The
Outlet Vent dialog box sets the boundary conditions for an outlet vent zone. It is opened from the
Boundary Conditions task page. See Section
7.3.12 for details about defining the items below.
Controls
Zone Name
sets the name of the zone.
Momentum
contains the momentum parameters.
Gauge Pressure
sets the gauge pressure at the outlet boundary.
Radial Equilibrium Pressure Distribution
enables the radial equilibrium pressure distribution. See Section
7.3.8 for details.
This item appears only for 3D and axisymmetric swirl solvers.
Backflow Direction Specification Method
specifies the method you will use to define the flow direction. If you choose
Direction Vector, you will define the flow direction components, and if you choose
Normal to Boundary or
From Neighboring Cell no inputs are required. See Section
7.3.3 for information on specifying flow direction.
Target Mass Flow Rate
allows you to set mass flow rate as a boundary condition at the outlet.
Loss-Coefficient
sets the nondimensional loss coefficient used to compute the pressure drop. See Section
7.3.12 for details.
Turbulence
contains the turbulence parameters.
Specification Method
specifies which method will be used to input the turbulence parameters. You can choose
K and Epsilon (
-
models and RSM only),
K and Omega (
-
models only),
Intensity and Length Scale,
Intensity and Viscosity Ratio,
Intensity and Hydraulic Diameter, or
Turbulent Viscosity Ratio (Spalart-Allmaras model only). See Section
7.3.2 for information about the inputs for each of these methods. (This item will appear only for turbulent flow calculations.)
Backflow Turbulent Kinetic Energy, Backflow Turbulent Dissipation Rate
set values for the turbulence kinetic energy
and its dissipation rate
. These items will appear if you choose
K and Epsilon as the
Specification Method.
Backflow Turbulent Kinetic Energy, Backflow Specific Dissipation Rate
set values for the turbulence kinetic energy
and its specific dissipation rate
. These items will appear if you choose
K and Omega as the
Specification Method.
Backflow Turbulent Intensity, Backflow Turbulent Length Scale
set values for turbulence intensity
and turbulence length scale
. These items will appear if you choose
Intensity and Length Scale as the
Specification Method.
Backflow Turbulent Intensity, Backflow Turbulent Viscosity Ratio
set values for turbulence intensity
and turbulent viscosity ratio
. These items will appear if you choose
Intensity and Viscosity Ratio as the
Specification Method.
Backflow Turbulent Intensity, Backflow Hydraulic Diameter
set values for turbulence intensity
and hydraulic diameter
. These items will appear if you choose
Intensity and Hydraulic Diameter as the
Specification Method.
Backflow Turbulent Viscosity Ratio
sets the value of the backflow turbulent viscosity ratio
. This item will appear if you choose
Turbulent Viscosity Ratio as the
Specification Method.
Reynolds-Stress Specification Method
specifies which method will be used to determine the backflow Reynolds stress boundary conditions when the Reynolds stress turbulence model is used. You can choose either
K or Turbulence Intensity or
Reynolds-Stress Components. If you choose the former,
ANSYS FLUENT will compute the Reynolds stresses for you. If you choose the latter, you will explicitly specify the Reynolds stresses yourself. See Section
12.14.3 for details. (This item will appear only for RSM turbulent flow calculations.)
Backflow UU,VV,WW,UV,VW,UW Reynolds Stresses
specify the backflow Reynolds stress components when
Reynolds-Stress Components is chosen as the
Reynolds-Stress Specification Method.
Thermal
contains the thermal parameters.
Backflow Total Temperature
sets the total temperature of the inflow stream should the flow reverse direction
Radiation
contains the radiation parameters.
Participates in Solar Ray Tracing
specifies whether or not outlet vent participate in solar ray tracing.
External Black Body Temperature Method, Internal Emissivity
set the radiation boundary conditions when you are using the P-1 model, the DTRM, the discrete ordinates model, or the S2S model for radiation heat transfer. See Section
13.3.6 for details.
Species
contains the species parameters.
Specify Species in Mole Fractions
allows you to specify the species in mole fractions rather than mass fractions.
Mean Mixture Fraction, Mixture Fraction Variance
set inlet values for the PDF mixture fraction and its variance. (These items will appear only if you are using the non-premixed or partially premixed combustion model.)
Secondary Mean Mixture Fraction, Secondary Mixture Fraction Variance
set inlet values for the secondary mixture fraction and its variance. (These items will appear only if you are using the non-premixed or partially premixed combustion model with two mixture fractions.)
Species Mass Fractions
contains inputs for the mass fractions of defined species. See Section
15.1.5 for details about these inputs. These items will appear only if you are modeling non-reacting multi-species flow or you are using the finite-rate reaction formulation.
Backflow Progress Variable
sets the value of the progress variable for premixed turbulent combustion. See Section
17.3.3 for details.
This item will appear only if the premixed or partially premixed combustion model is used.
DPM
contains the discrete phase parameters.
Discrete Phase BC Type
sets the way that the discrete phase behaves with respect to the boundary. This item appears when one or more injections have been defined.
reflect
rebounds the particle off the boundary with a change in its momentum as defined by the coefficient of restitution. (See Figure
23.4.1.)
trap
terminates the trajectory calculations and records the fate of the particle as "trapped''. In the case of evaporating droplets, their entire mass instantaneously passes into the vapor phase and enters the cell adjacent to the boundary. See Figure
23.4.2.
escape
reports the particle as having "escaped'' when it encounters the boundary. Trajectory calculations are terminated. See Figure
23.4.3.
wall-jet
indicates that the direction and velocity of the droplet particles are given by the resulting momentum flux, which is a function of the impingement angle. See Figure
15.6.1TH-dpm-disp-bound-walljet in the separate
Theory Guide.
wall-film
consists of four regimes: stick, rebound, spread, and splash, which are based on the impact energy and wall temperature. Detailed information on the wall-film model can be found in
this section in the separate
Theory Guide. The
Number Of Splashed Drops must be specified.
user-defined
specifies a user-defined function to define the discrete phase boundary condition type.
Discrete Phase BC Function
sets the user-defined function from the drop-down list.
Multiphase
contains the multiphase parameters.
Backflow Granular Temperature
specifies temperature for the solids phase and is proportional to the kinetic energy of the random motion of the particles.
Backflow Volume Fraction
specifies the volume fraction of the secondary phase selected in the
Boundary Conditions task page. This section of the dialog box will appear when one of the multiphase models is being used. See Section
24.2.9 for details.
UDS
contains the UDS parameters.
User-Defined Scalar Boundary Condition
appears only if user defines scalars are specified.
User Scalar-n
specifies the whether the scalar is a specified flux or a specified value.
User-Defined Scalar Boundary Value
appears only if user defines scalars are specified.