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Heat Transfer
10-1
ANSYS, Inc. Proprietary
© 2009 ANSYS, Inc. All rights reserved.
April 28, 2009
Inventory #002598
Training Manual
10-1
ANSYS, Inc. Proprietary
© 2009 ANSYS, Inc. All rights reserved.
April 28, 2009
Inventory #002598
Chapter 10
Heat Transfer
Introduction to CFX
Heat Transfer
10-2
ANSYS, Inc. Proprietary
© 2009 ANSYS, Inc. All rights reserved.
April 28, 2009
Inventory #002598
Training ManualGoverning Equations
Continuity
Momentum
Energy
where
Conservation Equations
Heat Transfer
10-3
ANSYS, Inc. Proprietary
© 2009 ANSYS, Inc. All rights reserved.
April 28, 2009
Inventory #002598
Training Manual
• Heat transfer in a fluid domain is governed by the Energy
Transport Equation:
• The Heat Transfer Model relates to the above equation as follows
– None: Energy Transport Equation not solved
– Isothermal: The Energy Transport Equation is not solved but a temperature is
required to evaluated fluid properties (e.g. when using an Ideal Gas)
– Thermal Energy: An Energy Transport Equation is solved which neglects variable
density 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 energy
effects. 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.
SourcesViscous workConvectionTransient Conduction
Governing Equations
Etot
tot
SUThU
t
p
t
h
+⋅⋅∇+∇⋅∇=⋅∇+
∂
∂
−
∂
∂
)()()(
)(
τλρ
ρ
Heat Transfer
10-4
ANSYS, Inc. Proprietary
© 2009 ANSYS, Inc. All rights reserved.
April 28, 2009
Inventory #002598
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 following
conduction equation
SourceTransient Conduction
Heat Transfer
10-5
ANSYS, Inc. Proprietary
© 2009 ANSYS, Inc. All rights reserved.
April 28, 2009
Inventory #002598
Training ManualSelecting a Heat Transfer Model
• The Heat Transfer model is selected
on the Domain > Fluid Models panel
• Enable the Viscous Work term
(Total Energy), or Viscous
Dissipation term (Thermal Energy),
if viscous shear in the fluid is large
(e.g. lubrication or high speed
compressible flows)
• Enable radiation model / submodels
if radiative heat transfer is
significant
Heat Transfer
10-6
ANSYS, Inc. Proprietary
© 2009 ANSYS, Inc. All rights reserved.
April 28, 2009
Inventory #002598
Training Manual
• Radiation effects should be accounted for when
is significant compared to
convective and conductive heat transfer rates
• To account for radiation, Radiative Intensity
Transport Equations (RTEs) are solved
– Local absorption by fluid and at boundaries couples
these RTEs with the energy equation
• Radiation intensity is directionally and
spatially dependent
• Transport mechanisms for radiation intensity:
– Local absorption
– Out-scattering (scattering away from
the direction)
– Local emission
– In-scattering (scattering into the direction)
Radiation
)( 4
min
4
maxrad TTQ −σ=
Heat Transfer
10-7
ANSYS, Inc. Proprietary
© 2009 ANSYS, Inc. All rights reserved.
April 28, 2009
Inventory #002598
Training Manual
• Several radiation models are available which provide approximate solutions
to the RTE
• Each radiation model has its assumptions, limitations, and benefits
1) Rosseland Model (Diffusion Approximation Model)
2) P-1 Model (Gibb’s Model/Spherical Harmonics Model)
3) Discrete Transfer Model (DTM) (Shah Model)
4) Monte Carlo Model (not available in the ANSYS CFD-Flo product)
Radiation Models
Heat Transfer
10-8
ANSYS, Inc. Proprietary
© 2009 ANSYS, Inc. All rights reserved.
April 28, 2009
Inventory #002598
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 the
radiation
• 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 much
computational effort
Heat Transfer
10-9
ANSYS, Inc. Proprietary
© 2009 ANSYS, Inc. All rights reserved.
April 28, 2009
Inventory #002598
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 uses
far less computational resources
• Surface to Surface Model
– Available for Monte Carlo and DTM
– Neglects the influence of the fluid on the radiation field (only boundaries
participate)
– Can significantly reduce the solution time
• Radiation in Solid Domains
– In transparent or semi-transparent solid domains (e.g. glass) only the
Monte Carlo model can be used
– There is no radiation in opaque solid domains
Heat Transfer
10-10
ANSYS, Inc. Proprietary
© 2009 ANSYS, Inc. All rights reserved.
April 28, 2009
Inventory #002598
Training Manual
• Inlet
– Static Temperature
– Total Temperature
– Total Enthalpy
• Outlet
– No details (except Radiation, see below)
• Opening
– Opening Temperature
– Opening Static Temperature
• 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
Heat Transfer Boundary Conditions
Heat Transfer
10-11
ANSYS, Inc. Proprietary
© 2009 ANSYS, Inc. All rights reserved.
April 28, 2009
Inventory #002598
Training ManualDomain Interfaces
• GGI connections are
recommended for Fluid-Solid and
Solid-Solid interfaces
• If radiation is modelled in one
domain and not the other, set
Emissivity and Diffuse Fraction
values on the side which includes
radiation
– Set these on the boundary
condition associated with the
domain interface
Heat Transfer
10-12
ANSYS, Inc. Proprietary
© 2009 ANSYS, Inc. All rights reserved.
April 28, 2009
Inventory #002598
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 heat
transfer through the thickness
– Create a Fluid-Fluid Domain Interface
– On the Additional Interface Models tab set
Mass and Momentum to No Slip Wall
• This makes the interface a wall rather than
an interface that fluid can pass through
– Enable the Heat Transfer toggle and pick
the Thin Material option
• Specify a Material and Thickness
• Other domain interface types (Fluid-Solid
etc) can use the Thin Material option to
represent coatings etc.
Heat Transfer
10-13
ANSYS, Inc. Proprietary
© 2009 ANSYS, Inc. All rights reserved.
April 28, 2009
Inventory #002598
Training ManualThermal Contact Resistance
• A Thermal Contact Resistance can be
specified using the same approach
as Thin Wall modeling
– Just select the Thermal Contact
Resistance option instead of the Thin
Material option
Heat Transfer
10-14
ANSYS, Inc. Proprietary
© 2009 ANSYS, Inc. All rights reserved.
April 28, 2009
Inventory #002598
Training ManualNatural Convection
• Natural convection occurs
when temperature differences in
the fluid result in density
variations
– This is one-type of buoyancy
driven flow
• Flow is induced by the force of
gravity acting on the density
variations
• As discussed in the Domains lecture, a source term
SM,buoy = (ρ – ρref) g is added to the momentum equations
• The density difference (ρ – ρref) is evaluated using either the Full
Buoyancy model or the Boussinesq model
• Depending on the physics the model is automatically chosen
Heat Transfer
10-15
ANSYS, Inc. Proprietary
© 2009 ANSYS, Inc. All rights reserved.
April 28, 2009
Inventory #002598
Training ManualSolution Notes
• When solving heat transfer
problems, make sure that you have
allowed sufficient solution time for
heat imbalances in all domains to
become very small, particularly
when Solid domains are included
• Sometimes residuals reach the
convergence criteria before global
imbalances trend towards zero
– Create Solver Monitors showing
IMBALANCE levels for fluid and
solid domains
– View the imbalance information
printed at the end of the solver
output file
– Use a Conservation Target when
defining Solver Control in CFX-Pre
Heat Transfer
10-16
ANSYS, Inc. Proprietary
© 2009 ANSYS, Inc. All rights reserved.
April 28, 2009
Inventory #002598
Training ManualHeat Transfer Variables
• The results file contains several variables related to heat transfer
– Variables starting with “Wall” are only defined on walls
)( refwallcw TThq −=
Where Tref is the Wall Adjacent
Temperature or the tbulk for htc
temperature if specified
Twall
qw
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
volume next to the wall
• Wall Heat Transfer Coefficient, hc
– By default this is based on Twall and the Wall
Adjacent Temperature, not the far-field fluid
temperature
– Set the expert parameter “tbulk for htc” to define a
far-field fluid temperature to use instead of the
Wall Adjacent Temperature
– Wall Heat Flux, qw
– This is the total heat flux into the domain by all
modes – convective and radiative (when modeled)
Heat Transfer
10-17
ANSYS, Inc. Proprietary
© 2009 ANSYS, Inc. All rights reserved.
April 28, 2009
Inventory #002598
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 fluid
Reference Temperature (which is a material property, usually 25 C)
• Wall Radiative Heat Flux
– 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

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18 cd 6
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Cfx12 10 heat_transfer

  • 1. Heat Transfer 10-1 ANSYS, Inc. Proprietary © 2009 ANSYS, Inc. All rights reserved. April 28, 2009 Inventory #002598 Training Manual 10-1 ANSYS, Inc. Proprietary © 2009 ANSYS, Inc. All rights reserved. April 28, 2009 Inventory #002598 Chapter 10 Heat Transfer Introduction to CFX
  • 2. Heat Transfer 10-2 ANSYS, Inc. Proprietary © 2009 ANSYS, Inc. All rights reserved. April 28, 2009 Inventory #002598 Training ManualGoverning Equations Continuity Momentum Energy where Conservation Equations
  • 3. Heat Transfer 10-3 ANSYS, Inc. Proprietary © 2009 ANSYS, Inc. All rights reserved. April 28, 2009 Inventory #002598 Training Manual • Heat transfer in a fluid domain is governed by the Energy Transport Equation: • The Heat Transfer Model relates to the above equation as follows – None: Energy Transport Equation not solved – Isothermal: The Energy Transport Equation is not solved but a temperature is required to evaluated fluid properties (e.g. when using an Ideal Gas) – Thermal Energy: An Energy Transport Equation is solved which neglects variable density 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 energy effects. 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. SourcesViscous workConvectionTransient Conduction Governing Equations Etot tot SUThU t p t h +⋅⋅∇+∇⋅∇=⋅∇+ ∂ ∂ − ∂ ∂ )()()( )( τλρ ρ
  • 4. Heat Transfer 10-4 ANSYS, Inc. Proprietary © 2009 ANSYS, Inc. All rights reserved. April 28, 2009 Inventory #002598 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 following conduction equation SourceTransient Conduction
  • 5. Heat Transfer 10-5 ANSYS, Inc. Proprietary © 2009 ANSYS, Inc. All rights reserved. April 28, 2009 Inventory #002598 Training ManualSelecting a Heat Transfer Model • The Heat Transfer model is selected on the Domain > Fluid Models panel • Enable the Viscous Work term (Total Energy), or Viscous Dissipation term (Thermal Energy), if viscous shear in the fluid is large (e.g. lubrication or high speed compressible flows) • Enable radiation model / submodels if radiative heat transfer is significant
  • 6. Heat Transfer 10-6 ANSYS, Inc. Proprietary © 2009 ANSYS, Inc. All rights reserved. April 28, 2009 Inventory #002598 Training Manual • Radiation effects should be accounted for when is significant compared to convective and conductive heat transfer rates • To account for radiation, Radiative Intensity Transport Equations (RTEs) are solved – Local absorption by fluid and at boundaries couples these RTEs with the energy equation • Radiation intensity is directionally and spatially dependent • Transport mechanisms for radiation intensity: – Local absorption – Out-scattering (scattering away from the direction) – Local emission – In-scattering (scattering into the direction) Radiation )( 4 min 4 maxrad TTQ −σ=
  • 7. Heat Transfer 10-7 ANSYS, Inc. Proprietary © 2009 ANSYS, Inc. All rights reserved. April 28, 2009 Inventory #002598 Training Manual • Several radiation models are available which provide approximate solutions to the RTE • Each radiation model has its assumptions, limitations, and benefits 1) Rosseland Model (Diffusion Approximation Model) 2) P-1 Model (Gibb’s Model/Spherical Harmonics Model) 3) Discrete Transfer Model (DTM) (Shah Model) 4) Monte Carlo Model (not available in the ANSYS CFD-Flo product) Radiation Models
  • 8. Heat Transfer 10-8 ANSYS, Inc. Proprietary © 2009 ANSYS, Inc. All rights reserved. April 28, 2009 Inventory #002598 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 the radiation • 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 much computational effort
  • 9. Heat Transfer 10-9 ANSYS, Inc. Proprietary © 2009 ANSYS, Inc. All rights reserved. April 28, 2009 Inventory #002598 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 uses far less computational resources • Surface to Surface Model – Available for Monte Carlo and DTM – Neglects the influence of the fluid on the radiation field (only boundaries participate) – Can significantly reduce the solution time • Radiation in Solid Domains – In transparent or semi-transparent solid domains (e.g. glass) only the Monte Carlo model can be used – There is no radiation in opaque solid domains
  • 10. Heat Transfer 10-10 ANSYS, Inc. Proprietary © 2009 ANSYS, Inc. All rights reserved. April 28, 2009 Inventory #002598 Training Manual • Inlet – Static Temperature – Total Temperature – Total Enthalpy • Outlet – No details (except Radiation, see below) • Opening – Opening Temperature – Opening Static Temperature • 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 Heat Transfer Boundary Conditions
  • 11. Heat Transfer 10-11 ANSYS, Inc. Proprietary © 2009 ANSYS, Inc. All rights reserved. April 28, 2009 Inventory #002598 Training ManualDomain Interfaces • GGI connections are recommended for Fluid-Solid and Solid-Solid interfaces • If radiation is modelled in one domain and not the other, set Emissivity and Diffuse Fraction values on the side which includes radiation – Set these on the boundary condition associated with the domain interface
  • 12. Heat Transfer 10-12 ANSYS, Inc. Proprietary © 2009 ANSYS, Inc. All rights reserved. April 28, 2009 Inventory #002598 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 heat transfer through the thickness – Create a Fluid-Fluid Domain Interface – On the Additional Interface Models tab set Mass and Momentum to No Slip Wall • This makes the interface a wall rather than an interface that fluid can pass through – Enable the Heat Transfer toggle and pick the Thin Material option • Specify a Material and Thickness • Other domain interface types (Fluid-Solid etc) can use the Thin Material option to represent coatings etc.
  • 13. Heat Transfer 10-13 ANSYS, Inc. Proprietary © 2009 ANSYS, Inc. All rights reserved. April 28, 2009 Inventory #002598 Training ManualThermal Contact Resistance • A Thermal Contact Resistance can be specified using the same approach as Thin Wall modeling – Just select the Thermal Contact Resistance option instead of the Thin Material option
  • 14. Heat Transfer 10-14 ANSYS, Inc. Proprietary © 2009 ANSYS, Inc. All rights reserved. April 28, 2009 Inventory #002598 Training ManualNatural Convection • Natural convection occurs when temperature differences in the fluid result in density variations – This is one-type of buoyancy driven flow • Flow is induced by the force of gravity acting on the density variations • As discussed in the Domains lecture, a source term SM,buoy = (ρ – ρref) g is added to the momentum equations • The density difference (ρ – ρref) is evaluated using either the Full Buoyancy model or the Boussinesq model • Depending on the physics the model is automatically chosen
  • 15. Heat Transfer 10-15 ANSYS, Inc. Proprietary © 2009 ANSYS, Inc. All rights reserved. April 28, 2009 Inventory #002598 Training ManualSolution Notes • When solving heat transfer problems, make sure that you have allowed sufficient solution time for heat imbalances in all domains to become very small, particularly when Solid domains are included • Sometimes residuals reach the convergence criteria before global imbalances trend towards zero – Create Solver Monitors showing IMBALANCE levels for fluid and solid domains – View the imbalance information printed at the end of the solver output file – Use a Conservation Target when defining Solver Control in CFX-Pre
  • 16. Heat Transfer 10-16 ANSYS, Inc. Proprietary © 2009 ANSYS, Inc. All rights reserved. April 28, 2009 Inventory #002598 Training ManualHeat Transfer Variables • The results file contains several variables related to heat transfer – Variables starting with “Wall” are only defined on walls )( refwallcw TThq −= Where Tref is the Wall Adjacent Temperature or the tbulk for htc temperature if specified Twall qw 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 volume next to the wall • Wall Heat Transfer Coefficient, hc – By default this is based on Twall and the Wall Adjacent Temperature, not the far-field fluid temperature – Set the expert parameter “tbulk for htc” to define a far-field fluid temperature to use instead of the Wall Adjacent Temperature – Wall Heat Flux, qw – This is the total heat flux into the domain by all modes – convective and radiative (when modeled)
  • 17. Heat Transfer 10-17 ANSYS, Inc. Proprietary © 2009 ANSYS, Inc. All rights reserved. April 28, 2009 Inventory #002598 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 fluid Reference Temperature (which is a material property, usually 25 C) • Wall Radiative Heat Flux – 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

Notas del editor

  1. These are the basic equations that are solved for fluid flow problems. More equations must be solved for more complex flows involving combustion, radiation, etc.