1.061 / 1.61 Transport Processes in the Environment

Size: px
Start display at page:

Download "1.061 / 1.61 Transport Processes in the Environment"

Transcription

1 MIT OpenCorseWare / 1.61 Transport Processes in the Environment Fall 008 For information abot citing these materials or or Terms of Use, visit:

2 Answer 8.1 Diffsion is a specific term referring to the net flx reslting from zero-mean, random motions. The random motions may be Brownian motion œ reslting in moleclar diffsion œ or may be de to trblent eddies. Strictly, the size of the eddies mst be small compared to the patch of particles in order for impact of the eddies on the patch to be trly random, and ths the net flx to be prely diffsive. Advection is the transport of particles (concentration) by the mean crrent. Dispersion is a broad term sed to describe all processes, except diffsion, that act to disperse a patch, and ths diminish concentration. Typically, dispersion coefficients reflect a combination of advection and diffsion processes that are difficlt to model separately. For example, the copled effect of differential longitdinal advection and cross-channel diffsion creates shear dispersion. The existence of mltiple discrete flow paths, e.g. throgh a poros medim, also creates a dispersion of particles, becase the time to traverse each path differs with its geometry and the degree of bending/trning œ often called the tortosity. Ths, many particles released together bt which take different pore pathways will get separated (dispersed) in the longitdinal direction. Finally, the lateral diffsion of particles into a region of zero velocity (a pore space with no otlet, a side-pool in a river, a wake behind an obstrction) will create longitdinal dispersion. The particles that enter the zones of zero velocity get held back relative to the particles that do not get trap. When the particles are eventally released from the dead-zone, they are separated in space (dispersed) from the rest of the clod. Answer 8. T he expression for longitdinal dispersion in a wide channel is K x = 5.93 * h, where * is the shear velocity and h the water depth. We wish to make the comparison, K X1 K X * 1h1 = (1) * h First consider how * will change between section 1 and. For steady niform flow driven by bed slope, the momentm balance reqires that * = ghs Eqation 3, Chapter 7. S ch that * 1/ * = (h 1 S 1 ) (h S ) () If the channel depth is constant, then from (1) K X1 = * 1 = S 1 K X * S > 1. The dispersion is greater in the steeper channel. If the channel width is constant, then from continity the channel depth mst change inversely with the depth-averaged velocity, U. Specifically, U1h1=U h, or h1/h = U/U1. (3)

3 If the sbstrate is the same, we can infer that U/ *, is constant. More formally, sing the drag coefficient for the bed, C b, we can write τbed=ρc b U =ρ *, which also indicates that for constant C b the ratio U/ * is constant, i.e. U1/ * 1 = U/ *. (4) Combining (3) and (4), h1/h = * / * 1. Using this ratio in (1), K X1 /K X = 1. That is, for a constant channel width, the longitdinal dispersion is the same in both sections. Answer 8.3 Vegetated Floodplain h1 h b When the water depth increases from h1 to h, flow enters the floodplain. Vegetative drag and the shallow depth combine to retard flow on the floodplain relative to the channel. This prodces strong lateral shear that agments dispersion. The lateral profile of depth-averaged velocity is shown below for flow depth h1 (red) and h (black). The velocity flctations, ', are deviations from the channel mean velocity, =Q/A total. Adapting the expression for shear dispersion (eq. 16, chap. 8) to the lateral shear, y y 1 B K x = ' ' dydydy, BD y 0 00 where B is the total channel width with the flood plain. From the sketch below, it is clear that the sm of spatial flctations, ', is greater when the water depth permits flow on the floodplain, and so we expect K X to increase at the greater water depth. This is a greater effect than the increase lateral diffsivity that might occr with increasing width, which according to the above eqation wold decrease K X. In particlar the lateral diffsivity cannot increase significantly throgh the floodplain becase of obstrction by vegetation.

4 Channel B Floodplain y ' ' Answer 8.4 Time t1<< B /4Dy: When the slg is initially released, it is very small compared to the width of the channel. Released in the center of the channel, the variation in velocity (shear) across the patch is negligible, and the entire patch advects at the same speed. Becase the patch is not experiencing differential advection, the spreading of the clod in the longitdinal direction is de to longitdinal diffsion only. The clod's longitdinal length scale is 4 Dt. More specifically, letting the release point be (x, y, z) = (0, 0, 0), the concentration field evolves as, M (x t) y z C(x, y, z, t) = 3/ exp ( 4 π Dt ) 4Dt 4Dt 4Dt

5 Time t>> 0.4 B /Dy. By this time the patch has grown to niformly fill the lateral dimension of the channel. In addition, sfficient time has passed for the longitdinal dispersion de to the lateral shear to reach Fickian behavior. The longitdinal length-scale of the patch is now 4 K x t, i.e. the patch growth rate is dictated by the dispersion coefficient, K X. In the vertical direction the clod contines to grow via vertical diffsion, sch that the concentration field evolves as, M DK x t exp (x - t) z C(x,z, t) = - - B 4π 4K x t 4Dt.

Momentum Equation. Necessary because body is not made up of a fixed assembly of particles Its volume is the same however Imaginary

Momentum Equation. Necessary because body is not made up of a fixed assembly of particles Its volume is the same however Imaginary Momentm Eqation Interest in the momentm eqation: Qantification of proplsion rates esign strctres for power generation esign of pipeline systems to withstand forces at bends and other places where the flow

More information

Prandl established a universal velocity profile for flow parallel to the bed given by

Prandl established a universal velocity profile for flow parallel to the bed given by EM 0--00 (Part VI) (g) The nderlayers shold be at least three thicknesses of the W 50 stone, bt never less than 0.3 m (Ahrens 98b). The thickness can be calclated sing Eqation VI-5-9 with a coefficient

More information

4 Exact laminar boundary layer solutions

4 Exact laminar boundary layer solutions 4 Eact laminar bondary layer soltions 4.1 Bondary layer on a flat plate (Blasis 1908 In Sec. 3, we derived the bondary layer eqations for 2D incompressible flow of constant viscosity past a weakly crved

More information

Spring Semester 2011 April 5, 2011

Spring Semester 2011 April 5, 2011 METR 130: Lectre 4 - Reynolds Averaged Conservation Eqations - Trblent Flxes (Definition and typical ABL profiles, CBL and SBL) - Trblence Closre Problem & Parameterization Spring Semester 011 April 5,

More information

5.1 Heat removal by coolant flow

5.1 Heat removal by coolant flow 5. Convective Heat Transfer 5.1 Heat removal by coolant flow Fel pellet Bond layer Cladding tbe Heat is transferred from the srfaces of the fel rods to the coolant. T Temperatre at center of fc fel pellet

More information

Applying Laminar and Turbulent Flow and measuring Velocity Profile Using MATLAB

Applying Laminar and Turbulent Flow and measuring Velocity Profile Using MATLAB IOS Jornal of Mathematics (IOS-JM) e-issn: 78-578, p-issn: 319-765X. Volme 13, Isse 6 Ver. II (Nov. - Dec. 17), PP 5-59 www.iosrjornals.org Applying Laminar and Trblent Flow and measring Velocity Profile

More information

The distortion observed in the bottom channel of Figure 1 can be predicted from the full transport equation, C t + u C. y D C. z, (1) x D C.

The distortion observed in the bottom channel of Figure 1 can be predicted from the full transport equation, C t + u C. y D C. z, (1) x D C. 1 8. Shear Dispersion. The transport models and concentration field solutions developed in previous sections assume that currents are spatially uniform, i.e. u f(,y,). However, spatial gradients of velocity,

More information

Effects of modifications on the hydraulics of Denil fishways

Effects of modifications on the hydraulics of Denil fishways BOREAL ENVIRONMENT RESEARCH 5: 67 79 ISSN 1239-6095 Helsinki 28 March 2000 2000 Effects of modifications on the hydralics of Denil fishways Riitta Kamla 1) and Jan Bärthel 2) 1) Water Resorces and Environmental

More information

Reflections on a mismatched transmission line Reflections.doc (4/1/00) Introduction The transmission line equations are given by

Reflections on a mismatched transmission line Reflections.doc (4/1/00) Introduction The transmission line equations are given by Reflections on a mismatched transmission line Reflections.doc (4/1/00) Introdction The transmission line eqations are given by, I z, t V z t l z t I z, t V z, t c z t (1) (2) Where, c is the per-nit-length

More information

Motion in One Dimension. A body is moving with velocity 3ms towards East. After s its velocity becomes 4ms towards North. The average acceleration of the body is a) 7ms b) 7ms c) 5ms d) ms. A boy standing

More information

EDEXCEL NATIONAL CERTIFICATE/DIPLOMA. PRINCIPLES AND APPLICATIONS of FLUID MECHANICS UNIT 13 NQF LEVEL 3 OUTCOME 3 - HYDRODYNAMICS

EDEXCEL NATIONAL CERTIFICATE/DIPLOMA. PRINCIPLES AND APPLICATIONS of FLUID MECHANICS UNIT 13 NQF LEVEL 3 OUTCOME 3 - HYDRODYNAMICS EDEXCEL NATIONAL CERTIFICATE/DIPLOMA PRINCIPLES AND APPLICATIONS of FLUID MECHANICS UNIT 3 NQF LEVEL 3 OUTCOME 3 - HYDRODYNAMICS TUTORIAL - PIPE FLOW CONTENT Be able to determine the parameters of pipeline

More information

Turbulence and boundary layers

Turbulence and boundary layers Trblence and bondary layers Weather and trblence Big whorls hae little whorls which feed on the elocity; and little whorls hae lesser whorls and so on to iscosity Lewis Fry Richardson Momentm eqations

More information

Section 7.4: Integration of Rational Functions by Partial Fractions

Section 7.4: Integration of Rational Functions by Partial Fractions Section 7.4: Integration of Rational Fnctions by Partial Fractions This is abot as complicated as it gets. The Method of Partial Fractions Ecept for a few very special cases, crrently we have no way to

More information

Discontinuous Fluctuation Distribution for Time-Dependent Problems

Discontinuous Fluctuation Distribution for Time-Dependent Problems Discontinos Flctation Distribtion for Time-Dependent Problems Matthew Hbbard School of Compting, University of Leeds, Leeds, LS2 9JT, UK meh@comp.leeds.ac.k Introdction For some years now, the flctation

More information

Mathematical and Numerical Modeling of Tsunamis in Nearshore Environment: Present and Future

Mathematical and Numerical Modeling of Tsunamis in Nearshore Environment: Present and Future Mathematical and Nmerical Modeling of Tsnamis in Nearshore Environment: Present and Ftre Philip L.-F. Li Cornell University DFG-Rond Table Discssion: Near- and Onshore Tsnami Effects FZK, Hannover, Germany,

More information

Pulses on a Struck String

Pulses on a Struck String 8.03 at ESG Spplemental Notes Plses on a Strck String These notes investigate specific eamples of transverse motion on a stretched string in cases where the string is at some time ndisplaced, bt with a

More information

UNIT V BOUNDARY LAYER INTRODUCTION

UNIT V BOUNDARY LAYER INTRODUCTION UNIT V BOUNDARY LAYER INTRODUCTION The variation of velocity from zero to free-stream velocity in the direction normal to the bondary takes place in a narrow region in the vicinity of solid bondary. This

More information

ρ u = u. (1) w z will become certain time, and at a certain point in space, the value of

ρ u = u. (1) w z will become certain time, and at a certain point in space, the value of THE CONDITIONS NECESSARY FOR DISCONTINUOUS MOTION IN GASES G I Taylor Proceedings of the Royal Society A vol LXXXIV (90) pp 37-377 The possibility of the propagation of a srface of discontinity in a gas

More information

FLUID FLOW FOR CHEMICAL ENGINEERING

FLUID FLOW FOR CHEMICAL ENGINEERING EKC FLUID FLOW FOR CHEMICL ENGINEERING CHTER 8 (SOLUTION WI EXERCISE): TRNSORTTION SYSTEM & FLUID METERING Dr Mohd zmier hmad Tel: +60 (4) 5996459 Email: chazmier@eng.sm.my . Benzene at 7.8 o C is pmped

More information

5. The Bernoulli Equation

5. The Bernoulli Equation 5. The Bernolli Eqation [This material relates predominantly to modles ELP034, ELP035] 5. Work and Energy 5. Bernolli s Eqation 5.3 An example of the se of Bernolli s eqation 5.4 Pressre head, velocity

More information

The prediction of turbulence intensities in unsteady flow

The prediction of turbulence intensities in unsteady flow University of Wollongong Research Online Faclty of Engineering and Information Sciences - Papers: Part A Faclty of Engineering and Information Sciences 24 The prediction of trblence intensities in nsteady

More information

Two identical, flat, square plates are immersed in the flow with velocity U. Compare the drag forces experienced by the SHADED areas.

Two identical, flat, square plates are immersed in the flow with velocity U. Compare the drag forces experienced by the SHADED areas. Two identical flat sqare plates are immersed in the flow with velocity U. Compare the drag forces experienced by the SHAE areas. F > F A. A B F > F B. B A C. FA = FB. It depends on whether the bondary

More information

Gravitational Instability of a Nonrotating Galaxy *

Gravitational Instability of a Nonrotating Galaxy * SLAC-PUB-536 October 25 Gravitational Instability of a Nonrotating Galaxy * Alexander W. Chao ;) Stanford Linear Accelerator Center Abstract Gravitational instability of the distribtion of stars in a galaxy

More information

CONCENTRATION METER FOR WIND TUNNEL STUDIES OF GASEOUS DISPERSION

CONCENTRATION METER FOR WIND TUNNEL STUDIES OF GASEOUS DISPERSION Atmospheric Environment Pergamon Press 1972. Vo\. 6, pp. 911-916. Printed in Great Britain. CONCENTRATION METER FOR WIND TUNNEL STUDIES OF GASEOUS DISPERSION JIRi MOTYCKA and HANS J. LEUTIIEUSSER Department

More information

Radiation Effects on Heat and Mass Transfer over an Exponentially Accelerated Infinite Vertical Plate with Chemical Reaction

Radiation Effects on Heat and Mass Transfer over an Exponentially Accelerated Infinite Vertical Plate with Chemical Reaction Radiation Effects on Heat and Mass Transfer over an Exponentially Accelerated Infinite Vertical Plate with Chemical Reaction A. Ahmed, M. N.Sarki, M. Ahmad Abstract In this paper the stdy of nsteady flow

More information

STATIC, STAGNATION, AND DYNAMIC PRESSURES

STATIC, STAGNATION, AND DYNAMIC PRESSURES STATIC, STAGNATION, AND DYNAMIC PRESSURES Bernolli eqation is g constant In this eqation is called static ressre, becase it is the ressre that wold be measred by an instrment that is static with resect

More information

A Model-Free Adaptive Control of Pulsed GTAW

A Model-Free Adaptive Control of Pulsed GTAW A Model-Free Adaptive Control of Plsed GTAW F.L. Lv 1, S.B. Chen 1, and S.W. Dai 1 Institte of Welding Technology, Shanghai Jiao Tong University, Shanghai 00030, P.R. China Department of Atomatic Control,

More information

Turbulence Deposition

Turbulence Deposition Trblene eposition ring trblent flid motions, partiles are transported by the trblene eddies and the Brownian diffsion. Ths, the partile flx is given by T dc J ( ) () dy where C is the average onentration

More information

DILUTE GAS-LIQUID FLOWS WITH LIQUID FILMS ON WALLS

DILUTE GAS-LIQUID FLOWS WITH LIQUID FILMS ON WALLS Forth International Conference on CFD in the Oil and Gas, Metallrgical & Process Indstries SINTEF / NTNU Trondheim, Noray 6-8 Jne 005 DILUTE GAS-LIQUID FLOWS WITH LIQUID FILMS ON WALLS John MORUD 1 1 SINTEF

More information

Kragujevac J. Sci. 34 (2012) UDC 532.5: :537.63

Kragujevac J. Sci. 34 (2012) UDC 532.5: :537.63 5 Kragjevac J. Sci. 34 () 5-. UDC 53.5: 536.4:537.63 UNSTEADY MHD FLOW AND HEAT TRANSFER BETWEEN PARALLEL POROUS PLATES WITH EXPONENTIAL DECAYING PRESSURE GRADIENT Hazem A. Attia and Mostafa A. M. Abdeen

More information

Homotopy Perturbation Method for Solving Linear Boundary Value Problems

Homotopy Perturbation Method for Solving Linear Boundary Value Problems International Jornal of Crrent Engineering and Technolog E-ISSN 2277 4106, P-ISSN 2347 5161 2016 INPRESSCO, All Rights Reserved Available at http://inpressco.com/categor/ijcet Research Article Homotop

More information

Section 9. Paraxial Raytracing

Section 9. Paraxial Raytracing OPTI-/ Geometrical and Instrmental Optics Copright 8 John E. Greivenkamp 9- Section 9 Paraxial atracing YNU atrace efraction (or reflection) occrs at an interface between two optical spaces. The transfer

More information

The Bow Shock and the Magnetosheath

The Bow Shock and the Magnetosheath Chapter 6 The Bow Shock and the Magnetosheath The solar wind plasma travels sally at speeds which are faster than any flid plasma wave relative to the magnetosphere. Therefore a standing shock wave forms

More information

Einstein Classes, Unit No. 102, 103, Vardhman Ring Road Plaza, Vikas Puri Extn., Outer Ring Road New Delhi , Ph. : ,

Einstein Classes, Unit No. 102, 103, Vardhman Ring Road Plaza, Vikas Puri Extn., Outer Ring Road New Delhi , Ph. : , PK K I N E M A T I C S Syllabs : Frame of reference. Motion in a straight line : Position-time graph, speed and velocity. Uniform and non-niform motion, average speed and instantaneos velocity. Uniformly

More information

A New Approach to Direct Sequential Simulation that Accounts for the Proportional Effect: Direct Lognormal Simulation

A New Approach to Direct Sequential Simulation that Accounts for the Proportional Effect: Direct Lognormal Simulation A ew Approach to Direct eqential imlation that Acconts for the Proportional ffect: Direct ognormal imlation John Manchk, Oy eangthong and Clayton Detsch Department of Civil & nvironmental ngineering University

More information

Finite Element Analysis of Heat and Mass Transfer of a MHD / Micropolar fluid over a Vertical Channel

Finite Element Analysis of Heat and Mass Transfer of a MHD / Micropolar fluid over a Vertical Channel International Jornal of Scientific and Innovative Mathematical Research (IJSIMR) Volme 2, Isse 5, Ma 214, PP 515-52 ISSN 2347-37X (Print) & ISSN 2347-3142 (Online) www.arcjornals.org Finite Element Analsis

More information

Classify by number of ports and examine the possible structures that result. Using only one-port elements, no more than two elements can be assembled.

Classify by number of ports and examine the possible structures that result. Using only one-port elements, no more than two elements can be assembled. Jnction elements in network models. Classify by nmber of ports and examine the possible strctres that reslt. Using only one-port elements, no more than two elements can be assembled. Combining two two-ports

More information

Design and Data Acquisition for Thermal Conductivity Matric Suction Sensors

Design and Data Acquisition for Thermal Conductivity Matric Suction Sensors 68 TRANSPORTATION RSARCH RCORD 1432 Design and Data Acqisition for Thermal Condctivity Matric Sction Sensors J. K.-M. GAN, D. G. FRDLUND, A. XING, AND W.-X. LI The principles behind sing the thermal condctivity

More information

10.2 Solving Quadratic Equations by Completing the Square

10.2 Solving Quadratic Equations by Completing the Square . Solving Qadratic Eqations b Completing the Sqare Consider the eqation ( ) We can see clearl that the soltions are However, What if the eqation was given to s in standard form, that is 6 How wold we go

More information

Lecture: Corporate Income Tax - Unlevered firms

Lecture: Corporate Income Tax - Unlevered firms Lectre: Corporate Income Tax - Unlevered firms Ltz Krschwitz & Andreas Löffler Disconted Cash Flow, Section 2.1, Otline 2.1 Unlevered firms Similar companies Notation 2.1.1 Valation eqation 2.1.2 Weak

More information

L = 2 λ 2 = λ (1) In other words, the wavelength of the wave in question equals to the string length,

L = 2 λ 2 = λ (1) In other words, the wavelength of the wave in question equals to the string length, PHY 309 L. Soltions for Problem set # 6. Textbook problem Q.20 at the end of chapter 5: For any standing wave on a string, the distance between neighboring nodes is λ/2, one half of the wavelength. The

More information

Modeling Effort on Chamber Clearing for IFE Liquid Chambers at UCLA

Modeling Effort on Chamber Clearing for IFE Liquid Chambers at UCLA Modeling Effort on Chamber Clearing for IFE Liqid Chambers at UCLA Presented by: P. Calderoni own Meeting on IFE Liqid Wall Chamber Dynamics Livermore CA May 5-6 3 Otline his presentation will address

More information

Formal Methods for Deriving Element Equations

Formal Methods for Deriving Element Equations Formal Methods for Deriving Element Eqations And the importance of Shape Fnctions Formal Methods In previos lectres we obtained a bar element s stiffness eqations sing the Direct Method to obtain eact

More information

Fluid Dynamics. Type of Flows Continuity Equation Bernoulli Equation Steady Flow Energy Equation Applications of Bernoulli Equation

Fluid Dynamics. Type of Flows Continuity Equation Bernoulli Equation Steady Flow Energy Equation Applications of Bernoulli Equation Tye of Flows Continity Eqation Bernolli Eqation Steady Flow Energy Eqation Alications of Bernolli Eqation Flid Dynamics Streamlines Lines having the direction of the flid velocity Flids cannot cross a

More information

This is a publisher-deposited version published in : Eprints ID : 18469

This is a publisher-deposited version published in :  Eprints ID : 18469 Open Archive TOULOUSE Archive Overte (OATAO) OATAO is an open access repository that collects the work of Tolose researchers and makes it freely available over the web where possible. This is a pblisher-deposited

More information

Physics of the Interstellar and Intergalactic Medium

Physics of the Interstellar and Intergalactic Medium Y4A04 Senior Sophister hysics of the Interstellar and Intergalactic edim Lectre 9: Shocks - revised Dr Graham. Harper School of hysics, TCD What a good physicist does best - Simplify eil Nebla ~8000 yr

More information

UNIT IV BOUNDARY LAYER AND FLOW THROUGH PIPES Definition of bonary layer Thickness an classification Displacement an momentm Thickness Development of laminar an trblent flows in circlar pipes Major an

More information

Lecture: Corporate Income Tax

Lecture: Corporate Income Tax Lectre: Corporate Income Tax Ltz Krschwitz & Andreas Löffler Disconted Cash Flow, Section 2.1, Otline 2.1 Unlevered firms Similar companies Notation 2.1.1 Valation eqation 2.1.2 Weak atoregressive cash

More information

A GNF framework for turbulent flow models of drag reducing fluids and proposal for a k ε type closure

A GNF framework for turbulent flow models of drag reducing fluids and proposal for a k ε type closure J. Non-Newtonian Flid Mech. 114 2003 149 184 A GNF framewor for trblent flow models of drag redcing flids and proposal for a ε type closre F. T. Pinho Centro de Estdos de Fenómenos de Transporte, DEMEGI,

More information

Study of the diffusion operator by the SPH method

Study of the diffusion operator by the SPH method IOSR Jornal of Mechanical and Civil Engineering (IOSR-JMCE) e-issn: 2278-684,p-ISSN: 2320-334X, Volme, Isse 5 Ver. I (Sep- Oct. 204), PP 96-0 Stdy of the diffsion operator by the SPH method Abdelabbar.Nait

More information

Variability sustained pattern formation in subexcitable media

Variability sustained pattern formation in subexcitable media Variability sstained pattern formation in sbexcitable media Erik Glatt, Martin Gassel, and Friedemann Kaiser Institte of Applied Physics, Darmstadt University of Technology, 64289 Darmstadt, Germany (Dated:

More information

Finite Difference Method of Modelling Groundwater Flow

Finite Difference Method of Modelling Groundwater Flow Jornal of Water Resorce and Protection, 20, 3, 92-98 doi:0.4236/warp.20.33025 Pblished Online March 20 (http://www.scirp.org/ornal/warp) Finite Difference Method of Modelling Grondwater Flow Abstract Magns.

More information

3.4-Miscellaneous Equations

3.4-Miscellaneous Equations .-Miscellaneos Eqations Factoring Higher Degree Polynomials: Many higher degree polynomials can be solved by factoring. Of particlar vale is the method of factoring by groping, however all types of factoring

More information

MODELLING OF TURBULENT ENERGY FLUX IN CANONICAL SHOCK-TURBULENCE INTERACTION

MODELLING OF TURBULENT ENERGY FLUX IN CANONICAL SHOCK-TURBULENCE INTERACTION MODELLING OF TURBULENT ENERGY FLUX IN CANONICAL SHOCK-TURBULENCE INTERACTION Rssell Qadros, Krishnend Sinha Department of Aerospace Engineering Indian Institte of Technology Bombay Mmbai, India 476 Johan

More information

1 JAXA Special Pblication JAXA-SP-1-E Small-scale trblence affects flow fields arond a blff body and therefore it governs characteristics of cross-sec

1 JAXA Special Pblication JAXA-SP-1-E Small-scale trblence affects flow fields arond a blff body and therefore it governs characteristics of cross-sec First International Symposim on Fltter and its Application, 1 11 IEXPERIMENTAL STUDY ON TURBULENCE PARTIAL SIMULATION FOR BLUFF BODY Hiroshi Katschi +1 and Hitoshi Yamada + +1 Yokohama National University,

More information

FEA Solution Procedure

FEA Solution Procedure EA Soltion Procedre (demonstrated with a -D bar element problem) EA Procedre for Static Analysis. Prepare the E model a. discretize (mesh) the strctre b. prescribe loads c. prescribe spports. Perform calclations

More information

Wall treatment in Large Eddy Simulation

Wall treatment in Large Eddy Simulation Wall treatment in arge Edd Simlation David Monfort Sofiane Benhamadoche (ED R&D) Pierre Sagat (Université Pierre et Marie Crie) 9 novembre 007 Code_Satrne User Meeting Wall treatment in arge Edd Simlation

More information

IJAET International Journal of Application of Engineering and Technology ISSN: Vol.1 No.1

IJAET International Journal of Application of Engineering and Technology ISSN: Vol.1 No.1 IJAET International Jornal of Application of Engineering and Technology ISSN: 395-3594 Vol1 No1 ANALYSIS OF SUPERSONIC FLOWS IN THE E -LAVAL NOZZLE AT 1 INTO A SUENLY EXPANE UCT AT L/=WITH CAVITY ASPECT

More information

The Linear Quadratic Regulator

The Linear Quadratic Regulator 10 The Linear Qadratic Reglator 10.1 Problem formlation This chapter concerns optimal control of dynamical systems. Most of this development concerns linear models with a particlarly simple notion of optimality.

More information

Second-Order Wave Equation

Second-Order Wave Equation Second-Order Wave Eqation A. Salih Department of Aerospace Engineering Indian Institte of Space Science and Technology, Thirvananthapram 3 December 016 1 Introdction The classical wave eqation is a second-order

More information

Flood flow at the confluence of compound river channels

Flood flow at the confluence of compound river channels Rier Basin Management VIII 37 Flood flow at the conflence of compond rier channels T. Ishikawa 1, R. Akoh 1 & N. Arai 2 1 Department of Enironmental Science and Technology, Tokyo Institte of Technology,

More information

Parametrization of turbulent fluxes in the outer layer

Parametrization of turbulent fluxes in the outer layer Parametriation of trblent flxes in the oter layer Irina Sand Oerie of models Blk models Local -closre -profile closre 0 order 1 st order ED/F closre non-local TE closre 1.5 th order Crrent closre in the

More information

Appendix A: The Fully Developed Velocity Profile for Turbulent Duct Flows

Appendix A: The Fully Developed Velocity Profile for Turbulent Duct Flows Appendix A: The lly Developed Velocity Profile for Trblent Dct lows This appendix discsses the hydrodynamically flly developed velocity profile for pipe and channel flows. The geometry nder consideration

More information

Microscopic Properties of Gases

Microscopic Properties of Gases icroscopic Properties of Gases So far we he seen the gas laws. These came from observations. In this section we want to look at a theory that explains the gas laws: The kinetic theory of gases or The kinetic

More information

Curves - Foundation of Free-form Surfaces

Curves - Foundation of Free-form Surfaces Crves - Fondation of Free-form Srfaces Why Not Simply Use a Point Matrix to Represent a Crve? Storage isse and limited resoltion Comptation and transformation Difficlties in calclating the intersections

More information

Residual Currents Induced by Asymmetric Tidal Mixing in Weakly Stratified Narrow Estuaries

Residual Currents Induced by Asymmetric Tidal Mixing in Weakly Stratified Narrow Estuaries SEPTEMBER 21 C H E N G E T A L. 2135 Residal Crrents Indced by Asymmetric Tidal Mixing in Weakly Stratified Narrow Estaries PENG CHENG* AND ARNOLDO VALLE-LEVINSON Department of Civil Coastal Engineering,

More information

RIVER & STREAMS HYDRAULICS

RIVER & STREAMS HYDRAULICS RIVER & STREAMS HYRAULICS Benoit Csman-Roisin artmot College River flow is 3 and nsteady (trblent). Bt: lengt of river >> widt & dept As a reslt, te downstream velocity, aligned wit te cannel, dominates

More information

Lesson 81: The Cross Product of Vectors

Lesson 81: The Cross Product of Vectors Lesson 8: The Cross Prodct of Vectors IBHL - SANTOWSKI In this lesson yo will learn how to find the cross prodct of two ectors how to find an orthogonal ector to a plane defined by two ectors how to find

More information

Two-media boundary layer on a flat plate

Two-media boundary layer on a flat plate Two-media bondary layer on a flat plate Nikolay Ilyich Klyev, Asgat Gatyatovich Gimadiev, Yriy Alekseevich Krykov Samara State University, Samara,, Rssia Samara State Aerospace University named after academician

More information

Ambipolar magnetic fluctuation-induced heat transport in toroidal devices*

Ambipolar magnetic fluctuation-induced heat transport in toroidal devices* Ambipolar magnetic flctation-indced heat transport in toroidal devices* P. W. Terry, G. Fisel, H. Ji, a) A. F. Almagri, M. Ceic, D. J. Den Hartog, P. H. Diamond, b) S. C. Prager, J. S. Sarff, W. Shen,

More information

arxiv: v1 [physics.flu-dyn] 4 Sep 2013

arxiv: v1 [physics.flu-dyn] 4 Sep 2013 THE THREE-DIMENSIONAL JUMP CONDITIONS FOR THE STOKES EQUATIONS WITH DISCONTINUOUS VISCOSITY, SINGULAR FORCES, AND AN INCOMPRESSIBLE INTERFACE PRERNA GERA AND DAVID SALAC arxiv:1309.1728v1 physics.fl-dyn]

More information

Chapter 6 Momentum Transfer in an External Laminar Boundary Layer

Chapter 6 Momentum Transfer in an External Laminar Boundary Layer 6. Similarit Soltions Chapter 6 Momentm Transfer in an Eternal Laminar Bondar Laer Consider a laminar incompressible bondar laer with constant properties. Assme the flow is stead and two-dimensional aligned

More information

Chapter 4 Supervised learning:

Chapter 4 Supervised learning: Chapter 4 Spervised learning: Mltilayer Networks II Madaline Other Feedforward Networks Mltiple adalines of a sort as hidden nodes Weight change follows minimm distrbance principle Adaptive mlti-layer

More information

Lecture Notes: Finite Element Analysis, J.E. Akin, Rice University

Lecture Notes: Finite Element Analysis, J.E. Akin, Rice University 9. TRUSS ANALYSIS... 1 9.1 PLANAR TRUSS... 1 9. SPACE TRUSS... 11 9.3 SUMMARY... 1 9.4 EXERCISES... 15 9. Trss analysis 9.1 Planar trss: The differential eqation for the eqilibrim of an elastic bar (above)

More information

Relativity II. The laws of physics are identical in all inertial frames of reference. equivalently

Relativity II. The laws of physics are identical in all inertial frames of reference. equivalently Relatiity II I. Henri Poincare's Relatiity Principle In the late 1800's, Henri Poincare proposed that the principle of Galilean relatiity be expanded to inclde all physical phenomena and not jst mechanics.

More information

WEAR PREDICTION OF A TOTAL KNEE PROSTHESIS TIBIAL TRAY

WEAR PREDICTION OF A TOTAL KNEE PROSTHESIS TIBIAL TRAY APPLIED PHYSICS MEDICAL WEAR PREDICTION OF A TOTAL KNEE PROSTHESIS TIBIAL TRAY L. CÃPITANU, A. IAROVICI, J. ONIªORU Institte of Solid Mechanics, Romanian Academy, Constantin Mille 5, Bcharest Received

More information

PhysicsAndMathsTutor.com

PhysicsAndMathsTutor.com . Two smooth niform spheres S and T have eqal radii. The mass of S is 0. kg and the mass of T is 0.6 kg. The spheres are moving on a smooth horizontal plane and collide obliqely. Immediately before the

More information

Localization in Undrained Deformation 1

Localization in Undrained Deformation 1 Localization in Undrained Deformation 1 J. W. Rdnicki Dept. of Civil and Env. Engn. and Dept. of Mech. Engn. Northwestern University Evanston, IL 6001-3109 John.Rdnicki@gmail.com Janary 7, 009 1 To appear

More information

A Decomposition Method for Volume Flux. and Average Velocity of Thin Film Flow. of a Third Grade Fluid Down an Inclined Plane

A Decomposition Method for Volume Flux. and Average Velocity of Thin Film Flow. of a Third Grade Fluid Down an Inclined Plane Adv. Theor. Appl. Mech., Vol. 1, 8, no. 1, 9 A Decomposition Method for Volme Flx and Average Velocit of Thin Film Flow of a Third Grade Flid Down an Inclined Plane A. Sadighi, D.D. Ganji,. Sabzehmeidani

More information

Conditions for Approaching the Origin without Intersecting the x-axis in the Liénard Plane

Conditions for Approaching the Origin without Intersecting the x-axis in the Liénard Plane Filomat 3:2 (27), 376 377 https://doi.org/.2298/fil7276a Pblished by Faclty of Sciences and Mathematics, University of Niš, Serbia Available at: http://www.pmf.ni.ac.rs/filomat Conditions for Approaching

More information

Two Phase Flow Analysis in Electro-Chemical Machining using CFD

Two Phase Flow Analysis in Electro-Chemical Machining using CFD Two Phase Flow Analysis in Electro-Chemical Machining sing CFD 1 Usharani Rath, 2 Chandan Kmar Biswas 1,2 Department of Mechanical Engineering, National Institte of Technology, Rorkela, 769008, India e-mail:

More information

STEP Support Programme. STEP III Hyperbolic Functions: Solutions

STEP Support Programme. STEP III Hyperbolic Functions: Solutions STEP Spport Programme STEP III Hyperbolic Fnctions: Soltions Start by sing the sbstittion t cosh x. This gives: sinh x cosh a cosh x cosh a sinh x t sinh x dt t dt t + ln t ln t + ln cosh a ln ln cosh

More information

7. Basics of Turbulent Flow Figure 1.

7. Basics of Turbulent Flow Figure 1. 1 7. Basics of Turbulent Flow Whether a flow is laminar or turbulent depends of the relative importance of fluid friction (viscosity) and flow inertia. The ratio of inertial to viscous forces is the Reynolds

More information

Non-contact flood discharge measurements using an X-band pulse radar (I) theory

Non-contact flood discharge measurements using an X-band pulse radar (I) theory Flow Measrement and Instrmentation 13 (00) 65 70 www.elsevier.com/locate/flowmeasinst Non-contact flood discharge measrements sing an X-band plse radar (I) theory Ming-Ching Lee a,, Chan-Ji Lai a, Jan-Mo

More information

Setting The K Value And Polarization Mode Of The Delta Undulator

Setting The K Value And Polarization Mode Of The Delta Undulator LCLS-TN-4- Setting The Vale And Polarization Mode Of The Delta Undlator Zachary Wolf, Heinz-Dieter Nhn SLAC September 4, 04 Abstract This note provides the details for setting the longitdinal positions

More information

EE2 Mathematics : Functions of Multiple Variables

EE2 Mathematics : Functions of Multiple Variables EE2 Mathematics : Fnctions of Mltiple Variables http://www2.imperial.ac.k/ nsjones These notes are not identical word-for-word with m lectres which will be gien on the blackboard. Some of these notes ma

More information

Vibrational modes of a rotating string

Vibrational modes of a rotating string Vibrational modes of a rotating string Theodore J. Allen Department of Physics, University of Wisconsin-Madison, 1150 University Avene, Madison, WI 53706 USA and Department of Physics, Eaton Hall Hobart

More information

CHAPTER 8 CONVECTION IN EXTERNAL TURBULENT FLOW

CHAPTER 8 CONVECTION IN EXTERNAL TURBULENT FLOW CHAPTER 8 CONVECTION IN EXTERNAL TURBULENT FLOW 8.1 Introdction Common phsical phenomenon, bt comple Still relies on empirical data and rdimentar conceptal drawings Tremendos growth in research over last

More information

ON THE SHAPES OF BILATERAL GAMMA DENSITIES

ON THE SHAPES OF BILATERAL GAMMA DENSITIES ON THE SHAPES OF BILATERAL GAMMA DENSITIES UWE KÜCHLER, STEFAN TAPPE Abstract. We investigate the for parameter family of bilateral Gamma distribtions. The goal of this paper is to provide a thorogh treatment

More information

Reduction of over-determined systems of differential equations

Reduction of over-determined systems of differential equations Redction of oer-determined systems of differential eqations Maim Zaytse 1) 1, ) and Vyachesla Akkerman 1) Nclear Safety Institte, Rssian Academy of Sciences, Moscow, 115191 Rssia ) Department of Mechanical

More information

Theoretical Fluid Mechanics Turbulent Flow Velocity Profile By James C.Y. Guo, Professor and P.E. Civil Engineering, U. of Colorado at Denver

Theoretical Fluid Mechanics Turbulent Flow Velocity Profile By James C.Y. Guo, Professor and P.E. Civil Engineering, U. of Colorado at Denver Theoretical Flid Mechanics Trblent Flow Velocit Proile B Jaes C.Y. Go, Proessor and P.E. Civil Engineering, U. o Colorado at Denver 1. Concept o Mixing Process in Trblent Flow Far awa ro the solid wall,

More information

Incompressible Viscoelastic Flow of a Generalised Oldroyed-B Fluid through Porous Medium between Two Infinite Parallel Plates in a Rotating System

Incompressible Viscoelastic Flow of a Generalised Oldroyed-B Fluid through Porous Medium between Two Infinite Parallel Plates in a Rotating System International Jornal of Compter Applications (97 8887) Volme 79 No., October Incompressible Viscoelastic Flow of a Generalised Oldroed-B Flid throgh Poros Medim between Two Infinite Parallel Plates in

More information

Turbulence is a ubiquitous phenomenon in environmental fluid mechanics that dramatically affects flow structure and mixing.

Turbulence is a ubiquitous phenomenon in environmental fluid mechanics that dramatically affects flow structure and mixing. Turbulence is a ubiquitous phenomenon in environmental fluid mechanics that dramatically affects flow structure and mixing. Thus, it is very important to form both a conceptual understanding and a quantitative

More information

Active Flux Schemes for Advection Diffusion

Active Flux Schemes for Advection Diffusion AIAA Aviation - Jne, Dallas, TX nd AIAA Comptational Flid Dynamics Conference AIAA - Active Fl Schemes for Advection Diffsion Hiroaki Nishikawa National Institte of Aerospace, Hampton, VA 3, USA Downloaded

More information

Microscale physics of fluid flows

Microscale physics of fluid flows Microscale physics of flid flows By Nishanth Dongari Senior Undergradate Department of Mechanical Engineering Indian Institte of Technology, Bombay Spervised by Dr. Sman Chakraborty Ot line What is microflidics

More information

Homework 5 Solutions

Homework 5 Solutions Q Homework Soltions We know that the colmn space is the same as span{a & a ( a * } bt we want the basis Ths we need to make a & a ( a * linearly independent So in each of the following problems we row

More information

1 Undiscounted Problem (Deterministic)

1 Undiscounted Problem (Deterministic) Lectre 9: Linear Qadratic Control Problems 1 Undisconted Problem (Deterministic) Choose ( t ) 0 to Minimize (x trx t + tq t ) t=0 sbject to x t+1 = Ax t + B t, x 0 given. x t is an n-vector state, t a

More information

A Survey of the Implementation of Numerical Schemes for Linear Advection Equation

A Survey of the Implementation of Numerical Schemes for Linear Advection Equation Advances in Pre Mathematics, 4, 4, 467-479 Pblished Online Agst 4 in SciRes. http://www.scirp.org/jornal/apm http://dx.doi.org/.436/apm.4.485 A Srvey of the Implementation of Nmerical Schemes for Linear

More information

Frequency Estimation, Multiple Stationary Nonsinusoidal Resonances With Trend 1

Frequency Estimation, Multiple Stationary Nonsinusoidal Resonances With Trend 1 Freqency Estimation, Mltiple Stationary Nonsinsoidal Resonances With Trend 1 G. Larry Bretthorst Department of Chemistry, Washington University, St. Lois MO 6313 Abstract. In this paper, we address the

More information

Fundamentals of magnetohydrodynamics

Fundamentals of magnetohydrodynamics Fndamentals of magnetohydrodynamics Part II Daniel Gómez 1, Email: dgomez@df.ba.ar Webpage: astro.df.ba.ar (1 Institto de Astronomía y Física del Espacio, CONICET, Argentina ( Departamento de Física, Universidad

More information