Extends from Modelica.Fluid.Icons.BaseClassLibrary (Icon for library).
Name | Description |
---|---|
Buoyancy | Model to add buoyancy if there is a temperature inversion in the tank |
ThirdOrderStratifier | Model to reduce the numerical dissipation in a tank |
This model outputs a heat flow rate that can be added to fluid volumes in order to emulate buoyancy during a temperature inversion. For simplicity, this model does not compute a buoyancy induced mass flow rate, but rather a heat flow that has the same magnitude as the enthalpy flow associated with the buoyancy induced mass flow rate.
Extends from Buildings.BaseClasses.BaseIcon (Base icon).
Type | Name | Default | Description |
---|---|---|---|
Volume | V | Volume [m3] | |
Integer | nSeg | 2 | Number of volume segments |
Time | tau | Time constant for mixing [s] |
Type | Name | Description |
---|---|---|
HeatPort_a | heatPort[nSeg] | Heat input into the volumes |
model Buoyancy "Model to add buoyancy if there is a temperature inversion in the tank" extends Buildings.BaseClasses.BaseIcon; replaceable package Medium = Modelica.Media.Interfaces.PartialMedium "Medium model"; parameter Modelica.SIunits.Volume V "Volume"; parameter Integer nSeg(min=2) = 2 "Number of volume segments"; parameter Modelica.SIunits.Time tau(min=0) "Time constant for mixing";Modelica.Thermal.HeatTransfer.Interfaces.HeatPort_a[nSeg] heatPort "Heat input into the volumes"; Modelica.SIunits.HeatFlowRate[nSeg-1] Q_flow "Heat flow rate from segment i+1 to i"; protected parameter Medium.ThermodynamicState sta0 = Medium.setState_pTX(T=Medium.T_default, p=Medium.p_default, X=Medium.X_default[1:Medium.nXi]); parameter Modelica.SIunits.Density rho_nominal=Medium.density(sta0) "Density, used to compute fluid mass"; parameter Modelica.SIunits.SpecificHeatCapacity cp0=Medium.specificHeatCapacityCp(sta0) "Specific heat capacity"; parameter Real k(unit="W/K") = V*rho_nominal*cp0/tau/nSeg "Proportionality constant, since we use dT instead of dH"; equation for i in 1:nSeg-1 loop Q_flow[i] = k*max(heatPort[i+1].T-heatPort[i].T, 0); end for; heatPort[1].Q_flow = -Q_flow[1]; for i in 2:nSeg-1 loop heatPort[i].Q_flow = -Q_flow[i]+Q_flow[i-1]; end for; heatPort[nSeg].Q_flow = Q_flow[nSeg-1];end Buoyancy;
This model reduces the numerical dissipation that is introduced by the standard first-order upwind discretization scheme which is created when connecting fluid volumes in series.
Since the model is used in conjunction with Modelica.Fluid, it computes a heat flux that needs to be added to each volume in order to give the results that a third-order upwind discretization scheme would give. If a standard third-order upwind discretization scheme were to be used, then the temperatures of the elements that face the tank inlet and outlet ports would overshoot by a few tenths of a Kelvin. To reduce this overshoot, the model uses a first order scheme at the boundary elements, and it adds a term that ensures that the energy balance is satisfied. Without this term, small numerical errors in the energy balance, introduced by the third order discretization scheme, would occur.
The model is used by Buildings.Fluid.Storage.StratifiedEnhanced.
Extends from Buildings.BaseClasses.BaseIcon (Base icon).
Type | Name | Default | Description |
---|---|---|---|
Integer | nSeg | 2 | Number of volume segments |
Type | Name | Description |
---|---|---|
HeatPort_a | heatPort[nSeg] | Heat input into the volumes |
input RealInput | m_flow | Mass flow rate from port a to port b |
input RealInput | H_flow[nSeg + 1] | Enthalpy flow between the volumes |
FluidPort_a | fluidPort[nSeg + 2] | Fluid port, needed to get pressure, temperature and species concentration |
model ThirdOrderStratifier "Model to reduce the numerical dissipation in a tank" extends Buildings.BaseClasses.BaseIcon; replaceable package Medium = Modelica.Media.Interfaces.PartialMedium "Medium model"; parameter Integer nSeg(min=2) = 2 "Number of volume segments";Modelica.Thermal.HeatTransfer.Interfaces.HeatPort_a[nSeg] heatPort "Heat input into the volumes"; Modelica.Blocks.Interfaces.RealInput m_flow "Mass flow rate from port a to port b"; Modelica.Blocks.Interfaces.RealInput[nSeg+1] H_flow "Enthalpy flow between the volumes"; Modelica.Fluid.Interfaces.FluidPort_a[nSeg+2] fluidPort( redeclare each package Medium = Medium) "Fluid port, needed to get pressure, temperature and species concentration"; protected Modelica.SIunits.SpecificEnthalpy[nSeg+2] hOut "Extended vector with new outlet enthalpies to reduce numerical dissipation"; Modelica.SIunits.SpecificEnthalpy[nSeg+2] h "Extended vector with port enthalpies, needed to simplify loop"; Modelica.SIunits.HeatFlowRate Q_flow[nSeg] "Heat exchange computed using upwind third order discretization scheme"; Modelica.SIunits.HeatFlowRate Q_flow_upWind "Heat exchange computed using upwind third order discretization scheme"; Integer s(min=-1, max=1) "Index shift to pick up or down volume"; parameter Medium.ThermodynamicState sta0 = Medium.setState_pTX(T=Medium.T_default, p=Medium.p_default, X=Medium.X_default[1:Medium.nXi]); parameter Modelica.SIunits.SpecificHeatCapacity cp0=Medium.specificHeatCapacityCp(sta0) "Density, used to compute fluid volume"; equation // assign zero flow conditions at port fluidPort[:].m_flow = zeros(nSeg+2); fluidPort[:].h_outflow = zeros(nSeg+2); fluidPort[:].Xi_outflow = zeros(nSeg+2, Medium.nXi); fluidPort[:].C_outflow = zeros(nSeg+2, Medium.nC); // assign extended enthalpy vectors for i in 1:nSeg+2 loop h[i] = inStream(fluidPort[i].h_outflow); end for; // in loop, i+1-s is the "down" volume, i+1+s is the "up" volume s = if m_flow > 0 then 1 else -1; hOut[1] = h[1]; hOut[nSeg+2] = h[nSeg+2]; for i in 1:nSeg loop // Third order scheme to approximate interface temperature if ( s > 0) then hOut[i+1] = if ( i==1) then h[2] else 0.5*(h[i+1+s]+h[i+1])-0.125*(h[i+2]+h[i]-2*h[i+1]); else hOut[i+1] = if ( i==nSeg) then h[end-1] else 0.5*(h[i+1+s]+h[i+1])-0.125*(h[i+2]+h[i]-2*h[i+1]); end if; end for; for i in 1:nSeg loop if s > 0 then Q_flow[i] = m_flow * (hOut[i+1] -hOut[i]) +H_flow[i] -H_flow[i+1]; else Q_flow[i] = m_flow * (hOut[i+2]-hOut[i+1]) +H_flow[i] -H_flow[i+1]; end if; end for; Q_flow_upWind = sum(Q_flow[i] for i in 1:nSeg); for i in 1:nSeg loop heatPort[i].Q_flow = Q_flow[i] - Q_flow_upWind/nSeg; end for;end ThirdOrderStratifier;