Boundary conditions

Introduction

This page details all the boundary conditions a user has access to as well as what the required input is. A boundary condition makes it so that a problem only has one solution. For example, defining an inlet temperature for the coolant will (for a given heatsink, pump, and heat load) fix the temperatures for the rest of the entities. A boundary condition allows a user to match the model as close as possible to reality; is a pump driving the fluid motion and if so, is this pump positioned upstream or downstream, etc.?

General overview

The following list shows all the available boundary conditions, applicability, and input parameters. Parameters denoted with * are required, the others are optional entries. Click on the name of the boundary condition for more information.

Boundary type Boundary condition Applicable to Input Parameters
Fluid Solid Fluid Solid
Inlet FixedFlowRateInlet :ballot-box-with-check: TT^*, (U(U, Q˙\dot Q or m˙)\dot m)^*, ω\omega
PressureInlet :ballot-box-with-check: TT^*, pp^*
PumpInlet :ballot-box-with-check: TT^*, Performance curve*
FanInlet :ballot-box-with-check: TT^*, Performance curve*
Outlet PressureOutlet :ballot-box-with-check: pp
FanOutlet :ballot-box-with-check: Performance curve*
PumpOutlet :ballot-box-with-check: Performance curve*
MinFlowrateOutlet :ballot-box-with-check: (U(U, Q˙\dot Q or m˙)\dot m)^*
Wall FixedTemperatureWall :ballot-box-with-check: :ballot-box-with-check: TT^* TT^*
HeatedWall :ballot-box-with-check: :ballot-box-with-check: QQ^*, RdR_d, RkR_k QQ^*
ExternalWall :ballot-box-with-check: :ballot-box-with-check: hh^*, TaT_a^*, RdR_d, RkR_k, εexternal\varepsilon_{external} hh^*, TaT_a^*, RdR_d, RkR_k, εexternal\varepsilon_{external}
InsulatedWall :ballot-box-with-check: :ballot-box-with-check: RlR_l^*
Slip :ballot-box-with-check:
Cyclic :ballot-box-with-check: :ballot-box-with-check: Another boundary of type 'Cyclic' Another boundary of type 'Cyclic'

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Important

Any boundary that isn't an interface or has any special boundary condition imposed is by default adiabatic. This means that it will be treated as if a wall with perfect insulation is placed next to it.

For fluids will also the no-slip condition be imposed.

Boundary Types

FixedFlowRateInlet

Name fixedFlowRateInlet
Type Inlet
Applicable to Fluids
Input parameters The temperature TT in [K][K] at the patch should be specified, as well as either the velocity UU in [m/s][m/s], the mass flow rate m˙\dot m in [kg/s][kg/s] or the volumetric flow rate Q˙\dot Q in [m3/s][m^3/s], depending on the chosen option. Also a rotational velocity ω\omega in [rad/s][rad/s] can be set.

With this boundary condition, a flow entering the domain at a certain velocity is specified. The flow can be described by:

  • Fixed value velocity: the magnitude of the inlet velocity at the patch is specified.
  • Mass flow rate: an average mass flow rate is specified, which is translated to a velocity at the patch with the fluid density by the software.
  • Volumetric flow rate: the average volumetric flow rate at the patch is specified. The inlet velocity is then automatically calculated by the software.

A fixedFlowRateInlet boundary condition is typically used in combination with a pressureOutlet boundary condition.

PressureInlet

Name pressureInlet
Type Inlet
Applicable to Fluids
Input parameters The temperature TT in [K][K] and pressure pp in [Pa][Pa] at the patch should be specified.

This boundary condition defines an inflow condition based on the inputted total pressure at the boundary. A pressureInlet condition is typically used in combination with a pressureOulet boundary condition.

The total pressure (Ptot)(P_{tot}) in PaPa relates to the static pressure (Pstat)(P_{stat}) in PaPa through the following relation:

Ptot=Pstat+12ρV2=Pstat+12ρQ˙2A2P_{tot} = P_{stat} + \frac{1}{2}\rho V^2 = P_{stat} +\frac{1}{2}\rho\frac{\dot Q^2}{A^2}

Where:

  • ρ\rho represents the density of the fluid in kgm3\frac{kg}{m^3}
  • VV represents the velocity of the fluid in ms\frac{m}{s}
  • Q˙\dot Q represents the volumetric flow rate of the fluid in m3s\frac{m^3}{s}
  • AA represents the area of the boundary patch in m2m^2

PumpInlet

Name pumpInlet
Type Inlet
Applicable to Fluids
Input parameters The temperature TT in [K][K] at the patch should be specified, as well as the performance curve of the pump.

This boundary condition sets the total pressure at the patch based on the pressure drop as a function of the volumetric flow rate as specified in the performance curve of the pump. This boundary condition is typically used in combination with a pressureOutlet boundary condition at the outlet.

The total pressure (Ptot)(P_{tot}) in PaPa relates to the static pressure (Pstat)(P_{stat}) in PaPa through the following relation:

Ptot=Pstat+12ρV2=Pstat+12ρQ˙2A2P_{tot} = P_{stat} + \frac{1}{2}\rho V^2 = P_{stat} +\frac{1}{2}\rho\frac{\dot Q^2}{A^2}

Where:

  • ρ\rho represents the density of the fluid in kgm3\frac{kg}{m^3}
  • VV represents the velocity of the fluid in ms\frac{m}{s}
  • Q˙\dot Q represents the volumetric flow rate of the fluid in m3s\frac{m^3}{s}
  • AA represents the area of the boundary patch in m2m^2

FanInlet

Name fanInlet
Type Inlet
Applicable to Fluids
Input parameters The temperature TT in [K][K] at the patch should be specified, as well as the performance curve of the fan.

This boundary condition can be used to set a total pressure inlet condition for a fan. The total pressure at the patch is set based on the pressure drop which is specified in the performance curve of the fan as a function of the volumetric flow rate. This boundary condition is typically used in combination with a pressureOutlet boundary condition at the outlet.

The total pressure (Ptot)(P_{tot}) in PaPa relates to the static pressure (Pstat)(P_{stat}) in PaPa through the following relation:

Ptot=Pstat+12ρV2=Pstat+12ρQ˙2A2P_{tot} = P_{stat} + \frac{1}{2}\rho V^2 = P_{stat} +\frac{1}{2}\rho\frac{\dot Q^2}{A^2}

Where:

  • ρ\rho represents the density of the fluid in kgm3\frac{kg}{m^3}
  • VV represents the velocity of the fluid in ms\frac{m}{s}
  • Q˙\dot Q represents the volumetric flow rate of the fluid in m3s\frac{m^3}{s}
  • AA represents the area of the boundary patch in m2m^2

PressureOutlet

Name pressureOutlet
Type Outlet
Applicable to Fluids
Input parameters Optionally, a pressure at the patch can be specified in [Pa][Pa]. If no pressure is specified, it is set to 0 PaPa. This boundary patch fixes the static pressure at that boundary.

This boundary condition defines an outflow condition based on the specified static pressure at the boundary. A pressureOutlet boundary condition is typically used in combination with a fixedFlowRateInlet, a fanInlet, or a pumpInlet.

FanOutlet

Name fanOutlet
Type Outlet
Applicable to Fluids
Input parameters The performance curve of the fan should be specified.

This boundary condition sets the total pressure at the patch based on the pressure drop as a function of the volumetric flow rate as specified in the performance curve of the fan. A fanOutlet condition is typically used in combination with a pressureInlet condition at the inlet.

PumpOutlet

Name pumpOutlet
Type Outlet
Applicable to Fluids
Input parameters The performance curve of the fan should be specified.

This boundary condition sets the total pressure at the patch based on the pressure drop as a function of the volumetric flow rate as specified in the performance curve of the pump. A pumpOutlet condition is typically used in combination with a pressureInlet condition at the inlet.

MinFlowrateOutlet

Name minFlowRateOutlet
Type Outlet
Applicable to Fluids
Input parameters A minFlowRateOutlet only requires one input parameter: either the velocity UU in [m/s][m/s] the mass flow rate m˙\dot m in [kg/s][kg/s] or the volumetric flow rate Q˙\dot Q in [m3/s][m^3/s] at the patch.

This boundary condition ensures that a specified minimum flow rate is achieved through the outlet. This minimum flow rate can be described by:

  • Fixed value velocity: the magnitude of the minimum outlet velocity at the patch is specified.
  • Mass flow rate: the minimum average mass flow rate at the patch is specified. The minimum outlet velocity is then automatically calculated by the software.
  • Volumetric flow rate: the minimum average volumetric flow rate at the patch is specified. The minimum outlet velocity is then automatically calculated by the software.

A minimumFlowRateOutlet boundary condition is typically used in combination with a pressureInlet boundary condition.

FixedTemperatureWall

Name fixedTemperatureWall
Type Wall
Applicable to Fluids and solids
Input parameters Fluid The temperature TT in [K][K] at the patch should be specified.
Solid The temperature TT in [K][K] at the patch should be specified.

With the fixedTemperatureWall, a constant temperature value can be assigned to the patch. This is useful if you want to model a constant temperature heat source or sink.

HeatedWall

Name fixedTemperatureWall
Type Wall
Applicable to Fluids and solids
Input parameters Fluid The heating power QQ in [W][W] should be specified. Optionally, a thermal resistance can be applied by providing the thickness of the thermal resistance layer RdR_d in [m][m] and the conductivity RkR_k of the resistance layer in [W/(mK)][W/(mK)].
Solid The heating power QQ in [W][W] should be specified.

With the heatedWall, a constant heating power value can be assigned to the patch. This is useful if you want to model a heat source or sink with a constant heat flux, specified as the total power.

ExternalWall

Name fixedTemperatureWall
Type Wall
Applicable to Fluids and solids
Input parameters Fluid The heat transfer coefficient hh in [W/(m2K)][W/(m^2K)] and the temperature of the environment TaT_a in [K][K] should be specified.
Optionally, a thermal resistance layer can be defined by setting the thickness of the layer RdR_d in [m][m] and the conductivity RkR_k of the thermal resistance layer in [W/(mK)][W/(mK)]. Optionally, an external emissivity εexternal\varepsilon_{external} in [−] can be set.
Solid The heat transfer coefficient hh in [W/(m2K)][W/(m^2K)] and the temperature of the environment TaT_a in [K][K] should be specified.
Optionally, a thermal resistance layer can be defined by setting the thickness of the layer RdR_d in [m][m] and the conductivity RkR_k of the thermal resistance layer in [W/(mK)][W/(mK)]. Optionally, an external emissivity εexternal\varepsilon_{external} in [−] can be set.

With this boundary condition, heat losses to or gains from the environment can be modeled. Optional thin thermal resistance layers can be specified through the thicknesses and the conductivity of the layers.

InsulatedWall

Name fixedTemperatureWall
Type Wall
Applicable to Fluids and solids
Input parameters Fluid The roughness length RlR_l in [m][m]
Solid /

As the name suggests, this boundary condition represents an adiabatic wall. These boundaries do not thermally interact with the rest of the case setup.

Slip

Name slip
Type Wall
Applicable to Fluids
Input parameters /

This boundary condition ensures that there can be no flow perpendicular to the boundary itself, but there can be flow (with a non-zero velocity) parallel to or along this boundary patch.

Cyclic

Name Cyclic
Type Wall
Applicable to Fluids and solids
Input parameters Another boundary of type 'Cyclic'

ColdStream allows you to assign periodicity. By using the Cyclic boundary patch option, the heat leaving through this boundary will enter again through the second, linked boundary.

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Warning

To link 2 boundaries with one another, they must be assigned to the same parent region. The shape of the linked boundaries must also match with one another.