abbas
posted this
19 February 2019

Thanks for your help.

# State file created: 2019/02/19 156:28

# Build 19.3 2018-11-16T2336.098000

LIBRARY:

MATERIAL: CO2

Binary Material1 = CO2L

Binary Material2 = CO2V

Material Group = User

Option = Homogeneous Binary Mixture

SATURATION PROPERTIES:

Component Name = CO2V

Option = Table

Table Format = TASCflow RGP

Table Name = Dcfx/CO2-high.rgp

END

END

MATERIAL: CO2L

Material Group = User

Option = Pure Substance

Thermodynamic State = Liquid

PROPERTIES:

Component Name = CO2L

Option = Table

Table Format = TASCflow RGP

Table Name = Dcfx/CO2-high.rgp

END

END

MATERIAL: CO2V

Material Group = User

Option = Pure Substance

Thermodynamic State = Gas

PROPERTIES:

Component Name = CO2V

Option = Table

Table Format = TASCflow RGP

Table Name = Dcfx/CO2-high.rgp

END

END

END

FLOW: Flow Analysis 1

SOLUTION UNITS:

Angle Units = [rad]

Length Units = [m]

Mass Units = [kg]

Solid Angle Units = [sr]

Temperature Units = [K]

Time Units = [s]

END

ANALYSIS TYPE:

Option = Steady State

EXTERNAL SOLVER COUPLING:

Option = None

END

END

DOMAIN: Default Domain

Coord Frame = Coord 0

Domain Type = Fluid

Location = SOLID

BOUNDARY: Default Domain Default

Boundary Type = WALL

Location = WALL

BOUNDARY CONDITIONS:

HEAT TRANSFER:

Option = Adiabatic

END

MASS AND MOMENTUM:

Option = No Slip Wall

END

WALL ROUGHNESS:

Option = Smooth Wall

END

END

END

BOUNDARY: OUT

Boundary Type = OUTLET

Location = OUT

BOUNDARY CONDITIONS:

FLOW REGIME:

Option = Subsonic

END

MASS AND MOMENTUM:

Option = Static Pressure

Relative Pressure = 0 [Pa]

END

END

END

BOUNDARY: inlet

Boundary Type = INLET

Location = IN

BOUNDARY CONDITIONS:

COMPONENT: CO2V

Mass Fraction = 1

Option = Mass Fraction

END

FLOW DIRECTION:

Option = Normal to Boundary Condition

END

FLOW REGIME:

Option = Subsonic

END

HEAT TRANSFER:

Option = Total Temperature

Total Temperature = 350 [K]

END

MASS AND MOMENTUM:

Option = Total Pressure

Relative Pressure = 0.5 [MPa]

END

TURBULENCE:

Option = Medium Intensity and Eddy Viscosity Ratio

END

END

END

DOMAIN MODELS:

BUOYANCY MODEL:

Option = Non Buoyant

END

DOMAIN MOTION:

Option = Stationary

END

MESH DEFORMATION:

Option = None

END

REFERENCE PRESSURE:

Reference Pressure = 7.5 [MPa]

END

END

FLUID DEFINITION: Fluid 1

Material = CO2

Option = Material Library

MORPHOLOGY:

Option = Continuous Fluid

END

END

FLUID MODELS:

COMBUSTION MODEL:

Option = None

END

COMPONENT: CO2L

Option = Equilibrium Constraint

END

COMPONENT: CO2V

Option = Equilibrium Fraction

END

HEAT TRANSFER MODEL:

Include Viscous Work Term = True

Option = Total Energy

END

THERMAL RADIATION MODEL:

Option = None

END

TURBULENCE MODEL:

Option = k epsilon

END

TURBULENT WALL FUNCTIONS:

High Speed Model = Off

Option = Scalable

END

END

END

OUTPUT CONTROL:

RESULTS:

File Compression Level = Default

Option = Standard

END

END

SOLVER CONTROL:

Turbulence Numerics = First Order

ADVECTION SCHEME:

Option = High Resolution

END

CONVERGENCE CONTROL:

Length Scale Option = Conservative

Maximum Number of Iterations = 100

Minimum Number of Iterations = 1

Timescale Control = Auto Timescale

Timescale Factor = 1.0

END

CONVERGENCE CRITERIA:

Residual Target = 1.E-4

Residual Type = RMS

END

DYNAMIC MODEL CONTROL:

Global Dynamic Model Control = On

END

END

END

COMMAND FILE:

Version = 19.3

END

Best regards,

Abbas