This package provides component models to compute heat conduction.
Extends from Modelica.Icons.VariantsPackage (Icon for package containing variants).
Name | Description |
---|---|
SingleLayer | Model for single layer heat conductance |
SingleLayerCylinder | Heat conduction in a cylinder |
MultiLayer | Model for heat conductance through a solid with multiple material layers |
BaseClasses | Package with base classes for Buildings.HeatTransfer.Conduction |
If the material is a record that extends
Buildings.HeatTransfer.Data.Solids and its
specific heat capacity (as defined by the record material.c
)
is non-zero, then this model computes transient heat conduction, i.e., it
computes a numerical approximation to the solution of the heat equation
ρ c (∂ T(u,t) ⁄ ∂t) = k (∂² T(u,t) ⁄ ∂u²),
where ρ is the mass density, c is the specific heat capacity per unit mass, T is the temperature at location u and time t and k is the heat conductivity. At the locations u=0 and u=x, where x is the material thickness, the temperature and heat flow rate is equal to the temperature and heat flow rate of the heat heat ports.
To spatially discretize the heat equation, the construction is
divided into compartments with material.nSta ≥ 1
state variables.
The state variables are connected to each other through thermal conductors.
There is also a thermal conductor
between the surfaces and the outermost state variables. Thus, to obtain
the surface temperature, use port_a.T
(or port_b.T
)
and not the variable T[1]
.
Each compartment has the same material properties.
To build multi-layer constructions,
use
Buildings.HeatTransfer.Conduction.MultiLayer instead of this model.
If material.c=0
, or if the material extends
Buildings.HeatTransfer.Data.Resistances,
then steady-state heat conduction is computed. In this situation, the heat
flow between its heat ports is
Q = A k ⁄ x (Ta-Tb),
where A is the cross sectional area, x is the layer thickness, Ta is the temperature at port a and Tb is the temperature at port b.
Extends from Buildings.HeatTransfer.Conduction.BaseClasses.PartialConductor (Partial model for heat conductor).
Type | Name | Default | Description |
---|---|---|---|
Area | A | Heat transfer area [m2] | |
ThermalResistance | R | if (material.R == 0) then ma... | Thermal resistance of construction [K/W] |
Material | material | redeclare parameter Data.Bas... | Material from Data.Solids or Data.Resistances |
Initialization | |||
Boolean | steadyStateInitial | false | =true initializes dT(0)/dt=0, false initializes T(0) at fixed temperature using T_a_start and T_b_start |
Temperature | T_a_start | 293.15 | Initial temperature at port_a, used if steadyStateInitial = false [K] |
Temperature | T_b_start | 293.15 | Initial temperature at port_b, used if steadyStateInitial = false [K] |
Type | Name | Description |
---|---|---|
HeatPort_a | port_a | Heat port at surface a |
HeatPort_b | port_b | Heat port at surface b |
model SingleLayer "Model for single layer heat conductance" extends Buildings.HeatTransfer.Conduction.BaseClasses.PartialConductor( final R=if (material.R == 0) then material.x/material.k/A else material.R/A); // if material.R == 0, then the material specifies material.k, and this model specifies x // For resistances, material.k need not be specified, and hence we use material.R // The value T[:].start is used by the solver when finding initial states // that satisfy dT/dt=0, which requires solving a system of nonlinear equations // if the convection coefficient is a function of temperature. Modelica.SIunits.Temperature T[nSta](start= {T_a_start+(T_b_start-T_a_start) * UA * sum(1/(if (k==1 or k==nSta+1) then UAnSta2 else UAnSta) for k in 1:i) for i in 1:nSta}, each nominal = 300) "Temperature at the states"; Modelica.SIunits.HeatFlowRate Q_flow[nSta+1] "Heat flow rate from state i to i+1"; replaceable parameter Data.BaseClasses.Material material "Material from Data.Solids or Data.Resistances"; parameter Boolean steadyStateInitial=false "=true initializes dT(0)/dt=0, false initializes T(0) at fixed temperature using T_a_start and T_b_start"; parameter Modelica.SIunits.Temperature T_a_start=293.15 "Initial temperature at port_a, used if steadyStateInitial = false"; parameter Modelica.SIunits.Temperature T_b_start=293.15 "Initial temperature at port_b, used if steadyStateInitial = false"; protected parameter Modelica.SIunits.HeatCapacity C = A*material.x*material.d*material.c/material.nSta "Heat capacity associated with the temperature state"; // nodes at surface have only 1/2 the layer thickness // final parameter Modelica.SIunits.ThermalConductance G[nSta+1](each fixed=false) // "Thermal conductance of layer between the states"; Modelica.SIunits.TemperatureSlope der_T[nSta] "Time derivative of temperature (= der(T))"; final parameter Integer nSta(min=1) = material.nSta "Number of state variables"; final parameter Modelica.SIunits.ThermalConductance UAnSta = UA*nSta "Thermal conductance between nodes"; final parameter Modelica.SIunits.ThermalConductance UAnSta2 = 2*UAnSta "Thermal conductance between nodes and surface boundary"; initial equation // G={UA*nSta * (if (i==1 or i==nSta+1) then 2 else 1) for i in 1:nSta+1}; // The initialization is only done for materials that store energy. if not material.steadyState then if steadyStateInitial then der_T = zeros(nSta); else for i in 1:nSta loop T[i] = T_a_start+(T_b_start-T_a_start) * UA * sum(1/(if (k==1 or k==nSta+1) then UAnSta2 else UAnSta) for k in 1:i); end for; end if; end if; equation port_a.Q_flow = +Q_flow[1]; port_b.Q_flow = -Q_flow[nSta+1]; port_a.T-T[1] = Q_flow[1]/UAnSta2; T[nSta] -port_b.T = Q_flow[nSta+1]/UAnSta2; for i in 2:nSta loop // Q_flow[i] is heat flowing from (i-1) to (i) T[i-1]-T[i] = Q_flow[i]/UAnSta; end for; if material.steadyState then der_T = zeros(nSta); for i in 2:nSta+1 loop Q_flow[i] = Q_flow[1]; end for; else for i in 1:nSta loop der(T[i]) = (Q_flow[i]-Q_flow[i+1])/C; der_T[i] = der(T[i]); end for; end if;end SingleLayer;
If the heat capacity of the material is non-zero, then this model computes transient heat conduction, i.e., it computes a numerical approximation to the solution of the heat equation
ρ c ( ∂ T(r,t) ⁄ ∂t ) = k ( ∂² T(r,t) ⁄ ∂r² + 1 ⁄ r ∂ T(r,t) ⁄ ∂r ),
where ρ is the mass density, c is the specific heat capacity per unit mass, T is the temperature at location r and time t and k is the heat conductivity. At the locations r=ra and r=rb, the temperature and heat flow rate are equal to the temperature and heat flow rate of the heat ports.
If the heat capacity of the material is set to zero, then steady-state heat flow is computed using
Q = 2 π k (Ta-Tb)⁄ ln(ra ⁄ rb),
where ra is the internal radius, rb is the external radius, Ta is the temperature at port a and Tb is the temperature at port b.
To spatially discretize the heat equation, the construction is
divided into compartments with material.nSta ≥ 1
state variables.
The state variables are connected to each other through thermal conductors.
There is also a thermal conductor
between the surfaces and the outermost state variables. Thus, to obtain
the surface temperature, use port_a.T
(or port_b.T
)
and not the variable T[1]
.
Type | Name | Default | Description |
---|---|---|---|
Generic | material | redeclare parameter Building... | Material thermal properties |
Height | h | Height of the cylinder [m] | |
Radius | r_a | Internal radius [m] | |
Radius | r_b | External radius [m] | |
Integer | nSta | Number of state variables | |
Real | griFac | 2 | Grid factor for spacing |
Initialization | |||
Temperature | TInt_start | 293.15 | Initial temperature at port_a, used if steadyStateInitial = false [K] |
Temperature | TExt_start | 293.15 | Initial temperature at port_b, used if steadyStateInitial = false [K] |
Boolean | steadyStateInitial | false | true initializes dT(0)/dt=0, false initializes T(0) at fixed temperature using T_a_start and T_b_start |
Type | Name | Description |
---|---|---|
HeatPort_a | port_a | Heat port at surface a |
HeatPort_b | port_b | Heat port at surface b |
model SingleLayerCylinder "Heat conduction in a cylinder" replaceable parameter Buildings.HeatTransfer.Data.Soil.Generic material "Material thermal properties"; parameter Modelica.SIunits.Height h "Height of the cylinder"; parameter Modelica.SIunits.Radius r_a "Internal radius"; parameter Modelica.SIunits.Radius r_b "External radius"; parameter Integer nSta(min=1) "Number of state variables"; parameter Modelica.SIunits.Temperature TInt_start=293.15 "Initial temperature at port_a, used if steadyStateInitial = false"; parameter Modelica.SIunits.Temperature TExt_start=293.15 "Initial temperature at port_b, used if steadyStateInitial = false"; parameter Boolean steadyStateInitial=false "true initializes dT(0)/dt=0, false initializes T(0) at fixed temperature using T_a_start and T_b_start"; parameter Real griFac(min=1) = 2 "Grid factor for spacing"; Modelica.SIunits.TemperatureDifference dT "port_a.T - port_b.T";Modelica.Thermal.HeatTransfer.Interfaces.HeatPort_a port_a "Heat port at surface a"; Modelica.Thermal.HeatTransfer.Interfaces.HeatPort_b port_b "Heat port at surface b"; Modelica.SIunits.Temperature T[nSta](start= {TInt_start+ (TExt_start-TInt_start)/Modelica.Math.log(r_b/r_a) *Modelica.Math.log((r_a+(r_b-r_a)/(nSta)*(i-0.5))/r_a) for i in 1:nSta}) "Temperature of the states"; Modelica.SIunits.HeatFlowRate Q_flow[nSta+1] "Heat flow rate from state i to i+1"; protected Modelica.SIunits.TemperatureSlope der_T[nSta] "Time derivative of temperature (= der(T))"; parameter Modelica.SIunits.Radius r[nSta+1](each fixed=false) "Radius to the boundary of the i-th domain"; parameter Modelica.SIunits.Radius rC[nSta](each fixed=false) "Radius to the center of the i-th domain"; final parameter Modelica.SIunits.SpecificHeatCapacity c= material.c "Specific heat capacity"; final parameter Modelica.SIunits.ThermalConductivity k= material.k "Thermal conductivity of the material"; final parameter Modelica.SIunits.Density d = material.d "Density of the material"; parameter Modelica.SIunits.ThermalConductance G[nSta+1](each fixed=false) "Heat conductance between the temperature nodes"; parameter Modelica.SIunits.HeatCapacity C[nSta](each fixed=false) "Heat capacity of each state"; initial equation assert(r_a < r_b, "Error: Model requires r_a < r_b."); assert(0 < r_a, "Error: Model requires 0 < r_a."); r[1] = r_a; for i in 2:nSta+1 loop r[i]= r[i-1] + ( r_b - r_a) * (1-griFac)/(1-griFac^(nSta)) * griFac^(i-2); end for; assert(abs(r[nSta+1]-r_b) < 1E-10, "Error: Wrong computation of radius. r[nSta+1]=" + String(r[nSta+1])); // Radii to the center of the domain for i in 1:nSta loop rC[i] = (r[i]+r[i+1])/2; end for; // Conductance between nodes (which are in the center of the domain) G[1] = 2*Modelica.Constants.pi*k*h/Modelica.Math.log(rC[1]/r_a); G[nSta+1] = 2*Modelica.Constants.pi*k*h/Modelica.Math.log(r_b/rC[nSta]); for i in 2:nSta loop G[i] = 2*Modelica.Constants.pi*k*h/Modelica.Math.log(rC[i]/rC[i-1]); end for; // Heat capacity of each segment for i in 1:nSta loop C[i] = (d*Modelica.Constants.pi*c*h*((r[i+1])^2-(r[i])^2)); end for; // The initialization is only done for materials that store energy. if not material.steadyState then if steadyStateInitial then der_T = zeros(nSta); else for i in 1:nSta loop T[i]=TInt_start+ (TExt_start-TInt_start)/Modelica.Math.log(r_b/r_a) * Modelica.Math.log(rC[i]/r_a); end for; end if; end if; equation dT = port_a.T - port_b.T; port_a.Q_flow = +Q_flow[1]; port_b.Q_flow = -Q_flow[nSta+1]; Q_flow[1] = G[1] * (port_a.T-T[1]); Q_flow[nSta+1] = G[nSta+1] * (T[nSta]-port_b.T); for i in 2:nSta loop Q_flow[i]=G[i]*(T[i-1]-T[i]); // Q_flow[i] represents the heat flowing betwen two nodes end for; if material.steadyState then der_T = zeros(nSta); for i in 2:nSta+1 loop Q_flow[i]=Q_flow[1]; end for; else for i in 1:nSta loop der(T[i])= (Q_flow[i]-Q_flow[i+1])/C[i]; der_T[i] = der(T[i]); end for; end if;end SingleLayerCylinder;
To obtain the surface temperature of the construction, use port_a.T
(or port_b.T
)
and not the variable T[1]
because there is a thermal resistance between the surface
and the temperature state.
Extends from Buildings.HeatTransfer.Conduction.BaseClasses.PartialConductor (Partial model for heat conductor), Buildings.HeatTransfer.Conduction.BaseClasses.PartialConstruction (Partial model for multi-layer constructions).
Type | Name | Default | Description |
---|---|---|---|
Area | A | Heat transfer area [m2] | |
ThermalResistance | R | sum(lay[:].R) | Thermal resistance of construction [K/W] |
Generic | layers | redeclare parameter Building... | Construction definition from Data.OpaqueConstructions |
Initialization | |||
Boolean | steadyStateInitial | false | =true initializes dT(0)/dt=0, false initializes T(0) at fixed temperature using T_a_start and T_b_start |
Temperature | T_a_start | 293.15 | Initial temperature at port_a, used if steadyStateInitial = false [K] |
Temperature | T_b_start | 293.15 | Initial temperature at port_b, used if steadyStateInitial = false [K] |
Type | Name | Description |
---|---|---|
HeatPort_a | port_a | Heat port at surface a |
HeatPort_b | port_b | Heat port at surface b |
model MultiLayer "Model for heat conductance through a solid with multiple material layers" extends Buildings.HeatTransfer.Conduction.BaseClasses.PartialConductor( final R=sum(lay[:].R)); Modelica.SIunits.Temperature T[sum(nSta)](each nominal = 300) "Temperature at the states"; Modelica.SIunits.HeatFlowRate Q_flow[sum(nSta)+nLay] "Heat flow rate from state i to i+1"; extends Buildings.HeatTransfer.Conduction.BaseClasses.PartialConstruction;protected Buildings.HeatTransfer.Conduction.SingleLayer[nLay] lay( each final A=A, material = layers.material, T_a_start = _T_a_start, T_b_start = _T_b_start, each steadyStateInitial = steadyStateInitial) "Material layer"; protected parameter Modelica.SIunits.Temperature _T_a_start[nLay](fixed=false) "Initial temperature at port_a of respective layer, used if steadyStateInitial = false"; parameter Modelica.SIunits.Temperature _T_b_start[nLay](fixed=false) "Initial temperature at port_b of respective layer, used if steadyStateInitial = false"; initial equation for i in 1:nLay loop _T_a_start[i] = T_b_start+(T_a_start-T_b_start) * 1/R * sum(lay[k].R for k in i:nLay); _T_b_start[i] = T_a_start+(T_b_start-T_a_start) * 1/R * sum(lay[k].R for k in 1:i); end for; equation // This section assigns the temperatures and heat flow rates of the layer models to // an array that makes plotting the results easier. for i in 1:nLay loop for j in 1:nSta[i] loop T[sum(nSta[k] for k in 1:(i-1)) +j] = lay[i].T[j]; end for; for j in 1:nSta[i]+1 loop Q_flow[sum(nSta[k] for k in 1:i-1)+(i-1)+j] = lay[i].Q_flow[j]; end for; end for;connect(port_a, lay[1].port_a); for i in 1:nLay-1 loopconnect(lay[i].port_b, lay[i+1].port_a); end for;connect(lay[nLay].port_b, port_b); end MultiLayer;