Fakhar Title Defence_Final

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    Thesis SupervisorDr. M. Afzaal Malik

    Guidance & Evaluation CommitteeCol Dr. Syed Waheed-ul-Haq

    Lt Col Dr. Aamer Ahmed Baqai

    Mr. Raja Aamir Azim

    MS Student

    Fakhar-e-Alam Khan

    2009-NUST-MSPhD-MECH-12

    http://www.missionislam.com/islamicart/wallpaper/images/bismillah3_jpg_jpg.jpg
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    Sequence Motivation

    Introduction

    Research Plan Knowledge Base

    Literature Survey

    Development of Model/Sub-Models (Mathematical Equations)

    Numerical Scheme

    MATLAB Code Integration of all Sub-Models

    Simulation of Results

    Conclusions

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    Motivation Interest in Thermal Sciences/Internal Combustion

    Engines.

    I am working at a testing lab in a private sector commercial

    organization. To look after Short Circuit Generator especially its

    lubricating oil unit.

    Lubricants make fluid film bearings reduce friction & wear,

    and Provide load capacity.

    That why I was keen to understand the Lubrication theoryof bearings and how heat affects its load carrying capacity.

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    Introduction The piston and top compression ring come into direct

    contact with hot combustion gases.

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    Introduction (Contd) The heat energy in the piston is absorbed by the rings.

    The rings then transfer this heat into the cylinderwalls.

    Approx. 70% of the piston's heat is carried away by thepiston rings, under both unloaded and loaded engine

    operation conditions, at 1,500 and 3,000 rpm.

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    Research Plan

    Knowledge Base

    Literature Survey

    Development of Model/Sub-Models (MathematicalEquations)

    Numerical Scheme

    MATLAB Code

    Integration of all Sub-Models

    Simulation of Results Conclusions

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    Knowledge BaseWhole or part of the following books were studied:

    Fundamentals of Fluid Film Lubricationby Bernard J.Hamrock & Steven R. Schmid

    EngineeringTribologyby Gwidon W. Stachowiak & AndrewW. Batchelor

    Elasto-HydrodynamicLubrication by D.Dowson &

    G.R.Higginson AppliedTribologyby Michael M. Khonsari & E. Richard

    Booser

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    Knowledge Base (Contd) ComputationalFluidDynamics by John D. Anderson, Jr.

    ComputationalHeatTransfer by Yogesh Jaluria & Kenneth E.

    Torrance HeatTransferCalculationsusingFiniteDifferenceEquations

    by David R. Croft & David G. Lilley

    InternalCombustionEngineFundamentals by John B.Heywood

    ComputationalFluidDynamics(Volume)by Klaus A.Hoffmann & Steve T. Chiang

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    Knowledge Base (Contd) Mathematical Statements of Physical processes

    (Differential Forms in Cartesian Coordinates):

    Continuity Equation (Mass is conserved):

    Conservation of Momentum (Momentum isconserved):

    x-Momentum:

    0)()()(

    z

    w

    y

    v

    x

    u

    t

    BxzxyxxxF

    x

    p

    zyxz

    uw

    y

    uv

    x

    uu

    t

    u

    )()(

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    Knowledge Base (Contd) y-Momentum:

    z-Momentum:

    ByzyyyxyF

    y

    p

    zyxz

    vw

    y

    vv

    x

    vu

    t

    v

    )()(

    BzzzyzxzF

    zp

    zyxzww

    ywv

    xwu

    tw

    )()(

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    Knowledge Base(Contd) Energy Equation (Energy is conserved):

    Reynolds's Equation:

    The differential equation governing the pressure distribution in

    fluid film lubrication is known as the Reynolds equation.

    )()()()(

    z

    Tk

    zy

    Tk

    yx

    Tk

    xz

    Tw

    y

    Tv

    x

    Tu

    t

    TCp

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    Knowledge Base (Contd)

    Couette term can further be expanded to:

    expansionlocalsqueezenormal

    squeezegeometric

    sheartoduerateflownetterm:Couette

    gradientspresuretoduerateflownet:termsPoiseuille

    3

    )(])([2

    1

    12 thww

    x

    hUhUU

    x)

    x

    P

    h(

    xabbba

    wedgedensity

    wedgephysicalstretchphysical

    sheartoduerateflownetterm:Couette

    )(2

    1)(2

    1)(2

    1])([2

    1

    xhUU

    x

    hUUUUx

    hhUUx

    babababa

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    Literature Survey Following journals were explored.

    ASME Journal of Engineering for Gas Turbines and Power

    ASME Journal of Heat Transfer

    ASME Journal of Thermal Science and EngineeringApplications

    ASME Journal of Tribology

    SAE Technical Paper Series

    SAGE Journal of Automobile Engineering Proceedings of IMechE

    Elsevier Journal of Applied Thermal Engineering

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    Literature Survey (Contd) Journal of Tribology International

    MIT MS/PhD thesis from dspace.mit.edu/

    Bulletin of The Japan Society of Mechanical Engineers (JSME)

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    Literature Survey (Contd) Yasuo Harigaya, Michiyoshi Suzuki, Fujio Toda, Masaaki Takiguchi,

    Analysis of Oil Film Thickness and Heat Transfer on a Piston Ring of aDiesel Engine: Effect of Lubricant Viscosity, ASME Journal of Engineeringfor Gas Turbines and Power, July 2006, Vol. 128/685.

    Jordan A. Kaplan, Modeling The Spark Ignition Engine Warm-Up ProcessTo Predict Component Temperatures, MS Thesis, MIT, 1990.

    Jordan A. Kaplan and John B. Heywood , Modeling the Spark IgnitionEngine Warm-Up Process to Predict Component Temperatures and

    Hydrocarbon Emissions, SAE paper 910302, 1991.

    V. Esfahanian, A. Javaheri, M. Ghaffarpour, Thermal analysis of an SIengine piston using different combustion boundary condition treatments,Applied Thermal Engineering 26 (2006) 277-287.

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    Literature Survey (Contd) Yong Liu and R. D. Reitz, Modeling of heat conduction within chamber

    walls for multidimensional internal combustion engine simulations, Int. J.Heat & Mass Transfer, Vol. 41, Nos 6-7, pp. 859-869, 1998.

    Ravindra Prasad and N. K. Samria, Transient heat transfer analysis in aninternal combustion engine piston, Computers & Structures Vol. 34, No.5,pp.787-793,1990.

    Toshio TADA, Shoichi Furuhama, On the Heat Flow from the Pistons in a

    Farm Type Gasoline Engine, Bulletin of JSME, 621.434-242:621.434.016.4.

    Toshio TADA, Yoshitane OYA, Piston Temperatures of an AutomobileEngine, Bulletin of JSME, 621.434-242:621.434.016.4.

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    Mathematical Modeling

    Energy Equation in Cylindrical Coordinates:

    Energy Equation in Cylindrical Coordinates is:

    In absence of motion and neglecting the source term , the

    energy equation reduces to the governing equation for heatconduction in Piston Crown and Top Ring.

    )()(

    1)(

    1)(

    2 z

    Tk

    z

    Tk

    rr

    Tkr

    rrz

    Tu

    T

    r

    w

    r

    Tv

    t

    TCp

    )()(1

    )(1

    2z

    Tk

    z

    Tk

    rr

    Tkr

    rrt

    TCp

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    Energy Equation in Cylindrical

    Coordinates (Contd)

    Assuming constant thermal conductivity and

    axisymmetry, the conduction heat equation is:

    )()(

    1

    z

    T

    kzr

    T

    krrrt

    T

    Cp

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    Numerical Scheme Normally Closed form/exact solutions for real world

    engineering problems do not exist.

    Numerical Scheme is used.

    Real world Engineering problems are mostly solved byusing any one of the following numerical schemes:

    Finite Difference Scheme Finite Volume Scheme

    Finite Element Scheme

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    Numerical Scheme (Contd) Finite Difference Scheme will be used.

    Finite Difference Schemes are further classified asExplicit or Implicit Schemes.

    Explicit schemes are easier to implement but these areconditionally stable schemes.

    Implicit schemes are unconditionally stable schemes.

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    Numerical Scheme (Contd) 2-D Parabolic Partial Differential Equations are

    normally solved by Alternating Direction Implicit(ADI) scheme.

    Split the time step into half.

    For the first half, treat one term implicitly while theother explicitly to get the solution by tridiagonal

    algorithm. For the next half, reverse the implicit-explicit

    formulation to again get the solution by tridiagonalalgorithm.

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    Numerical Scheme (Contd) Finite Differencing of 2-D Heat Equation using ADI

    Scheme:

    Let = Thermal Diffusivity

    &

    First Half:

    pC

    k

    2)(

    )(

    r

    trr

    2)(

    )(

    z

    trz

    n

    ji

    n

    ji

    n

    ji

    n

    ji

    n

    ji

    n

    ji Tr

    rrrTrT

    r

    rrrTrTrTr

    rrrrzzz ,1,,1

    1

    1,

    1

    ,

    1

    1, )2

    ()21()2

    ()21(

    Implicitz(j)Explicit,)( ir

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    Numerical Scheme (Contd) Second Half: Explicitz(j)Implicit,)( ir

    1

    1,

    1

    ,

    1

    1,

    2

    ,1

    2

    ,

    2

    ,1 )21()2

    ()21()2

    (

    n

    ji

    n

    ji

    n

    ji

    n

    ji

    n

    ji

    n

    ji TrTrTrTr

    rrrTrT

    r

    rrr

    zzzrrrrr

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    Code Development Normally, simulation of results are obtained by using

    Either Commercial Software

    Writing Own Code in any Programming Language like C,FORTRAN, MATLAB etc

    Due to strong graphics capabilities, the numerical

    programming code is being written in MATLAB.

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    Integration of all sub-models The following equations will be coupled to get the

    overall simulation results:

    2-D Heat Equation in Piston Crown

    1-D Heat Equation in Top Compression Ring

    Convective Heat Transfer in lubricant film

    Reynolds's Equation

    Piston Dynamics Equation

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    Simulation of Results/Conclusions

    Simulation of results will show the effect ofCombustion Heat over the load carrying capacity ofthe top compression ring.

    Conclusions will be drawn from the above simulation

    results.

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    Thank You