heat transfer 10-1 ansys, inc. proprietary © 2009 ansys, inc. all rights reserved. april 28, 2009...

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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

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Page 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

Heat Transfer

10-1ANSYS, Inc. Proprietary© 2009 ANSYS, Inc. All rights reserved.

April 28, 2009Inventory #002598

Training Manual

10-1ANSYS, Inc. Proprietary© 2009 ANSYS, Inc. All rights reserved.

April 28, 2009Inventory #002598

Chapter 10

Heat Transfer

Introduction to CFX

Page 2: 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

Heat Transfer

10-2ANSYS, Inc. Proprietary© 2009 ANSYS, Inc. All rights reserved.

April 28, 2009Inventory #002598

Training ManualGoverning Equations

Continuity

Momentum

Energy

where

Conservation Equations

Page 3: 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

Heat Transfer

10-3ANSYS, Inc. Proprietary© 2009 ANSYS, Inc. All rights reserved.

April 28, 2009Inventory #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

Etottot SUThU

t

p

t

h

)()() (

)(

Page 4: 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

Heat Transfer

10-4ANSYS, Inc. Proprietary© 2009 ANSYS, Inc. All rights reserved.

April 28, 2009Inventory #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

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Heat Transfer

10-5ANSYS, Inc. Proprietary© 2009 ANSYS, Inc. All rights reserved.

April 28, 2009Inventory #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

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Heat Transfer

10-6ANSYS, Inc. Proprietary© 2009 ANSYS, Inc. All rights reserved.

April 28, 2009Inventory #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

)( 4min

4maxrad TTQ

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Heat Transfer

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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

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Heat Transfer

10-8ANSYS, Inc. Proprietary© 2009 ANSYS, Inc. All rights reserved.

April 28, 2009Inventory #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

Page 9: 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

Heat Transfer

10-9ANSYS, Inc. Proprietary© 2009 ANSYS, Inc. All rights reserved.

April 28, 2009Inventory #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

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Heat Transfer

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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

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Heat Transfer

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April 28, 2009Inventory #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

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Heat Transfer

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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.

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Heat Transfer

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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

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Heat Transfer

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Training ManualNatural Convection

• Natural convection occurswhen 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 termSM,buoy = ( – ref) g is added to the momentum equations

• The density difference ( – ref) is evaluated using either the Full Buoyancy model or the Boussinesq model

• Depending on the physics the model is automatically chosen

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Heat Transfer

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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

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Heat Transfer

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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)

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Heat Transfer

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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