyon, 6934 Ecully, France arxiv:42.535v [physics.flu-dyn] 6 Dec

More information

Turbulence modelling. Sørensen, Niels N. Publication date: Link back to DTU Orbit

Turbulence modelling. Sørensen, Niels N. Publication date: Link back to DTU Orbit Downloaded from orbit.dtu.dk on: Dec 19, 2017 Turbulence modelling Sørensen, Niels N. Publication date: 2010 Link back to DTU Orbit Citation (APA): Sørensen, N. N. (2010). Turbulence modelling. Paper presented

More information

7 The Itô/Stratonovich dilemma

7 The Itô/Stratonovich dilemma 7 The Iô/Sraonovich dilemma The dilemma: wha does he idealizaion of dela-funcion-correlaed noise mean? ẋ = f(x) + g(x)η() η()η( ) = κδ( ). (1) Previously, we argued by a limiing procedure: aking noise

More information

EXPERIMENTAL AND NUMERICAL STUDIES OF FLOW IN A LOGARITHMIC SPIRAL CURVED DIFFUSER. Mohamed S. Mohamed, Berge Djebedjian and Magdy Abou Rayan

EXPERIMENTAL AND NUMERICAL STUDIES OF FLOW IN A LOGARITHMIC SPIRAL CURVED DIFFUSER. Mohamed S. Mohamed, Berge Djebedjian and Magdy Abou Rayan Proceedings of FEDSM 000 000 ASME Fluids Engineering Summer Conference June 11-15, 000, Boson FEDSM00-1118 EXPERIMENTAL AND NUMERICAL STUDIES OF FLOW IN A LOGARITHMIC SPIRAL CURVED DIFFUSER Mohamed S.

More information

Math Final Exam Solutions

Math Final Exam Solutions Mah 246 - Final Exam Soluions Friday, July h, 204 () Find explici soluions and give he inerval of definiion o he following iniial value problems (a) ( + 2 )y + 2y = e, y(0) = 0 Soluion: In normal form,

More information

R t. C t P t. + u t. C t = αp t + βr t + v t. + β + w t

R t. C t P t. + u t. C t = αp t + βr t + v t. + β + w t Exercise 7 C P = α + β R P + u C = αp + βr + v (a) (b) C R = α P R + β + w (c) Assumpions abou he disurbances u, v, w : Classical assumions on he disurbance of one of he equaions, eg. on (b): E(v v s P,

More information

The Green Kubo Relations

The Green Kubo Relations Chaper 4. The Green Kubo Relaions 4.1 The Langevin Equaion 4.2 Mori-Zwanzig Theory 4.3 Shear Viscosiy 4.4 Green-Kubo Relaions for Navier-Sokes Transpor Coefficiens Chaper 4-2 4.1 The Langevin Equaion In

More information

GEM4 Summer School OpenCourseWare

GEM4 Summer School OpenCourseWare GEM4 Summer School OpenCourseWare hp://gem4.educommons.ne/ hp://www.gem4.org/ Lecure: Thermal Forces and Brownian Moion by Ju Li. Given Augus 11, 2006 during he GEM4 session a MIT in Cambridge, MA. Please

More information

Relaxation. T1 Values. Longitudinal Relaxation. dm z dt. = " M z T 1. (1" e "t /T 1 ) M z. (t) = M 0

Relaxation. T1 Values. Longitudinal Relaxation. dm z dt. =  M z T 1. (1 e t /T 1 ) M z. (t) = M 0 Relaxaion Bioengineering 28A Principles of Biomedical Imaging Fall Quarer 21 MRI Lecure 2 An exciaion pulse roaes he magneiaion vecor away from is equilibrium sae (purely longiudinal). The resuling vecor

More information

TURBULENCE MODEL ANALYSIS OF FLOW INSIDE A HYDROCYCLONE

TURBULENCE MODEL ANALYSIS OF FLOW INSIDE A HYDROCYCLONE Sevenh Inernaional Conference on CFD in he Minerals and Process Indusries CSIRO, Melbourne, Ausralia 9-11 December 009 TURBULENCE MODEL ANALYSIS OF FLOW INSIDE A HYDROCYCLONE D.W. STEPHENS* AND K. MOHANARANGAM

More information

System of Linear Differential Equations

System of Linear Differential Equations Sysem of Linear Differenial Equaions In "Ordinary Differenial Equaions" we've learned how o solve a differenial equaion for a variable, such as: y'k5$e K2$x =0 solve DE yx = K 5 2 ek2 x C_C1 2$y''C7$y

More information

Representation of Stochastic Process by Means of Stochastic Integrals

Representation of Stochastic Process by Means of Stochastic Integrals Inernaional Journal of Mahemaics Research. ISSN 0976-5840 Volume 5, Number 4 (2013), pp. 385-397 Inernaional Research Publicaion House hp://www.irphouse.com Represenaion of Sochasic Process by Means of

More information

Simulation-Solving Dynamic Models ABE 5646 Week 2, Spring 2010

Simulation-Solving Dynamic Models ABE 5646 Week 2, Spring 2010 Simulaion-Solving Dynamic Models ABE 5646 Week 2, Spring 2010 Week Descripion Reading Maerial 2 Compuer Simulaion of Dynamic Models Finie Difference, coninuous saes, discree ime Simple Mehods Euler Trapezoid

More information

Wall. x(t) f(t) x(t = 0) = x 0, t=0. which describes the motion of the mass in absence of any external forcing.

Wall. x(t) f(t) x(t = 0) = x 0, t=0. which describes the motion of the mass in absence of any external forcing. MECHANICS APPLICATIONS OF SECOND-ORDER ODES 7 Mechanics applicaions of second-order ODEs Second-order linear ODEs wih consan coefficiens arise in many physical applicaions. One physical sysems whose behaviour

More information

k B 2 Radiofrequency pulses and hardware

k B 2 Radiofrequency pulses and hardware 1 Exra MR Problems DC Medical Imaging course April, 214 he problems below are harder, more ime-consuming, and inended for hose wih a more mahemaical background. hey are enirely opional, bu hopefully will

More information

NUMERICAL INVESTIGATION OF STROUHAL FREQUENCIES OF TWO STAGGERED BLUFF BODIES

NUMERICAL INVESTIGATION OF STROUHAL FREQUENCIES OF TWO STAGGERED BLUFF BODIES NUMERICAL INVESTIGATION OF STROUHAL FREQUENCIES OF TWO STAGGERED BLUFF BODIES Eswaran M 1, P. Goyal, Anu Dua, G.R. Reddy, R. K. Singh and K.K. Vaze Bhabha Aomic Research Cenre, Mumbai, India. 1 Corresponding

More information

Smagorinsky constant in LES modeling of anisotropic MHD turbulence

Smagorinsky constant in LES modeling of anisotropic MHD turbulence Theor. Compu. Fluid Dyn. DOI.7/s62-7-64-z ORIIAL ARTICLE Anaoliy Vorobev Oleg Zianov Smagorinsy consan in LES modeling of anisoropic MHD urbulence Received: 3 May 26 / Acceped: 7 Augus 27 Springer-Verlag

More information

Harmonic oscillator in quantum mechanics

Harmonic oscillator in quantum mechanics Harmonic oscillaor in quanum mechanics PHYS400, Deparmen of Physics, Universiy of onnecicu hp://www.phys.uconn.edu/phys400/ Las modified: May, 05 Dimensionless Schrödinger s equaion in quanum mechanics

More information

arxiv: v1 [math.fa] 3 Jan 2019

arxiv: v1 [math.fa] 3 Jan 2019 DAMPED AND DIVERGENCE EXACT SOLUTIONS FOR THE DUFFING EQUATION USING LEAF FUNCTIONS AND HYPERBOLIC LEAF FUNCTIONS A PREPRINT arxiv:9.66v [mah.fa] Jan 9 Kazunori Shinohara Deparmen of Mechanical Sysems

More information

CFD Investigation on the Steady Interaction between an Offset Jet and an Oblique Wall Jet

CFD Investigation on the Steady Interaction between an Offset Jet and an Oblique Wall Jet Journal of Applied Fluid Mechanics, Vol. 11, No. 4, pp. 885-894, 218. Available online a www.afmonline.ne, ISSN 1735-3572, EISSN 1735-3645. DOI: 1.18869/acadpub.afm.73.247.28214 CFD Invesigaion on he Seady

More information

Transform Techniques. Moment Generating Function

Transform Techniques. Moment Generating Function Transform Techniques A convenien way of finding he momens of a random variable is he momen generaing funcion (MGF). Oher ransform echniques are characerisic funcion, z-ransform, and Laplace ransform. Momen

More information

Lecture 14. The term Brownian motion derives its name from the botanist Robert Brown whom, in 1828, made careful

Lecture 14. The term Brownian motion derives its name from the botanist Robert Brown whom, in 1828, made careful Lecure 4. Brownian moion. Einsein-Smoluhowski heory of he Brownian moion. Langevin heory of he Brownian moion Approach o equilibrium: Foker-Planck equaion. The flucuaion-dissipaion heorem. The erm Brownian

More information

ON THE EVALUATION OF NUMERICAL DISSIPATION RATE AND VISCOSITY IN A COMMERCIAL CFD CODE

ON THE EVALUATION OF NUMERICAL DISSIPATION RATE AND VISCOSITY IN A COMMERCIAL CFD CODE June 30 - July 3, 2015 Melbourne, Ausralia 9 7B-1 ON THE EVALUATION OF NUMERICAL DISSIPATION RATE AND VISCOSITY IN A COMMERCIAL CFD CODE G. Casiglioni and J. A. Domaradzki Deparmen of Aerospace and Mechanical

More information

From Particles to Rigid Bodies

From Particles to Rigid Bodies Rigid Body Dynamics From Paricles o Rigid Bodies Paricles No roaions Linear velociy v only Rigid bodies Body roaions Linear velociy v Angular velociy ω Rigid Bodies Rigid bodies have boh a posiion and

More information

Stochastic Modelling in Finance - Solutions to sheet 8

Stochastic Modelling in Finance - Solutions to sheet 8 Sochasic Modelling in Finance - Soluions o shee 8 8.1 The price of a defaulable asse can be modeled as ds S = µ d + σ dw dn where µ, σ are consans, (W ) is a sandard Brownian moion and (N ) is a one jump

More information

MEC 654 Polytechnique-UPMC-Caltech Year

MEC 654 Polytechnique-UPMC-Caltech Year MEC 654 Polyechnique-UPMC-Calech Year 04-05 urbulence eaching Course : raining : Lauren Jacquin Professor a Ecole Polyechnique Direcor of Fundamenal / Experimenal Aerodynamics Dep (DAFE) ONERA (French

More information

4.1 Other Interpretations of Ridge Regression

4.1 Other Interpretations of Ridge Regression CHAPTER 4 FURTHER RIDGE THEORY 4. Oher Inerpreaions of Ridge Regression In his secion we will presen hree inerpreaions for he use of ridge regression. The firs one is analogous o Hoerl and Kennard reasoning

More information

COMPUTATIONAL STUDY OF STRATIFIED TWO PHASE OIL/WATER FLOW IN HORIZONTAL PIPES

COMPUTATIONAL STUDY OF STRATIFIED TWO PHASE OIL/WATER FLOW IN HORIZONTAL PIPES HEFAT2008 6 h Inernaional Conference on Hea Transfer, Fluid Mechanics and Thermodynamics 30 June o 2 July 2008 Preoria, Souh Africa Paper number: KW1 COMPUTATIONAL STUDY OF STRATIFIED TWO PHASE OIL/WATER

More information

Math 221: Mathematical Notation

Math 221: Mathematical Notation Mah 221: Mahemaical Noaion Purpose: One goal in any course is o properly use he language o ha subjec. These noaions summarize some o he major conceps and more diicul opics o he uni. Typing hem helps you

More information

Class Meeting # 10: Introduction to the Wave Equation

Class Meeting # 10: Introduction to the Wave Equation MATH 8.5 COURSE NOTES - CLASS MEETING # 0 8.5 Inroducion o PDEs, Fall 0 Professor: Jared Speck Class Meeing # 0: Inroducion o he Wave Equaion. Wha is he wave equaion? The sandard wave equaion for a funcion

More information

Polymer Engineering (MM3POE)

Polymer Engineering (MM3POE) Polymer Engineering (MM3POE) VISCOELASTICITY hp://www.noingham.ac.uk/~eazacl/mm3poe Viscoelasiciy 1 Conens Wha is viscoelasiciy? Fundamenals Creep & creep recovery Sress relaxaion Modelling viscoelasic

More information

Computation of Developing Turbulent Flow through a Straight Asymmetric Diffuser with Moderate Adverse Pressure Gradient

Computation of Developing Turbulent Flow through a Straight Asymmetric Diffuser with Moderate Adverse Pressure Gradient Journal of Applied Fluid Mechanics, Vol. 0, No. 4, pp. 09-043, 07. Available online a www.afmonline.ne, ISSN 735-357, EISSN 735-3645. DOI: 0.8869/acadpub.afm.73.4.63 Compuaion of Developing Turbulen Flow

More information

Summary of shear rate kinematics (part 1)

Summary of shear rate kinematics (part 1) InroToMaFuncions.pdf 4 CM465 To proceed o beer-designed consiuive equaions, we need o know more abou maerial behavior, i.e. we need more maerial funcions o predic, and we need measuremens of hese maerial

More information

IB Physics Kinematics Worksheet

IB Physics Kinematics Worksheet IB Physics Kinemaics Workshee Wrie full soluions and noes for muliple choice answers. Do no use a calculaor for muliple choice answers. 1. Which of he following is a correc definiion of average acceleraion?

More information

Numerical Investigation of Medium Range Re Number Aerodynamics Characteristics for NACA0018 Airfoil

Numerical Investigation of Medium Range Re Number Aerodynamics Characteristics for NACA0018 Airfoil Hassan e al FD Leers Vol. 6(4) 014 www.cfdl.issres.ne Vol. 6 (4) December 014 Numerical Invesigaion of Medium Range Re Number Aerodynamics haracerisics for NAA0018 Airfoil asser E. Hassan 1c, Amany Hassan,

More information

Math 23 Spring Differential Equations. Final Exam Due Date: Tuesday, June 6, 5pm

Math 23 Spring Differential Equations. Final Exam Due Date: Tuesday, June 6, 5pm Mah Spring 6 Differenial Equaions Final Exam Due Dae: Tuesday, June 6, 5pm Your name (please prin): Insrucions: This is an open book, open noes exam. You are free o use a calculaor or compuer o check your

More information

Econ Autocorrelation. Sanjaya DeSilva

Econ Autocorrelation. Sanjaya DeSilva Econ 39 - Auocorrelaion Sanjaya DeSilva Ocober 3, 008 1 Definiion Auocorrelaion (or serial correlaion) occurs when he error erm of one observaion is correlaed wih he error erm of any oher observaion. This

More information

t is a basis for the solution space to this system, then the matrix having these solutions as columns, t x 1 t, x 2 t,... x n t x 2 t...

t is a basis for the solution space to this system, then the matrix having these solutions as columns, t x 1 t, x 2 t,... x n t x 2 t... Mah 228- Fri Mar 24 5.6 Marix exponenials and linear sysems: The analogy beween firs order sysems of linear differenial equaions (Chaper 5) and scalar linear differenial equaions (Chaper ) is much sronger

More information

Hall Effects on Rayleigh-Stokes Problem for Heated Second Grade Fluid

Hall Effects on Rayleigh-Stokes Problem for Heated Second Grade Fluid Proceedings of he Pakisan Academy of Sciences 49 (3):193 198 (1) Copyrigh Pakisan Academy of Sciences ISSN: 377-969 Pakisan Academy of Sciences Original Aricle Hall Effecs on Rayleigh-Sokes Problem for

More information

The equation to any straight line can be expressed in the form:

The equation to any straight line can be expressed in the form: Sring Graphs Par 1 Answers 1 TI-Nspire Invesigaion Suden min Aims Deermine a series of equaions of sraigh lines o form a paern similar o ha formed by he cables on he Jerusalem Chords Bridge. Deermine he

More information

Couplage du principe des grandes déviations et de l homogénisation dans le cas des EDP paraboliques: (le cas constant)

Couplage du principe des grandes déviations et de l homogénisation dans le cas des EDP paraboliques: (le cas constant) Couplage du principe des grandes déviaions e de l homogénisaion dans le cas des EDP paraboliques: (le cas consan) Alioune COULIBALY U.F.R Sciences e Technologie Universié Assane SECK de Ziguinchor Probabilié

More information

FloEFD simulation of micro-turbine engine

FloEFD simulation of micro-turbine engine FloEFD simulaion of micro-urbine engine T.V. Trebunskikh, A.V. Ivanov, G.E. Dumnov Menor Graphics, Moscow, Russia Absrac Keywords: micro-urbine engine, CFD, combusion, compressor, urbine Turboje engines

More information

Electrical Circuits. 1. Circuit Laws. Tools Used in Lab 13 Series Circuits Damped Vibrations: Energy Van der Pol Circuit

Electrical Circuits. 1. Circuit Laws. Tools Used in Lab 13 Series Circuits Damped Vibrations: Energy Van der Pol Circuit V() R L C 513 Elecrical Circuis Tools Used in Lab 13 Series Circuis Damped Vibraions: Energy Van der Pol Circui A series circui wih an inducor, resisor, and capacior can be represened by Lq + Rq + 1, a

More information

1 1 + x 2 dx. tan 1 (2) = ] ] x 3. Solution: Recall that the given integral is improper because. x 3. 1 x 3. dx = lim dx.

1 1 + x 2 dx. tan 1 (2) = ] ] x 3. Solution: Recall that the given integral is improper because. x 3. 1 x 3. dx = lim dx. . Use Simpson s rule wih n 4 o esimae an () +. Soluion: Since we are using 4 seps, 4 Thus we have [ ( ) f() + 4f + f() + 4f 3 [ + 4 4 6 5 + + 4 4 3 + ] 5 [ + 6 6 5 + + 6 3 + ]. 5. Our funcion is f() +.

More information

Reliability of Technical Systems

Reliability of Technical Systems eliabiliy of Technical Sysems Main Topics Inroducion, Key erms, framing he problem eliabiliy parameers: Failure ae, Failure Probabiliy, Availabiliy, ec. Some imporan reliabiliy disribuions Componen reliabiliy

More information

Some Basic Information about M-S-D Systems

Some Basic Information about M-S-D Systems Some Basic Informaion abou M-S-D Sysems 1 Inroducion We wan o give some summary of he facs concerning unforced (homogeneous) and forced (non-homogeneous) models for linear oscillaors governed by second-order,

More information

Finite Element Analysis of Structures

Finite Element Analysis of Structures KAIT OE5 Finie Elemen Analysis of rucures Mid-erm Exam, Fall 9 (p) m. As shown in Fig., we model a russ srucure of uniform area (lengh, Area Am ) subjeced o a uniform body force ( f B e x N / m ) using

More information

Physics 127b: Statistical Mechanics. Fokker-Planck Equation. Time Evolution

Physics 127b: Statistical Mechanics. Fokker-Planck Equation. Time Evolution Physics 7b: Saisical Mechanics Fokker-Planck Equaion The Langevin equaion approach o he evoluion of he velociy disribuion for he Brownian paricle migh leave you uncomforable. A more formal reamen of his

More information

arxiv:math/ v1 [math.pr] 27 Jul 2006

arxiv:math/ v1 [math.pr] 27 Jul 2006 Sochasic Sokes drif wih ineria arxiv:mah/6777v1 [mah.pr] 27 Jul 26 By Kalvis M. Jansons Deparmen of Mahemaics, Universiy College London, Gower Sree, London WC1E 6BT, UK We consider boh he effec of paricle

More information

Week 1 Lecture 2 Problems 2, 5. What if something oscillates with no obvious spring? What is ω? (problem set problem)

Week 1 Lecture 2 Problems 2, 5. What if something oscillates with no obvious spring? What is ω? (problem set problem) Week 1 Lecure Problems, 5 Wha if somehing oscillaes wih no obvious spring? Wha is ω? (problem se problem) Sar wih Try and ge o SHM form E. Full beer can in lake, oscillaing F = m & = ge rearrange: F =

More information

Applications of the Basic Equations Chapter 3. Paul A. Ullrich

Applications of the Basic Equations Chapter 3. Paul A. Ullrich Applicaions of he Basic Equaions Chaper 3 Paul A. Ullrich paullrich@ucdavis.edu Par 1: Naural Coordinaes Naural Coordinaes Quesion: Why do we need anoher coordinae sysem? Our goal is o simplify he equaions

More information

AP CALCULUS AB 2003 SCORING GUIDELINES (Form B)

AP CALCULUS AB 2003 SCORING GUIDELINES (Form B) SCORING GUIDELINES (Form B) Quesion A blood vessel is 6 millimeers (mm) long Disance wih circular cross secions of varying diameer. x (mm) 6 8 4 6 Diameer The able above gives he measuremens of he B(x)

More information

1. VELOCITY AND ACCELERATION

1. VELOCITY AND ACCELERATION 1. VELOCITY AND ACCELERATION 1.1 Kinemaics Equaions s = u + 1 a and s = v 1 a s = 1 (u + v) v = u + as 1. Displacemen-Time Graph Gradien = speed 1.3 Velociy-Time Graph Gradien = acceleraion Area under

More information

Lecture #31, 32: The Ornstein-Uhlenbeck Process as a Model of Volatility

Lecture #31, 32: The Ornstein-Uhlenbeck Process as a Model of Volatility Saisics 441 (Fall 214) November 19, 21, 214 Prof Michael Kozdron Lecure #31, 32: The Ornsein-Uhlenbeck Process as a Model of Volailiy The Ornsein-Uhlenbeck process is a di usion process ha was inroduced

More information

Physical Transport in Surface Waters

Physical Transport in Surface Waters Physical Transpor in Surface Waers odule : Surface Waers, ecure 1 Chemical Fae and Transpor in he Environmen, nd ediion. H.F. Hemond and E.J. Fechner-evy. Academic Press. ondon. 000..1.1 Naure of Surface

More information

Math 334 Test 1 KEY Spring 2010 Section: 001. Instructor: Scott Glasgow Dates: May 10 and 11.

Math 334 Test 1 KEY Spring 2010 Section: 001. Instructor: Scott Glasgow Dates: May 10 and 11. 1 Mah 334 Tes 1 KEY Spring 21 Secion: 1 Insrucor: Sco Glasgow Daes: Ma 1 and 11. Do NOT wrie on his problem saemen bookle, excep for our indicaion of following he honor code jus below. No credi will be

More information

3, so θ = arccos

3, so θ = arccos Mahemaics 210 Professor Alan H Sein Monday, Ocober 1, 2007 SOLUTIONS This problem se is worh 50 poins 1 Find he angle beween he vecors (2, 7, 3) and (5, 2, 4) Soluion: Le θ be he angle (2, 7, 3) (5, 2,

More information

LAPLACE TRANSFORM AND TRANSFER FUNCTION

LAPLACE TRANSFORM AND TRANSFER FUNCTION CHBE320 LECTURE V LAPLACE TRANSFORM AND TRANSFER FUNCTION Professor Dae Ryook Yang Spring 2018 Dep. of Chemical and Biological Engineering 5-1 Road Map of he Lecure V Laplace Transform and Transfer funcions

More information

Turbulence - Theory and Modelling GROUP-STUDIES:

Turbulence - Theory and Modelling GROUP-STUDIES: Lund Institute of Technology Department of Energy Sciences Division of Fluid Mechanics Robert Szasz, tel 046-0480 Johan Revstedt, tel 046-43 0 Turbulence - Theory and Modelling GROUP-STUDIES: Turbulence

More information

arxiv: v1 [math.na] 23 Feb 2016

arxiv: v1 [math.na] 23 Feb 2016 EPJ Web of Conferences will be se by he publisher DOI: will be se by he publisher c Owned by he auhors, published by EDP Sciences, 16 arxiv:163.67v1 [mah.na] 3 Feb 16 Numerical Soluion of a Nonlinear Inegro-Differenial

More information

Computation of turbulent buoyant ows in enclosures with low-reynolds-number k-x models

Computation of turbulent buoyant ows in enclosures with low-reynolds-number k-x models Inernaional Journal of Hea and Fluid Flow 0 (1999) 17±184 Compuaion of urbulen buoyan ows in enclosures wih low-reynolds-number k-x models Shia-Hui Peng a,b, Lars Davidson a, * a Thermo and Fluid Dynamics,

More information