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    Heat Transfer

    Training Manual

    Chapter 10

    Heat Transfer

    10-1ANSYS, Inc. Proprietary 2009 ANSYS, Inc. All rights reserved. April 28, 2009Inventory #002598

    10-1ANSYS, Inc. Proprietary 2009 ANSYS, Inc. All rights reserved. April 28, 2009Inventory #002598

    Introduction to CFX

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    Heat Transfer

    Training ManualGoverning Equations

    Continuity

    Momentum

    Conservation Equations

    10-2ANSYS, Inc. Proprietary 2009 ANSYS, Inc. All rights reserved. April 28, 2009Inventory #002598

    Energy

    where

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    Heat Transfer

    Training Manual

    Heat transfer in a fluid domain is governed by the EnergyTransport Equation:

    SourcesViscous workConvectionTransient Conduction

    Governing Equations

    Etottot

    SUThUt

    p

    t

    h

    ++=+

    )()()(

    )(

    10-3ANSYS, Inc. Proprietary 2009 ANSYS, Inc. All rights reserved. April 28, 2009Inventory #002598

    None: Energy Transport Equation not solved

    Isothermal: The Energy Transport Equation is not solved but a temperature isrequired to evaluated fluid properties (e.g. when using an Ideal Gas)

    Thermal Energy: An Energy Transport Equation is solved which neglects variabledensity effects. It is suitable for low speed liquid flow with constant specific heats.An optional viscous dissipation term can be included if viscous heating is significant.

    Total Energy: This models the transport of enthalpy and includes kinetic energyeffects. It should be used for gas flows where the Mach number exceeds 0.2, and

    high speed liquid flows where viscous heating effects arise in the boundary layer,where kinetic energy effects become significant.

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    Heat Transfer

    Training ManualGoverning Equations For multicomponent flows, reacting flows and radiation modeling

    additional terms are included in the energy equation

    Heat transfer in a solid domain is modeled using the followingconduction equation

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    SourceTransient Conduction

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    Heat Transfer

    Training ManualSelecting a Heat Transfer Model The Heat Transfer model is selected

    on the Domain > Fluid Models panel

    Enable the Viscous Workterm(Total Energy), or ViscousDissipationterm (Thermal Energy),

    10-5ANSYS, Inc. Proprietary 2009 ANSYS, Inc. All rights reserved. April 28, 2009Inventory #002598

    if viscous shear in the fluid is large

    (e.g. lubrication or high speedcompressible flows)

    Enable radiation model / submodels

    if radiative heat transfer issignificant

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    Heat Transfer

    Training Manual

    Radiation effects should be accounted for whenis significant compared to

    convective and conductive heat transfer rates

    To account for radiation, Radiative IntensityTransport Equations (RTEs) are solved

    Local absorption by fluid and at boundaries couplesthese RTEs with the energy equation

    Radiation

    )(4

    min

    4

    maxrad TTQ =

    10-6ANSYS, Inc. Proprietary 2009 ANSYS, Inc. All rights reserved. April 28, 2009Inventory #002598

    a at on ntens ty s rect ona y anspatially dependent

    Transport mechanisms for radiation intensity: Local absorption

    Out-scattering (scattering away fromthe direction)

    Local emission

    In-scattering (scattering into the direction)

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    Heat Transfer

    Training Manual

    Several radiation models are available which provide approximate solutions

    to the RTE

    1) Rosseland Model (Diffusion Approximation Model)

    2) P-1 Model (Gibbs Model/Spherical Harmonics Model)

    3) Discrete Transfer Model (DTM) (Shah Model)

    Radiation Models

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    Each radiation model has its assumptions, limitations, and benefits

    on e ar o o e (not available in the ANSYS CFD-Flo product)

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    Heat Transfer

    Training ManualChoosing a Radiation Model The optical thickness should be determined before choosing a

    radiation model

    Optically thin means that the fluid is transparent to the radiation at

    wavelengths where the heat transfer occurs The radiation only interacts with the boundaries of the domain

    Optically thick/dense means that the fluid absorbs and re-emits theradiation

    10-8ANSYS, Inc. Proprietary 2009 ANSYS, Inc. All rights reserved. April 28, 2009Inventory #002598

    For optically thick media the P1 model is a good choice Many combustion simulations fall into this category since combustion

    gases tend to absorb radiation

    The P1 models gives reasonable accuracy without too muchcomputational effort

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    Heat Transfer

    Training ManualChoosing a Radiation Model For optically thin media the Monte Carlo or Discrete Transfer models

    may be used

    DTM can be less accurate in models with long/thin geometries

    Monte Carlo uses the most computational resources, followed by DTM

    Both models can be used in optically thick media, but the P1 model usesfar less computational resources

    10-9ANSYS, Inc. Proprietary 2009 ANSYS, Inc. All rights reserved. April 28, 2009Inventory #002598

    Available for Monte Carlo and DTM

    Neglects the influence of the fluid on the radiation field (only boundariesparticipate)

    Can significantly reduce the solution time

    Radiation in Solid Domains

    In transparent or semi-transparent solid domains (e.g. glass) only theMonte Carlo model can be used

    There is no radiation in opaque solid domains

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    Heat Transfer

    Training Manual

    Inlet Static Temperature

    Total Temperature

    Total Enthalpy

    Outlet No details (except Radiation, see below)

    Opening Opening Temperature

    Opening Static Temperature

    Heat Transfer Boundary Conditions

    10-10ANSYS, Inc. Proprietary 2009 ANSYS, Inc. All rights reserved.

    April 28, 2009Inventory #002598

    Wall Adiabatic

    Fixed Temperature

    Heat Flux

    Heat Transfer Coefficient

    Radiation Quantities

    Local Temperature (Inlet/Outlet/Opening)

    External Blackbody Temperature(Inlet/Outlet/Opening)

    Opaque

    Specify Emissivity and Diffuse Fraction

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    Heat Transfer

    Training ManualDomain Interfaces GGI connections are

    recommended for Fluid-Solid andSolid-Solid interfaces

    If radiation is modelled in onedomain and not the other, setEmissivity and Diffuse Fraction

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    radiation Set these on the boundary

    condition associated with the

    domain interface

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    Heat Transfer

    Training ManualThin Wall Modeling Using solid domains to model heat transfer through thin solids can present

    meshing problems

    The thickness of the material must be resolved by the mesh

    Domain interfaces can be used to model a thin material Normal conduction only; neglects any in-plane conduction

    Example: to model a baffle with heattransfer through the thickness

    10-12ANSYS, Inc. Proprietary 2009 ANSYS, Inc. All rights reserved.

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    Create a Fluid-Fluid Domain Interface

    On the Additional Interface Modelstab setMass and Momentumto No Slip Wall

    This makes the interface a wall rather thanan interface that fluid can pass through

    Enable the Heat Transfertoggle and pickthe Thin Material option

    Specify a Material and Thickness

    Other domain interface types (Fluid-Solidetc) can use the Thin Material option torepresent coatings etc.

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    Heat Transfer

    Training ManualThermal Contact Resistance

    A Thermal Contact Resistance can bespecified using the same approach

    as Thin Wall modeling Just select the Thermal Contact

    Resistance option instead of the ThinMaterial option

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    Heat Transfer

    Training ManualNatural Convection Natural convection occurs

    when temperature differences inthe fluid result in densityvariations

    This is one-type of buoyancydriven flow

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    gravity acting on the densityvariations

    As discussed in the Domains lecture, a source termSM,buoy= (ref) g is added to the momentum equations

    The density difference (ref) is evaluated using either the FullBuoyancy model or the Boussinesq model

    Depending on the physics the model is automatically chosen

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    Heat Transfer

    Training ManualSolution Notes When solving heat transfer

    problems, make sure that you have

    allowed sufficient solution time forheat imbalances in all domains to

    become very small, particularlywhen Solid domains are included

    Sometimes residuals reach the

    10-15ANSYS, Inc. Proprietary

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    imbalances trend towards zero Create Solver Monitors showing

    IMBALANCElevels for fluid andsolid domains

    View the imbalance informationprinted at the end of the solver

    output file

    Use a Conservation Target whendefining Solver Control in CFX-Pre

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    Heat Transfer

    Training ManualHeat Transfer Variables The results file contains several variables related to heat transfer

    Variables starting with Wall are only defined on walls

    Mesh

    Control Volumes

    Temperature

    This is the local fluid temperature

    When plotted on a wall it is the temperature on the

    wall, Twall

    Wall Adjacent Temperature

    This is the average temperature in the control

    10-16ANSYS, Inc. Proprietary

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    April 28, 2009

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    )( refwallcw TThq =

    Where Tref is the Wall AdjacentTemperatureor the tbulk for htctemperature if specified

    Twallqw

    volume next to the wall

    Wall Heat Transfer Coefficient, hc

    By default this is based on Twall and the WallAdjacent Temperature, not the far-field fluidtemperature

    Set the expert parameter tbulk for htc to define

    a far-field fluid temperature to use instead of theWall Adjacent Temperature

    Wall Heat Flux, qw This is the total heat flux into the domain by all

    modes convective and radiative (when modeled)

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    Heat Transfer

    Training ManualHeat Transfer Variables Heat Flux

    This is the total convective heat flux into the domain

    Does not include radiative heat transfer when a radiation model is used

    Convective heat flux contains heat transfer due to both advection and diffusion

    It can be plotted on all boundaries (inlets, outlets, walls etc)

    At an inlet it would represent the energy carried with the incoming fluid relative to the fluidReference Temperature (which is a material property, usually 25 C)

    Wall Radiative Heat Flux

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    The net radiative energy leaving the boundary (emission minus incoming)

    Heat Flux+ Wall Radiative Heat Flux= Wall Heat Flux

    Only applicable when radiation is modeled

    Wall Irradiation Flux

    The incoming radiative flux Only applicable when radiation is modeled