The Detection of Journal Bearing Cavitation with Use of Ultrasound

Total Page:16

File Type:pdf, Size:1020Kb

The Detection of Journal Bearing Cavitation with Use of Ultrasound THE DETECTION OF JOURNAL BEARING CAVITATION WITH USE OF ULTRASOUND TECHNOLOGY By GREGORIO MIRANDA Submitted in Partial Fulfillment of the Requirements for the Degree of Master of Science Department of Mechanical Engineering CASE WESTERN RESERVE UNIVERSITY May 2016 CASE WESTERN RESERVE UNIVERSITY SCHOOL OF GRADUATE STUDIES We hereby approve the thesis of Gregorio Miranda Candidate for the degree of Master of Science Committee Chair Dr. Joseph M. Prahl Committee Member Dr. Paul Barnhart Committee Member Dr. Roger D. Quinn Date of Defense April 4, 2016 We also certify that written approval has been obtained for any proprietary material contained therein. ii TABLE OF CONTENTS TABLE OF CONTENTS……………………………………………………………………....III LIST OF TABLES…………………………………………………………………………….....V LIST OF FIGURES…………………………………………………………………………….VI ABBREVIATIONS…………………………………………………………………………….IX LIST OF SYMBOLS…………………………………………………………………………….X ACKNOWLEDGEMENTS……………………………………………………………….....XIV ABSTRACT…..………………………………………………………………………………..XV CHAPTER I. INTRODUCTION…………………………………………………………………...1 II. REVIEW OF LITERATURE……………………………………………………….6 2.1 CAVITATION, THE PHYSICAL PHENOMENA……………………………….6 2.1.1 Definition…………………………………………………………………………..6 2.1.2 Vapor Pressure …………………………………………………………………...7 2.1.3 Main Forms of Vapor Cavities ……………………………………………...…..9 2.2 PHASE CHANGE, NUCLEATION, & CAVITATION…………………………14 2.2.1 Liquid State……………………………………………………………………....14 2.2.2 Tensile Strength …………………………………………………………………15 2.2.3 Cavitation & Boiling……………………………………………………………16 2.2.4 Nucleation……………………………………………………………………..…17 2.2.5 Cavitation Number………………………………………………………………19 2.2.6 Inception of Cavitation………………………………………………………….20 2.3 CAVITATION IN LIQUID FLOWS…………………………………………….22 2.3.1 Cavitation Regimes……………………………………………………………...22 2.3.2 Favorable Situations that Yield Cavitation…………………………………..23 2.3.3 Effects of Cavitation…………………………………………………………….24 2.3.4 Existence in Automotive Plain Bearings……………………………………..25 2.4 HYDRODYNAMIC BEARINGS……………………………………………….26 2.4.1 Introduction……………………………………………………………………...26 2.4.2 Definition of Terms……………………………………………………………...26 2.4.3 Fundamental Theory of Operation……………………………………………28 2.4.4 Cavitation in Journal Bearings………………………………………………..36 iii III. NUMERICAL SETUP & PROCEDURES………………………………………..39 3.1 INTRODUCTION…………………………………………………………….....39 3.2 DERIVATION OF REYNOLDS EQUATION………………………………….39 3.2.1 Reynolds Equation……………………………………………………………....39 3.2.2 Cavitation Model………………………………………………………………..44 3.3 NUMERICAL IMPLEMENTATION & DISCRETIZATION…………………..47 3.4 PREDICTED CAVITATION REGION IN BEARING DESIGN……………….53 IV. EXPERIMENTAL SETUP & PROCEDURES………………...…………………54 4.1 INTRODUCTION…………………………...…………………………………..54 4.2 JOURNAL BEARING TEST BENCH DESIGN………………………………...55 4.2.1 Bearing Design…………………………………………………………………..55 4.2.2 Overview of Test Apparatus……………………………………………………58 4.2.3 Bearing Load Application.……………………………………………...……...61 4.2.4 Lubrication System…………………………………………………...…………62 4.2.5 Data Acquisition & Control……………………………………………………64 4.3 APPLICATION OF ULTRASOUND TECHNOLOGY…………………...……65 4.3.1 Introduction…………………………………………………………………...…65 4.3.2 Theory of Operation……………....………………………………………….…66 4.3.3 Setup & Application………………………………………………………….….69 4.3.4 Data Acquisition and Signal Processing……………………………………..70 4.3.5 Pulsing Settings………………………………………………………………….72 4.3.6 Testing Procedure……………………………………………………………….72 V. RESULTS………………………………………………………………..…………79 5.1 INTRODUCTION……………………………………………...………………..79 5.2 EXPERIMENTAL RESULTS…………………………………………………...79 VI. CONCLUSIONS & RECOMMENDATIONS………………………………..…..87 APPENDICES………………………………...………………………………………………...92 APPENDIX A………………………………………………………………………...…………93 APPENDIX B……………………………………………………………………………...…..105 APPENDIX C………………………………………………………………………………….109 APPENDIX D……………………………………………………………………………...…..116 BIBLIOGRAPHY…………………………………………………………………………......125 iv LIST OF TABLES Table 2.1 Formulae for determining pressurized lubricant flow in typical lubricant feed designs [7][10]…………………………………………………………………………………………………….…34 Table 3.1 Reynolds simplifying assumptions……………………………………………………….…..40 Table 3.2 Source code inputs……………………………………………………………………………..53 Table 3.3 Source code outputs…………………………………………………………………….……..53 Table 4.1 Bearing housing and journal design geometries……………………………………….….55 Table 4.2 Bearing housing and journal surface finish, material, and material hardness specifications…………………………………………………………………………………………….....56 Table 4.3 Test bench recorded and controlled parameters…………………………………….…….64 Table 4.4 Tribosonics Ltd UPR pulsing configuration…………………………………………….….72 Table 4.5 Test lubricant specifications…………………………………………………………….……76 Table 4.6a Summary of test bench ultrasound data captures (Tests 1-49)………………………....77 Table 4.6b Summary of test bench ultrasound data captures (Tests 49-96)…………………….….78 Table 5.1 Ultrasound DAC channel gain and offset values for RMS voltage determination…………………………………………………………………………………………….…80 v LIST OF FIGURES Figure 2.1 Pressure vs. Temperature Phase Diagram [1]……………………………………………..8 Figure 2.2 Numerical results from Herring and Gilmore’s incompressible analysis; relative cavity Mach number to bubble relative radius [2]…………………………………………………….11 Figure 2.3 Hickling and Plesset pressure distribution before and after cavity collapse [2]………………………………………………………………………………………………………….…12 Figure 2.4 Plesset and Chapman numerical results for bubble collapse velocities near wall [2]…………………………………………………………………………………………………………….13 Figure 2.5 Typical phase diagram [2]……………………………………………………….………….14 Figure 2.6 Modes of heterogeneous nucleation [2]………………………………………….………..19 Figure 2.7 Hydrodynamic bearing………………………………………….…………………….……..27 Figure 2.8 Illustration of the Three Lubrication Regimes [8]………………………………….…....29 Figure 2.9 Principle of hydrodynamic pressure generation between non-parallel surfaces [7]………………………………………………………………………………………………………….…30 Figure 2.10 Load components and pressure field generation in a journal bearing [7]……………………………………………………………………………………………………...…….31 Figure 2.11 Typical lubricant delivery designs [7][10]………………………………………….…..32 Figure 2.12 Table for determining parameters 푓1 and 푓2 for pressurized rectangular lubricant feed grooves [7][10]……………………………………………………………………………………....35 Figure 3.1 Definition of Cartesian coordinates in bearing application……………………….……41 Figure 3.2 Unwrapped bearing subdomain grid point structure………………………………….…48 Figure 3.3 Grid point cluster for unwrapped bearing subdomain grid structure………………....49 Figure 3.4 Pressure distribution for unwrapped hydrodynamic bearing…...……………………...54 Figure 4.1 Fabricated bearing housing……………………………………………………….……..…57 Figure 4.2 Fabricated translucent bearing housing………………………………………….……….58 Figure 4.3 Orthographic rendering of hydrodynamic bearing test bench……………………….…59 Figure 4.4 Rendering of hydrodynamic bearing test bench……………………………………….….59 Figure 4.5 Hydrodynamic bearing test bench…………………………………………………….……60 vi Figure 4.6 Hydrodynamic bearing test bench housing……………………………………….……….61 Figure 4.7 Static load application via pulley and hanging weights………...………………………62 Figure 4.8 Hydrodynamic bearing test bench lubrication system schematic………………………63 Figure 4.9 Sending and receiving ultrasound signals through bearing material………………….67 Figure 4.10 Instrumented bearing housing with ultrasound sensor………………………………...68 Figure 4.11 Final instrumented bearing housing……………………………...………………….…..68 Figure 4.12 Schematic of cavitation detection system…………………………………………….…..70 Figure 4.13 Typical acquired ultrasound signal……………………………………………………....71 Figure 4.14 Measurement of converging and diverging bearing operation with single housing and ultrasound sensor combination……………………………………………………………………..73 Figure 4.15 Journal bearing operation with ultrasound sensor positioned in the diverging region………………………………………………………………………………………………………..74 Figure 4.16 Journal bearing operation with ultrasound sensor positioned in the converging region………………………………………………………………………………………………………..75 Figure 5.1 Measured ultrasound binary raw RMS value standard deviation by measurement region; Converging vs. Diverging ………………..…………………………………………………..…80 Figure 5.2 Measured ultrasound average binary RMS value by region; Converging vs. Diverging……………………………………………………………………………...…………………….81 Figure 5.3 Measured ultrasound average binary RMS value vs. bearing/sensor temperature………………………………………………………………………..…………………….….82 Figure 5.4 Measured ultrasound binary RMS value standard deviation vs. lubricant feed pressure………………………………………………………..…………………………………………….83 Figure 5.5 Measured ultrasound binary RMS value standard deviation vs. lubricant inlet temperature…………………………………………………………………………………………...…….84 Figure 5.6 Measured ultrasound average binary RMS value vs. lubricant feed pressure…………………………………………………………………………………….………….…….85 Figure 5.7 Measured ultrasound average binary RMS value vs. lubricant feed temperature………………………………………………………...……………………………………….86 Figure A-1 Cartesian coordinate system for derivation of Reynolds equation…………………….94 Figure A-2 Equilibrium of single control element in fluid film in x-direction…………………......95 vii Figure A-3 Equilibrium of single control element in fluid film in y-direction...…………………...99 viii ABBREVIATIONS VM Viscosity Modifier PIB Polyisobutylene PMA Polymethacrylate OCP Olefin Copolymer SEMACP Esters of Styrene Maleic Anhydride Copolymer HSDCP Hydrogenated Styrene-diene Copolymer STAR Hydrogenated Radial Polyisoprene OEM Original Equipment Manufacturer UPR Ultrasound Pulser/Reciever
Recommended publications
  • The Role of MHD Turbulence in Magnetic Self-Excitation in The
    THE ROLE OF MHD TURBULENCE IN MAGNETIC SELF-EXCITATION: A STUDY OF THE MADISON DYNAMO EXPERIMENT by Mark D. Nornberg A dissertation submitted in partial fulfillment of the requirements for the degree of Doctor of Philosophy (Physics) at the UNIVERSITY OF WISCONSIN–MADISON 2006 °c Copyright by Mark D. Nornberg 2006 All Rights Reserved i For my parents who supported me throughout college and for my wife who supported me throughout graduate school. The rest of my life I dedicate to my daughter Margaret. ii ACKNOWLEDGMENTS I would like to thank my adviser Cary Forest for his guidance and support in the completion of this dissertation. His high expectations and persistence helped drive the work presented in this thesis. I am indebted to him for the many opportunities he provided me to connect with the world-wide dynamo community. I would also like to thank Roch Kendrick for leading the design, construction, and operation of the experiment. He taught me how to do science using nothing but duct tape, Sharpies, and Scotch-Brite. He also raised my appreciation for the artistry of engineer- ing. My thanks also go to the many undergraduate students who assisted in the construction of the experiment, especially Craig Jacobson who performed graduate-level work. My research partner, Erik Spence, deserves particular thanks for his tireless efforts in modeling the experiment. His persnickety emendations were especially appreciated as we entered the publi- cation stage of the experiment. The conversations during our morning commute to the lab will be sorely missed. I never imagined forging such a strong friendship with a colleague, and I hope our families remain close despite great distance.
    [Show full text]
  • Friction Loss Along a Pipe
    FRICTION LOSS ALONG A PIPE 1. INTRODUCTION The frictional resistance to which fluid is subjected as it flows along a pipe results in a continuous loss of energy or total head of the fluid. Fig 1 illustrates this in a simple case; the difference in levels between piezometers A and B represents the total head loss h in the length of pipe l. In hydraulic engineering it is customary to refer to the rate of loss of total head along the pipe, dh/dl, by the term hydraulic gradient, denoted by the symbol i, so that 푑ℎ = 푑푙 Fig 1 Diagram illustrating the hydraulic gradient Osborne Reynolds, in 1883, recorded a number of experiments to determine the laws of resistance in pipes. By introducing a filament of dye into the flow of water along a glass pipe he showed the existence of two different types of motion. At low velocities the filament appeared as a straight line which passed down the whole length of the tube, indicating laminar flow. At higher velocities, the filament, after passing a little way along the tube, suddenly mixed with the surrounding water, indicating that the motion had now become turbulent. 1 Experiments with pipes of different and with water at different temperatures led Reynolds to conclude that the parameter which determines whether the flow shall be laminar or turbulent in any particular case is 휌푣퐷 푅 = 휇 In which R denotes the Reynolds Number of the motion 휌 denotes the density of the fluid v denotes the velocity of flow D denotes the diameter of the pipe 휇 denotes the coefficient of viscosity of the fluid.
    [Show full text]
  • Chapter 5 Dimensional Analysis and Similarity
    Chapter 5 Dimensional Analysis and Similarity Motivation. In this chapter we discuss the planning, presentation, and interpretation of experimental data. We shall try to convince you that such data are best presented in dimensionless form. Experiments which might result in tables of output, or even mul- tiple volumes of tables, might be reduced to a single set of curves—or even a single curve—when suitably nondimensionalized. The technique for doing this is dimensional analysis. Chapter 3 presented gross control-volume balances of mass, momentum, and en- ergy which led to estimates of global parameters: mass flow, force, torque, total heat transfer. Chapter 4 presented infinitesimal balances which led to the basic partial dif- ferential equations of fluid flow and some particular solutions. These two chapters cov- ered analytical techniques, which are limited to fairly simple geometries and well- defined boundary conditions. Probably one-third of fluid-flow problems can be attacked in this analytical or theoretical manner. The other two-thirds of all fluid problems are too complex, both geometrically and physically, to be solved analytically. They must be tested by experiment. Their behav- ior is reported as experimental data. Such data are much more useful if they are ex- pressed in compact, economic form. Graphs are especially useful, since tabulated data cannot be absorbed, nor can the trends and rates of change be observed, by most en- gineering eyes. These are the motivations for dimensional analysis. The technique is traditional in fluid mechanics and is useful in all engineering and physical sciences, with notable uses also seen in the biological and social sciences.
    [Show full text]
  • Cavitation in Valves
    VM‐CAV/WP White Paper Cavitation in Valves Table of Contents Introduction. 2 Cavitation Analysis. 2 Cavitation Data. 3 Valve Coefficient Data. 4 Example Application. .. 5 Conclusion & Recommendations . 5 References. 6 Val‐Matic Valve & Mfg. Corp. • www.valmatic.com • [email protected] • PH: 630‐941‐7600 Copyright © 2018 Val‐Matic Valve & Mfg. Corp. Cavitation in Valves INTRODUCTION Cavitation can occur in valves when used in throttling or modulating service. Cavitation is the sudden vaporization and violent condensation of a liquid downstream of the valve due to localized low pressure zones. When flow passes through a throttled valve, a localized low pressure zone forms immediately downstream of the valve. If the localized pressure falls below the vapor pressure of the fluid, the liquid vaporizes (boils) and forms a vapor pocket. As the vapor bubbles flow downstream, the pressure recovers, and the bubbles violently implode causing a popping or rumbling sound similar to tumbling rocks in a pipe. The sound of cavitation in a pipeline is unmistakable. The condensation of the bubbles not only produces a ringing sound, but also creates localized stresses in the pipe walls and valve body that can cause severe pitting. FIGURE 1. Cavitation Cavitation is a common occurrence in shutoff valves during the last few degrees of closure when the supply pressure is greater than about 100 psig. Valves can withstand limited durations of cavitation, but when the valve must be throttled or modulated in cavitating conditions for long periods of time, the life of the valve can be drastically reduced. Therefore, an analysis of flow conditions is needed when a valve is used for flow or pressure control.
    [Show full text]
  • Control Valve Sizing Theory, Cavitation, Flashing Noise, Flashing and Cavitation Valve Pressure Recovery Factor
    Control Valve Sizing Theory, Cavitation, Flashing Noise, Flashing and Cavitation Valve Pressure Recovery Factor When a fluid passes through the valve orifice there is a marked increase in velocity. Velocity reaches a maximum and pressure a minimum at the smallest sectional flow area just downstream of the orifice opening. This point of maximum velocity is called the Vena Contracta. Downstream of the Vena Contracta the fluid velocity decelerates and the pressure increases of recovers. The more stream lined valve body designs like butterfly and ball valves exhibit a high degree of pressure recovery where as Globe style valves exhibit a lower degree of pressure recovery because of the Globe geometry the velocity is lower through the vena Contracta. The Valve Pressure Recovery Factor is used to quantify this maximum velocity at the vena Contracta and is derived by testing and published by control valve manufacturers. The Higher the Valve Pressure Recovery Factor number the lower the downstream recovery, so globe style valves have high recovery factors. ISA uses FL to represent the Valve Recovery Factor is valve sizing equations. Flow Through a restriction • As fluid flows through a restriction, the Restriction Vena Contracta fluid’s velocity increases. Flow • The Bernoulli Principle P1 P2 states that as the velocity of a fluid or gas increases, its pressure decreases. Velocity Profile • The Vena Contracta is the point of smallest flow area, highest velocity, and Pressure Profile lowest pressure. Terminology Vapor Pressure Pv The vapor pressure of a fluid is the pressure at which the fluid is in thermodynamic equilibrium with its condensed state.
    [Show full text]
  • Cavitation Experimental Investigation of Cavitation Regimes in a Converging-Diverging Nozzle Willian Hogendoorn
    Cavitation Experimental investigation of cavitation regimes in a converging-diverging nozzle Willian Hogendoorn Technische Universiteit Delft Draft Cavitation Experimental investigation of cavitation regimes in a converging-diverging nozzle by Willian Hogendoorn to obtain the degree of Master of Science at the Delft University of Technology, to be defended publicly on Wednesday May 3, 2017 at 14:00. Student number: 4223616 P&E report number: 2817 Project duration: September 6, 2016 – May 3, 2017 Thesis committee: Prof. dr. ir. C. Poelma, TU Delft, supervisor Prof. dr. ir. T. van Terwisga, MARIN Dr. R. Delfos, TU Delft MSc. S. Jahangir, TU Delft, daily supervisor An electronic version of this thesis is available at http://repository.tudelft.nl/. Contents Preface v Abstract vii Nomenclature ix 1 Introduction and outline 1 1.1 Introduction of main research themes . 1 1.2 Outline of report . 1 2 Literature study and theoretical background 3 2.1 Introduction to cavitation . 3 2.2 Relevant fluid parameters . 5 2.3 Current state of the art . 8 3 Experimental setup 13 3.1 Experimental apparatus . 13 3.2 Venturi. 15 3.3 Highspeed imaging . 16 3.4 Centrifugal pump . 17 4 Experimental procedure 19 4.1 Venturi calibration . 19 4.2 Camera settings . 21 4.3 Systematic data recording . 21 5 Data and data processing 23 5.1 Videodata . 23 5.2 LabView data . 28 6 Results and Discussion 29 6.1 Analysis of starting cloud cavitation shedding. 29 6.2 Flow blockage through cavity formation . 30 6.3 Cavity shedding frequency . 32 6.4 Cavitation dynamics . 34 6.5 Re-entrant jet dynamics .
    [Show full text]
  • Philosophical Transactions
    L « i 1 INDEX TO THE PHILOSOPHICAL TRANSACTIONS, S e r ie s A, FOR THE YEAR 1897 (YOL. 190). A. A b n e y (W. d e W.). The Sensitiveness of the Retina to Light and Colour, 155. iEther in relation to Contained Matter; Constitution o f; mechanical Models of; Radiation across Moving Matter mechanical Reaction of Radiation; Theory of Diamagnetism, &c. (L ar m o r ), 205. B. B xI d e n -P o w ell (Sir G e o r g e ). Total Eclipse of the Sun, 1896.—The Novaya Zemlya Observations, 197. Bakerian Lecture. See R e y n o l d s and Mo o r by . Barometer—Self-recording Frequency-Barometer, by G. U. Yule (P earson and Le e ), 423. Barometric Heights, Frequency-distribution of, at 23 Stations in British Isles ; Correlation of ; Prediction Formulae (Pearson and Lee), 423. Boomerangs, Account of; Air-pressure on ; Trajectories of (W alk er ), 23. C. Cathode Rays, various Kinds ; Electrostatic Deflexion ; Splash Phenomena (T h o m pso n ), 471. Colour, Sensitiveness of Retina to; Extinction dependent on Angular Aperture of Image; Relation of Colour Fields to Intensity of Colour (A b n e y ), 153. Contact Action, Molecular Theory of ; Forcives divided into Molecular and Mechanical; Electric and Magnetic Stresses ; Electrostriction and Magnetostriction (Larmor), 205. Corona, Note by W. H. W e sl e y on Photographs of, obtained in Novaya Zemlya Eclipse of 1890 (B a d e n -P o w e l l ), 197. Cr o o k e s’ Tubes, Dendritic Forms of Luminescence in (T h o m pso n ), 471.
    [Show full text]
  • Eulerian–Lagrangian Method for Simulation of Cloud Cavitation ∗ Kazuki Maeda , Tim Colonius
    Journal of Computational Physics 371 (2018) 994–1017 Contents lists available at ScienceDirect Journal of Computational Physics www.elsevier.com/locate/jcp Eulerian–Lagrangian method for simulation of cloud cavitation ∗ Kazuki Maeda , Tim Colonius Division of Engineering and Applied Science, California Institute of Technology, 1200 East California Boulevard, Pasadena, CA 91125, USA a r t i c l e i n f o a b s t r a c t Article history: We present a coupled Eulerian–Lagrangian method to simulate cloud cavitation in a Received 3 December 2017 compressible liquid. The method is designed to capture the strong, volumetric oscillations Received in revised form 10 April 2018 of each bubble and the bubble-scattered acoustics. The dynamics of the bubbly mixture Accepted 16 May 2018 is formulated using volume-averaged equations of motion. The continuous phase is Available online 18 May 2018 discretized on an Eulerian grid and integrated using a high-order, finite-volume weighted Keywords: essentially non-oscillatory (WENO) scheme, while the gas phase is modeled as spherical, Bubble dynamics Lagrangian point-bubbles at the sub-grid scale, each of whose radial evolution is tracked Cavitation by solving the Keller–Miksis equation. The volume of bubbles is mapped onto the Eulerian Eulerian–Lagrangian method grid as the void fraction by using a regularization (smearing) kernel. In the most general Compressible multiphase flows case, where the bubble distribution is arbitrary, three-dimensional Cartesian grids are used Multiscale modeling for spatial discretization. In order to reduce the computational cost for problems possessing Reduced-order modeling translational or rotational homogeneities, we spatially average the governing equations along the direction of symmetry and discretize the continuous phase on two-dimensional or axi-symmetric grids, respectively.
    [Show full text]
  • A Numerical Algorithm for MHD of Free Surface Flows at Low Magnetic Reynolds Numbers
    A Numerical Algorithm for MHD of Free Surface Flows at Low Magnetic Reynolds Numbers Roman Samulyak1, Jian Du2, James Glimm1;2, Zhiliang Xu1 1Computational Science Center, Brookhaven National Laboratory, Upton, NY 11973 2 Department of Applied Mathematics and Statistics, SUNY at Stony Brook, Stony Brook, NY 11794, USA November 7, 2005 Abstract We have developed a numerical algorithm and computational soft- ware for the study of magnetohydrodynamics (MHD) of free surface flows at low magnetic Reynolds numbers. The governing system of equations is a coupled hyperbolic/elliptic system in moving and ge- ometrically complex domains. The numerical algorithm employs the method of front tracking for material interfaces, high resolution hy- perbolic solvers, and the embedded boundary method for the elliptic problem in complex domains. The numerical algorithm has been imple- mented as an MHD extension of FronTier, a hydrodynamic code with free interface support. The code is applicable for numerical simulations of free surface conductive liquids or flows of weakly ionized plasmas. Numerical simulations of the Muon Collider/Neutrino Factory target have been discussed. 1 Introduction Computational magnetohydrodynamics, greatly inspired over the last decades by the magnetic confinement fusion and astrophysics problems, has achieved significant results. However the major research effort has been in the area of highly ionized plasmas. Numerical methods and computational software for MHD of weakly conducting materials such as liquid metals or weakly ionized plasmas have not been developed to such an extent despite the need 1 for fusion research and industrial technologies. Liquid metal MHD, driven by potential applications of flowing liquid metals or electrically conducting liquid salts as coolant in magnetic confinement fusion reactors as well as some industrial problems, has attracted broad theoretical, computational, and experimental studies (see [16, 17, 18] and references therein).
    [Show full text]
  • Toward a Self-Generating Magnetic Dynamo: the Role of Turbulence
    PHYSICAL REVIEW E VOLUME 61, NUMBER 5 MAY 2000 Toward a self-generating magnetic dynamo: The role of turbulence Nicholas L. Peffley, A. B. Cawthorne, and Daniel P. Lathrop* Department of Physics, University of Maryland, College Park, Maryland 20742 ͑Received 6 July 1999͒ Turbulent flow of liquid sodium is driven toward the transition to self-generating magnetic fields. The approach toward the transition is monitored with decay measurements of pulsed magnetic fields. These mea- surements show significant fluctuations due to the underlying turbulent fluid flow field. This paper presents experimental characterizations of the fluctuations in the decay rates and induced magnetic fields. These fluc- tuations imply that the transition to self-generation, which should occur at larger magnetic Reynolds number, will exhibit intermittent bursts of magnetic fields. PACS number͑s͒: 47.27.Ϫi, 47.65.ϩa, 05.45.Ϫa, 91.25.Cw I. INTRODUCTION Reynolds number will be quite large for all flows attempting to self-generate ͑where Re ӷ1 yields Reӷ105)—implying The generation of magnetic fields from flowing liquid m turbulent flow. These turbulent flows will cause the transition metals is being pursued by a number of scientific research to self-generation to be intermittent, showing both growth groups in Europe and North America. Nuclear engineering and decay of magnetic fields irregularly in space and time. has facilitated the safe use of liquid sodium, which has con- This intermittency is not something addressed by kinematic tributed to this new generation of experiments. With the dynamo studies. The analysis in this paper focuses on three highest electrical conductivity of any liquid, sodium retains main points: we quantify the approach to self-generation and distorts magnetic fields maximally before they diffuse with increasing Rem , characterize the turbulence of induced away.
    [Show full text]
  • Numerical Study of Cavitation Within Orifice Flow
    NUMERICAL STUDY OF CAVITATION WITHIN ORIFICE FLOW A Thesis by PENGZE YANG Submitted to the Office of Graduate and Professional Studies of Texas A&M University in partial fulfillment of the requirements for the degree of MASTER OF SCIENCE Chair of Committee, Robert Handler Committee Members, David Staack Prabir Daripa Head of Department, Andreas Polycarpou December 2015 Major Subject: Mechanical Engineering Copyright 2015 Pengze Yang ABSTRACT Cavitation generally occurs when the pressure at certain location drops to the vapor pressure and the liquid water evaporates as a consequence. For the past several decades, numerous experimental researches have been conducted to investigate this phenomenon due to its degradation effects on hydraulic device structures, such as erosion, noise and vibration. A plate orifice is an important restriction device that is widely used in many industries. It serves functions as restricting flow and measuring flow rate within a pipe. The plate orifice is also subject to intense cavitation at high pressure difference, therefore, the simulation research of the cavitation phenomenon within an orifice flow becomes quite essential for understanding the causes of cavitation and searching for possible preventing methods. In this paper, all researches are simulation-oriented by using ANSYS FLUENT due to its high resolution comparing to experiments. Standard orifice plates based on ASME PTC 19.5-2004 are chosen and modeled in the study with the diameter ratio from 0.2 to 0.75. Steady state studies are conducted for each diameter ratio at the cavitation number roughly from 0.2 to 2.5 to investigate the dependency of discharge coefficient on the cavitation number.
    [Show full text]
  • Osborne Reynolds Apparatus
    fluid mechanics H215 Osborne Reynolds Apparatus Free-standing apparatus that gives a visual demonstration of laminar and turbulent flow. It also allows students to investigate the effect of varying viscosity and investigate Reynolds numbers. Optional Heater Module (H215a) Key features • Constant head reservoir and flow-smoothing parts for a smooth flow • Uses dye injector system to show flow patterns • Investigates Reynolds number at transition • Clear tube and light-coloured shroud to help flow visualisation (see flow more clearly) • Shows turbulent and laminar flow • Optional heater module available for tests at different viscosities • Ideal for classroom demonstrations and student experiments TecQuipment Ltd, Bonsall Street, long eaton, Nottingham NG10 2AN, UK tecquipment.com +44 115 972 2611 [email protected] PE/DB/BW/1019 Page 1 of 2 H215 Osborne Reynolds Apparatus Description Learning Outcomes The apparatus consists of a precision-bore glass pipe (test • Demonstration of transition between laminar and tube) held vertically in a large shroud. The shroud is open turbulent flow. at the front and the inside surface is light coloured. This • Determination of transition Reynolds numbers and allows the students to see the flow clearly. comparison with accepted values. Water enters a constant head tank (reservoir) above the • Investigation of the effect of varying viscosity and test tube and passes through a diffuser and stilling bed. It demonstration that the Reynolds number at transition is then passes through a specially shaped bell-mouth into independent of viscosity. the test tube. This arrangement ensures a steady, uniform flow at entry to the test tube. A thermometer measures the temperature in the constant head reservoir.
    [Show full text]