SOLUTION OF BOUNDARY LAYER



Similar documents
DIFFERENTIAL FORMULATION OF THE BASIC LAWS

8. Forced Convection Heat Transfer

Figure 2.1. a. Block diagram representation of a system; b. block diagram representation of an interconnection of subsystems

Risk Management for Derivatives


Climate control of a bulk storage room for foodstuffs

1D STEADY STATE HEAT

Heat transfer to or from a fluid flowing through a tube

Incline and Friction Examples

Pipe Flow Calculations

ME THERMODYNAMICS I

CIVE2400 Fluid Mechanics. Section 1: Fluid Flow in Pipes

Heat and Mass Correlations

A) When two objects slide against one another, the magnitude of the frictional force is always equal to μ

Give a formula for the velocity as a function of the displacement given that when s = 1 metre, v = 2 m s 1. (7)

Worked Examples. v max =?

Darcy Friction Factor Formulae in Turbulent Pipe Flow

Chapter 5: Applying Newton s Laws

Empirical correlations of overconsolidation ratio, coefficient of earth pressure at rest and undrained strength

Basic Principles in Microfluidics

6. Friction, Experiment and Theory

Tridiagonal Solvers on the GPU and Applications to Fluid Simulation. Nikolai Sakharnykh, NVIDIA

EXAMPLE: Water Flow in a Pipe

Work, Energy & Power. AP Physics B

THE EFFECTS OF DUCT SHAPE ON THE NUSSELT NUMBER

Prediction of Pressure Drop in Chilled Water Piping System Using Theoretical and CFD Analysis

Mannheim curves in the three-dimensional sphere

Heat Transfer Prof. Dr. Ale Kumar Ghosal Department of Chemical Engineering Indian Institute of Technology, Guwahati

Solution of the Heat Equation for transient conduction by LaPlace Transform

U = x x x 1 4. What are the equilibrium relative prices of the three goods? traders has members who are best off?

Rotated Ellipses. And Their Intersections With Lines. Mark C. Hendricks, Ph.D. Copyright March 8, 2012

Graph-based Simplex Method for Pairwise Energy Minimization with Binary Variables

MECH Statics & Dynamics

Chapter 11 Relative Velocity

4 Impulse and Impact. Table of contents:

CHAPTER ONE VECTOR GEOMETRY

Basic Equations, Boundary Conditions and Dimensionless Parameters

ES240 Solid Mechanics Fall Stress field and momentum balance. Imagine the three-dimensional body again. At time t, the material particle ( x, y,

Open channel flow Basic principle

11 CHAPTER 11: FOOTINGS

Accurate Calibration of Stereo Cameras for Machine Vision

Section 1.4. Difference Equations

Fluid Pressure and Fluid Force

The Concept of the Effective Mass Tensor in GR. The Equation of Motion

Scalar Transport. Introduction. T. J. Craft George Begg Building, C41. Eddy-Diffusivity Modelling. TPFE MSc Advanced Turbulence Modelling

and that of the outgoing water is mv f

LINES AND PLANES IN R 3

Fluid Mechanics: Static s Kinematics Dynamics Fluid

SIMULATION OF DIRECT TORQUE CONTROLLED PERMANENT MAGNET SYNCHRONOUS MOTOR DRIVE

Numerical investigation of heat transfer process form with constant heat flux in exothermic board by natural convection inside a closed cavity

Lecture 7 Force and Motion. Practice with Free-body Diagrams and Newton s Laws

FLUID DYNAMICS. Intrinsic properties of fluids. Fluids behavior under various conditions

CSI:FLORIDA. Section 4.4: Logistic Regression

Kinetic Molecular Theory of Matter

The FitzHugh-Nagumo Model

On Secure Network Coding with Unequal Link Capacities and Restricted Wiretapping Sets

Heat Transfer From A Heated Vertical Plate

MHD effects on natural convection laminar flow from a horizontal circular cylinder in presence of radiation

Chapter 8: Flow in Pipes

Bob York. Simple FET DC Bias Circuits

σ m using Equation 8.1 given that σ

Reading: Ryden chs. 3 & 4, Shu chs. 15 & 16. For the enthusiasts, Shu chs. 13 & 14.

Practice Problems on the Navier-Stokes Equations

Precision Mass Flow Metering For CVD Applications.

Iterative calculation of the heat transfer coefficient

HEAT AND MASS TRANSFER

A technical guide to 2014 key stage 2 to key stage 4 value added measures

Turbulent Mixing and Chemical Reaction in Stirred Tanks

Black-Scholes model under Arithmetic Brownian Motion

On sediment transport under dam-break flow

Lecture 6 Black-Scholes PDE

Ross Recovery Empirical Project

Pipe flow with friction losses solutions using HP and TI calculators By Gilberto E. Urroz, October 2005

240EQ014 - Transportation Science

LAB1 2D and 3D step-index waveguides. TE and TM modes.

Flow Calculations for the V-Cone and Wafer-Cone Flowmeters

Optimal Digital Content Distribution Strategy in the Presence of the Consumer-to-Consumer Channel

Dimensionless versus Dimensional Analysis in CFD and Heat Transfer

Heat transfer in Flow Through Conduits

FLUID FLOW STREAMLINE LAMINAR FLOW TURBULENT FLOW REYNOLDS NUMBER

THE FLEXURE AND SHEAR DESIGN OF CORBEL (BRACKET)

Poiseuille and Nusselt Numbers for Laminar Flow in Microchannels with Rounded Corners

3 The boundary layer equations

Viscous flow in pipe

CE 3500 Fluid Mechanics / Fall 2014 / City College of New York

Advanced Multiphase Modeling of Solidification

University of Maryland Fraternity & Sorority Life Spring 2015 Academic Report

Acceleration due to Gravity

Ch 2 Properties of Fluids - II. Ideal Fluids. Real Fluids. Viscosity (1) Viscosity (3) Viscosity (2)

Two Dimensional FEM Simulation of Ultrasonic Wave Propagation in Isotropic Solid Media using COMSOL

Transcription:

SOUION OF BOUNDARY AYER EQUAIONS Prabal alkar Aociate Proeor Department o Mechanical Engineering II Delhi E-mail: prabal@mech.iit.ac.in P.alkar/Mech-IID

Bonar laer Approimation X momentm: ρ μ P Appling Newton n law in the -irection, we get -momentm eqation ρ μ P h,p P P P() Hence, For a late plate, ince U contant an otie the bonar laer, X- momentm eqation gie P P P.alkar/Mech-IID hereore, or low oer a lat plate, the prere remain contant oer the entire plate (both inie an otie the bonar laer).

Bonar laer oer a lat plate P.alkar/Mech-IID

Pal Richar Heinrich Blai (88 97) wa a German Fli Dnamic Engineer. He wa one o the irt tent o Prantl. he continit an momentm eqation were irt ole in 98 b the German engineer H. Blai, a tent to. Prantl. Born Die Fiel Alma mater Doctoral aior 9 Agt 88 Berlin, German 4 April 97 (age 86) Hambrg, Wet German Fli mechanic an mechanical engineering Unierit o Göttingen wig Prantl hi wa one b tranorming the two partial ierential eqation into a ingle orinar ierential eqation b introcing a new inepenent ariable, calle the imilaritariable. he ining o ch a ariable, aming it eit, i more o an art than cience, an it reqire to hae a goo inight o the problem. P.alkar/Mech-IID

he hape o the elocit proile remain the ame along the plate. Blai reaone that the nonimenional elocit proile / hol remain nchange when plotte againt the nonimenional itance /δ, where δ i the thickne o the local elocit bonar laer at a gien. hat i, althogh both δ an at a gien ar with, the elocit at a ie / δ remain contant Blai wa alo aware rom the work o Stoke that δ i proportional to P.alkar/Mech-IID

Scale Anali Diiing b to epre the relt in imenionle orm gie P.alkar/Mech-IID

Similarit Variable he igniicant ariable i /δ, an we ame that the elocit ma be epree a a nction cto o othi aabe.wete ariable. then hae We hi eine make, / / δ Here, i calle the imilarit ariable, an g() i the nction we eek a a oltion P.alkar/Mech-IID

Variable ranormation A tream nction wa eine ch that: to get ri o continit eqation Ψ Ψ to get ri o continit eqation Ψ ( ) Ψ ) g( ) ( where ( ) ( ) Ψ Ψ Ψ Ψ Ψ P.alkar/Mech-IID

Dierentiating the preio eqation with repect to an, Sbtitting thee relation into the momentm eqation an, Sbtitting thee relation into the momentm eqation an impliing, we obtain hi i a thir-orer nonlinear ierential eqation. hi wa the tem o two PDE i conerte to one ODE hi wa the tem o two PDE i conerte to one ODE. P.alkar/Mech-IID

Blai Soltion he ale o correponing to /.99 i 5. 5 δ P.alkar/Mech-IID δ 5. 5. Re Signiicance o,,

P.alkar/Mech-IID

he hear tre at the wall can be etermine rom: τ w μ μ τ w ρμ.. ρ Re ocal kin riction coeicient become C, τ ρv w ρ τ w.664re P.alkar/Mech-IID Note that nlike the bonar laer thickne, wall hear tre an the kin riction coeicient ecreae along the plate a -/.

Energ Eqation Introce a non-imenional temperatre θ(, ) (, ) Sbtittion gie an energ eqation o the orm: θ θ θ α emperatre proile or low oer an iothermal lat plate are imilar like the elocit proile. h, we epect a imilarit oltion or temperatre to eit. Frther, the thickne o the thermal bonar laer i proportional to / Uing the chain rle an btitting the an epreion into the energ eqation gie θ θ θ α P.alkar/Mech-IID

Uing the chain rle an btitting the an epreion into the energ eqation gie θ θ θ α / i replace b θ θ θ Pr Compare For Pr θ ( ) an θ ( ) an h we concle that the elocit an thermal bonar laer coincie, an the nonimenional elocit an temperatre proile (/ an θ) areientical or tea, incompreible, laminar low o a li with contant propertie an Pr oer an iothermal lat plate he ale o the temperatre graient at the race (Pr )?? θ P.alkar/Mech-IID.

θ θ Pr hi eq. i ole or nmero ale o Prantl nmber. For Pr >.6, the nonimenional temperatre graient at the race i on to be proportional to Pr / Pr >.6 θ. Pr θ(, ) (, ) δ he temperatre graient at the race i θ ( ) ( ) θ ( ). Pr P.alkar/Mech-IID

P.alkar/Mech-IID hi oltion i gien b Pohlhaen

he local conection coeicient can be epree a: k q h. Pr k ( ) ( ). Pr ( ) An the local Nelt nmber become h N k. Pr Re Pr >.6 Soling the thermal bonar laer eqation nmericall or the temperatre proile or ierent Prantl nmber, an ing the einition o the thermal bonar laer, it i etermine that δ δ t Pr P.alkar/Mech-IID δ t δ Pr Pr 5. Re

Non-imenionalization Non imenionalization p μ ρ μ ρ k ρ p k c an V p,p V, V,, ρ P.alkar/Mech-IID

p Continit: p Re Momentm: Pr Re Energ: With the bonar conition: ( ) ( ) ( ) ( ) ( ) ( ) ( ) ( ) ( ) ( ) ( ),,,,,,,,,,,, P.alkar/Mech-IID

P.alkar/Mech-IID Geometricall Similar

Fnctional orm o Friction an Conection Coeicient i Momentm: p Re For a gien geometr, the oltion or can be epree a (,,Re ) hen the hear tre at the race become τ μ μ V μ V (, Re ) (, Re ) (, Re ) (, Re ) τ μv C, ρvv ρ V Re P.alkar/Mech-IID

Energ: he oltion or can be epree a Re Pr g (,,Re,Pr) Uing the einition o, the conection heat traner coeicient become h k k( ) ( ) k Nelt nmber: N h k g (, Re,Pr) Note that the Nelt nmber i eqialent to the imenionle temperatre graient at the race, an th it i properl reerre to a the imenionle heat traner coeicient P.alkar/Mech-IID

P.alkar/Mech-IID Aerage riction coeicient

Renol Analog Renol Analog When Pr (approimatel the cae or gae) an P/ (e g For lat Re or gae) an P / (e.g. For lat plate) Re h N k N N V V μ μ μ τ, N Re V N V V C ρ μ ρ τ, N Re C (Pr) Re V ρv ρ, St C (Pr) P.alkar/Mech-IID Pr Re N V c h St p ρ

Clinton-Colbrn Analog Alo calle moiie Renol analog C.664Re, N. Pr Re aking the ratio between C, an N Vali or.6<pr<6 P.alkar/Mech-IID C, Re C, N Pr Pr jh ρcpv h Colbrn j-actor Althogh thi relation i eelope ing relation or laminar low oer a lat plate (or which P/ ), eperimental tie how that it i alo applicable approimatel or trblent t low oer a race, een in the preence o prere graient. For laminar low, howeer, the analog i not applicable nle P/. hereore, it oe not appl to laminar low in a pipe