Thermal Network
Description
 Heat flow through solids, liquids, or gases.
 Heat flow from one surface to another surface through electromagnetic waves.
 Heat flow applied directly at a point.
Use Flow Simulator to integrate thermal resistances of conduction, convection and radiation, and direct heat application, either as a standalone network or as a thermal network, coupled with a flow network to generate combined results. SteadyState and Transient analyses are available for both options.
The flow solver and thermal network solver are segregated. The thermal network and flow network carry out their runs separately and reach convergence independently of each other. They both must reach convergence for the run to complete successfully.
Thermal Network Model Creation in the GUI
Use Flow Simulator to couple one (or more) thermal network with a flow network, or model standalone thermal networks. The Thermal Network section is placed after the Flow section in the Element Library. Moreover, all thermal network elements used in the models are listed in Thermal Model Browser.
Standalone Thermal Network Model
In the standalone thermal network models, the thermal network elements are segregated from any flow elements. Place boundary and internal nodes and then connect resistors (Conductor, Convector, Radiator, and Heat Flow elements) to Thermal Nodes. The figure below shows all Thermal Nodes and Resistors connected to each other.
Node Temperature must be set for all Boundary Temperature nodes. Currently, Flow Simulator does not have an initialization for the thermal network, thus Node Temperature, as an initial, guess must be defined for Internal Temperature Nodes in the Property Editor as well. If there exists a constant Heat input at the Internal Boundary location, this should be given as Nodal Heat input.
All entities in the Property Editor must be filled for all used resistors.
There are two subtypes of the Conductor resistor. The conductivity can either be a fixed value or be selected from the enabled materials; Flow Simulator uses conductivity of that material. The geometric inputs of CrossSection Area and Thickness for Simple Conductor and Inner  Outer Radiuses and Length of the Radial Conductor can be given as value or can automatically be obtained by selecting Tnodes or by measuring from the GUI view.
The Convector element requires two inputs. If the Convector element is not associated with a Flow Element, then the only enabled HTC Relation is the Fixed HTC and its value should be given. The second input is Surface Area.
The Radiator resistor has two subtypes, Simple Radiation, which calculates the heat transfer on a single surface due to radiation, requires three inputs: Surface Area, Emissivity, and View Factor LR. However, when the radiation occurs between two parallel surfaces, select the Radiation Between two Surfaces subtype, and parameters of Surface Area and Emissivity should be given for both surfaces. The View Factor is given based on the View Factor option. If the View Factor is from LefttoRight, then View Factor LR should be given, and View Factor RL should be filled if View Factor is RighttoLeft.
The Heat Flow resistor must be positioned before or after a Boundary Temperature node, since, for internal heat addition, the Internal Tnode is added with an input Q option as Nodal Heat. Set Surface Area and Heat Input in the Property Editor for the Heat Flow resistor.
 Steady State Thermal  steady analysis
 Transient Thermal  transient analysis
If needed, thermal network convergence tolerance and damping factors can be adjusted from the Solvers Convergence and Damping Controls panels, respectively.
Thermal Networks Combined with the Flow Network
There are two ways to combine a thermal network with a flow network.
ThermalNetworks Coupled with the Flow Network
In the above example, the Boundary Temperature Nodes are associated with the Tube element and each Convector Resistor is linked to one of the tube segments. The Convector Resistor is coupled with a Momentum Chamber.
When a Boundary Temperature Node is associated with an element, the temperature of the Boundary Tnode is equivalent to the temperature of the fluid. Then, define the associated Element ID and the element’s Axial Segment.
All other resistors are constructed as stated in the previous section.
 Steady State Flow + Steady State Thermal
 Transient Flow + Transient Thermal
 QuasiSteady Flow + Transient ThermalNote: If the flow model does not have transient components, such as tanks or accumulators, this option can be used.
Thermal Networks Attached to the Flow Network
If the thermal network and flow network consist of many resistors and elements, respectively, it is also possible to attach thermal networks to a flow network through the TN Box. Use the TN box to group thermal items.
The TN Box is dragged and dropped in the model area near the element to which the thermal network is attached.
 Press the Shift key and leftclick to select the element or chamber.
 Continue to press the Shift and doubleclick on the same element or chamber.
 The TN Box relates to the target item with a dashed line.
 Doubleclick on the TN box to get inside.
 Draganddrop thermal nodes and thermal resistor elements to form the Thermal Network. The procedure explained in the previous section can be followed.
Thermal Network Element Input Variables
Thermal Node Input Variables  

Index  UI Name (.flo label)  Description 
1  Type (TNODE_TYPE)  Type of a Thermal Node, it can be either Boundary or Internal 
2  Associated with an Element (ASSOC_TYPE)  Type of a fluid entity with which the thermal node is associated. If the TNODE is not associated with a flow entity, then it takes NONE 
3  Element ID (ASSOC_ID)  The identification number of the flow element that is associated with the Thermal Node. 
4  Axial Segment ID (ASSOC_SEG)  If the associated element (Incompressible or Compressible TUBE or Advanced Orifice) has Stations, the parts between these stations are SEGMENTs. This variable defines which part of the element will communicate with the Thermal Node. 
5  (ASSOC_SIDE)  If the associated element (Incompressible Tube or Advanced Orifice) has Wall Sides defined for the segments, then this variable specifies the wall side of the target segment of the target entity that the Tnode is associated with. 
6  Node Temperature (TEMPERATURE)  Total temperature of the solid if the Tnode is not associated with flow entity. Otherwise, it is Fluid temperature, and should be set as FROM_FLUID. For the Internal TNODE, this value is an initial guess if it is not associated with Flow entity. 
7  Volume (VOLUME)  Volume of the internal temperature node. This variable used
to calculate mass of the node only if the analysis is transient.
NODE_MASS = NODE_VOLUME * RHO_NODE 
8  Material List (MATERIAL)  Material of the internal temperature node, and again, it is
activated only at the transient analysis. The supported
materials are:

9  (COUPLING)  This is type of data being transferred between the
temperature node and the associated flow entity. There are five
inputs as a coupling method:
Note: This is auto Generated
Input.

10  Nodal Heat (NODAL_HEAT)  Constant heat input for the Internal Temperature Node 
11  Surface Rotation (SURF_ROTATION)  Surface rotational speed represented by this Thermal Node.
0.0: Specifies a stationary element. 1.0: Rotor 1, as defined in Analysis Reference Data. 2.0: Rotor 2, as defined in Analysis Reference Data. 3.0: Rotor 3, as defined in Analysis Reference Data. 
Thermal Conductor Input Variables  

Index  UI Name (.flo label)  Description 
1  Not in UI (LEFT_NODE)  Identification number of Conductor resistor’s upstream Thermal Node. 
2  Not in UI (RIGHT_NODE)  Identification number of Conductor resistor’s downstream Thermal Node. 
3  Conductor Type (SUB_TYPE)  Determines which subtype of a Conductor Resistor is used:

4  Material List (CONDUC/MAT)  A fixed Conductivity [] value can be given or one of the
supported materials can be selected and Flow Simulator determines the
conductivity during the analysis.

5  CrossSection Area (SURFACE_AREA)  Conduction area 
6  Thickness (THICKNESS)  Conduction length, in other words, the thickness of the conductor in the heat flow direction. 
7  Inner Radius (INNER_RADIUS)  Inner Radius of the conductor 
8  Outer Radius (OUTER_RADIUS)  Outer Radius of the conductor 
Thermal Conductor Input Variables  

Index  UI Name (.flo label)  Description 
1  Not in UI (LEFT_NODE)  Identification number of Conductor resistor’s upstream Thermal Node. 
2  Not in UI (RIGHT_NODE)  Identification number of Conductor resistor’s downstream Thermal Node. 
3  Use Element Heat Transfer Settings (HEAT_TRANSFER_FLAG)  When this option is selected, the flag becomes ‘FROM_FLUID’ and the heat transfer calculation will be done based on the associated element’s heat transfer settings. If this option is not selected, then the flag is NONE, and HTC_METHOD should be defined. 
4  Surface Area (SURFACE AREA)  Surface area of the Convector 
5  HTC Relation (HTC_METHOD)  Specifies the Heat Transfer calculation method:
If the Convector resistor is coupled to an element:
If the Convector resistor is coupled to a
chamber:

6  Heat Transfer Coefficient (HTC_VALUE)  If HTC_METHOD is specified as FIXED_HTC, then its value
should be set to HTC_VALUE. If either HEAT_TRANSFER_FLAG is set to FROM_FLUID or HTC_METHOD is set to one of the enabled HTC calculation methods, then the HTC_VALUE becomes 0. 
7  Turbulent HT Inlet Effects (HT_INLET_EFF)  Heat Transfer inlet effect
Note: Turbulent HT Inlet Effects are
available only for some of the HTC Relations
(LapidesGoldstein, DittusBoelter, SiederTate,
Gnielinski, BhattiShah)

8  Laminar HTC relation (LAMINAR_NUSSELT)  Laminar HTC relation
Note: Laminar HTC Relations are
available only for some of the HTC Relations
(LapidesGoldstein, DittusBoelter, SiederTate,
Gnielinski, BhattiShah)

9  Subtype (SUBTYPE)  For Plate in XFlow, Turb., Avg (Colburn), Plate in XFlow,
Turb., Local (Colburn), Cylinder in XFlow, Turb., Avg
(ChurchillBernstein):
For Hor. Plate in Free Conv., Turb., Avg.:

10  (LENGTH_SCALE)  For Plate in XFlow, Turb., Avg (Colburn), Plate in XFlow,
Turb., Local (Colburn)
For Cylinder in XFlow, Turb., Avg (ChurchillBernstein)
and Hor. Cylinder in free Convection., Turb., Avg.
(ChurchillChu)
For Vert. Prism in Free Conv., Turb., Avg.
(McAdams), Hor. Plate in Free Conv., Turb., Avg.

11  Cross Velocity  For Plate in XFlow, Turb., Avg (Colburn), Plate in XFlow,
Turb., Local (Colburn), Cylinder in XFlow, Turb., Avg (ChurchillBernstein)

12  Tangential Angle  For Plate in XFlow, Turb., Avg (Colburn), Plate in XFlow,
Turb., Local (Colburn), Cylinder in XFlow, Turb., Avg (ChurchillBernstein)

13  Radial Angle  For Plate in XFlow, Turb., Avg (Colburn), Plate in XFlow,
Turb., Local (Colburn), Cylinder in XFlow, Turb., Avg (ChurchillBernstein)

Thermal Conductor Input Variables  

Index  UI Name (.flo label)  Description 
1  Not in UI (LEFT_NODE)  Identification number of Conductor resistor’s upstream Thermal Node. 
2  Not in UI (RIGHT_NODE)  Identification number of Conductor resistor’s downstream Thermal Node. 
3  Radiator Type (SUB_TYPE)  Determines which subtype of a Radiator Resistor is used:

4  Surface Area (Left) (SURFACE_AREA_L)  Surface Area of the left surface 
5  Surface Area (Right) (SURFACE_AREA_R)  Surface Area of the right surface 
6  Emissivity (Left) (EMISS_L)  Emissivity of the left surface 
7  Emissivity (Right) (EMISS_R)  Emissivity of the right surface 
8  View Factor (VIEW_FAC)  Radiation view factor, the portion of the radiation which leaves the left surface (or surface 1) and hits the right surface (or surface 2). View factor is based on lineofsight, orientation, and distance between the two surfaces. 
Thermal Conductor Input Variables  

Index  UI Name (.flo label)  Description 
1  Not in UI (LEFT_NODE)  Identification number of Conductor resistor’s upstream Thermal Node. 
2  Not in UI (RIGHT_NODE)  Identification number of Conductor resistor’s downstream Thermal Node. 
3  Heat Flow into Node (Q_INPUT)  Constant heat value added on the surface 
4  Surface Area (SURFACE_AREA)  Surface area 
Thermal Network Theory
 Heat (Q) can be along heat resistors (branches)
 Heat (Q) is balanced at user defined temperature nodes (TNodes)
Therefore, at a temperature node I, energy balance is written as
 Conductors
 Simple Conductor
 Radial Conductor
 Convectors
 Radiators
 Simple Radiator
 Two Surface Radiation
 Heat Flow
Thermal Resistors and Heat Flow Equations
Conductors
 Simple Conductor: Heat is carried from Left Node to
Right Node and regardless of the actual heat flow direction, (positive or
negative) is carried from Left to Right.
(2) Where:
k: Conductivity
A: Surface Area
L: Thickness
 Radial Conductor: Heat is carried from Left Node to Right Node
along a radial conductor.
(3) Where:
r_{2}: Outer Radius
r_{1}: Inner Radius
Convector
Heat flows from Left Node to Right Node along a convector.
Where:
h: Heat transfer coefficient (can either be fixed or based on a correlations). Refer Solver General theory sections for Heat Transfer Correlations.
A: Surface area
T: Temperature
If the convector is attached to a fluid chamber, the convector uses a relative total temperature from the fluid chamber. The relative total temperature applies to models with rotating surfaces, as found in a gas turbine secondary air systems. The swirl of the fluid in the chamber and the rotational speed of the surface (set on the thermal node) are used to calculate the relative total temperature.
Radiators
 Simple Radiator: Heat is carried from Left Node to Right Node
through a simple radiator.
(5) Where:
σ: StefanBoltzmann constant
: Emissivity of Left Surface
A_{L}: Left Surface’s Area
 Two Surface Radiation:Heat is carried from Left Surface to
Right Surface.
(6) Where:
F_{LR}: View Factor
Heat Flow
User inserted Heat is carried from Left Node to Right Node. Since the Heat Flow resistor provides a constant heat flow, the derivatives are always zero.
Where:
Q: user inserted heat
Numerical Method
At a Node I, the energy imbalance can be defined as:
And we try to obtain:
Therefore, the Newton’s method can be employed as
Jacobian Matrices
2D Jacobian Matrix for Linear Solver
The Jacobian matrix used in Newton’s method is formed by looping over all heat resistors and the residual vector is obtained for free. It’s assumed that heat is flowing from Left node to Right node. The Jacobian matrix for each type of resistor has the form:
1D Jacobian Matrix for Sparse Solver
As the 2D Jacobian matrix requires Tnodes*Tnodes memory allocation, Linear Solver becomes inadequate for larger models. Thus, 1D coefficient matrix is formed again by looping all heat resistors, and sparse matrix is obtained by using the coordinate storage format.
Thermal Network Elements Outputs
Outputs in file with “res” extension. Output units controlled by user setting in “Output Control” panel.
Name  Description  Units ENG, SI 

THERMAL_NETWORK  More than one Thermal Networks can be constructed in one model; thus, this variable specifies the Thermal Network’s identification number.  None 
WITH ASSOC_ITEMS  If the Thermal Network is coupled with Flow Network, the associated Flow entities are listed with this variable. Exx represents Elements, and Cxx represents Chambers.  None 
SIMULATION  The Analysis type (either STEADYSTATE or TRANSIENT) is stated with this parameter.  None 
MATRIX SOLVER  The Jacobian matrix can be solved either by Linear Solver or by Sparse Solver.  None 
NUM_STREAMS  Number of fluid streams in the thermal network, taken from associated fluid network item  None 
NUM_TNODES  Number of Active Thermal Nodes (Boundary TNode and Internal TNode)  None 
NUM_CONDUCT  Number of Active Conductors  None 
NUM_CONVECT  Number of Active Convectors  None 
NUM_RADIAT  Number of Active Radiators  None 
NUM_HEAT_FLOW  Number of Active Heat Flows  None 
CONVERGE INFO  Line of text that gives convergence information for the thermal network. Gives the number of thermal iterations model took to converge, which fluid network (MAIN SOLVER) iteration the thermal network ran on and the rootmeansquare error of the thermal network solution  None 
Thermal Node Results  
TNODE  Thermal node number  None 
TYPE  Type of Thermal Node; Boundary Tnode (B) or Internal Tnode (I)  None 
COUPLING 
Information about the associated flow item

None 
QIMBALANCE  Heat (Q) imbalance at the thermal node  Btu/s, W 
TT  Total Temperature of the Thermal Node  Deg F, Deg K 
CAPACITANCE  Thermal capacitance of the Thermal Node material  Btu/DegF, J/Deg K 
DENSITY  Density of the Thermal Node material  Lbm/ft^{3}, kg/ft^{3} 
CP  Specific heat of the Thermal Node material  Btu/lbmDeg F, J/kgDeg K 
NODAL_HEAT  Heat addition or removal from the Thermal Node  Btu/s, W 
Resistor Results  
IDNUM  Identification number of the resistor  None 
TYPE  Type of the resistor:

None 
SUBTYPE  Subtype of the resistors:

None 
HEAT_FLOW  Heat flow across the resistor  Btu/s, W 
CONDUCTANCE  Conductance of the resistor  Btu/s/Deg F, W/Deg K 
LNODE  Identification number of the resistor’s leftside node  None 
LCOUPLING  Information about coupling of the left node. Follows same scheme as COUPLING in the Thermal Node Results table (see above), except that the LCOUPLING line will start with either B for a boundary thermal node or I for an internal thermal node  None 
L_TT  Total temperature of the Left Thermal Node (relative fluid total temperature for rotating right node).  Deg F, Deg K 
RNODE  Identification number of the resistor’s rightside node  None 
RCOUPLING  Information about coupling of the right node. Follows same scheme as COUPLING in the Thermal Node Results table (see above), except that the LCOUPLING line will start with either B for a boundary thermal node or I for an internal thermal node  None 
R_TT  Total temperature of the right Thermal Node (relative fluid total temperature for rotating left node).  Deg F, Deg K 
HTC  Heat transfer coefficient calculated for the Convector resistor  B/HrFt^{2}F, W/m^{2}/K 
COND  Conductivity through the Conductor resistor  B/HrFt degF, W/m/Deg K 
EMIS1  Emissivity of the left node surface (Radiator resistor only)  None 
EMIS2  Emissivity of the right node surface (Radiator resistor only)  None 
References
 Chapman, A. J. (n.d.). Fundamentals of Heat Transfer. 1987: Macmillan.
 Churchill, S. a. (1977). A Correlating Equation for Forced Convection From Gases and Liquids to a Circular Cylinder in Crossflow. J. Heat Transfer, 300306.
 Churchill, S. W. (1975). averaged Nusselt number for turbulent free convection around a. Int. J. Heat Mass Transfer, 1049.
 Holman, J. P. (n.d.). Heat Transfer (8th ed.).
 Incropera F.P., D. D. (n.d.). Fundamentals of Heat and Mass Transfer", 7th edition Eq. 8.62.
 Incropera, F. a. (2006). Fundamentals of Heat and Mass Transfer, 6th Edition. John Wiley & Sons.
 Kreith, F. a. (1980). Basic Heat Transfer.
 Lapides, M. a. (1957). HEAT TRANSFER SOURCE FILE DATA. APEX 425 United States.
 M.E.Crawford, W. a. (1976). Convective Heat and Mass Transfer.
 R.K.Shah, M. a. (1987). Turbulent and transition flow convective heat transfer in ducts, in Handbook of SinglePhase Convective Heat Transfer Chapter 4.
 Weise, S. (n.d.). Average turbulent Nu on short, vertical planes and cylinders, Heat Transmission, Third Edition. McAdams.