This run of the CFX Release 17.0 Solver started at 12:11:01 on 28 Apr
2016 by user A.Chernomazov on WS-NT-02 (intel_xeon64.sse2_winnt) using
the command:
"C:\Program Files\ANSYS Inc\v170\CFX\bin\perllib\cfx5solve.pl"
-stdout-comms -batch -ccl -
Release 17.0
Point Releases and Patches installed:
ANSYS, Inc. Products Release 17.0
ANSYS Mechanical Products Release 17.0
ANSYS Autodyn Release 17.0
ANSYS LS-DYNA Release 17.0
ANSYS AIM Release 17.0
ANSYS CFX (includes ANSYS CFD-Post) Release 17.0
ANSYS Fluent (includes ANSYS CFD-Post) Release 17.0
ANSYS TurboGrid Release 17.0
ANSYS Polyflow (includes ANSYS CFD-Post) Release 17.0
ANSYS Forte Release 17.0
ANSYS ICEM CFD Release 17.0
ANSYS Aqwa Release 17.0
ANSYS Composite PrepPost Release 17.0
ANSYS Icepak (includes ANSYS CFD-Post) Release 17.0
AutoCAD Release 17.0
ACIS Release 17.0
Catia, Version 4 Release 17.0
Catia, Version 6 Release 17.0
Creo Elements/Direct Modeling Release 17.0
Inventor Release 17.0
JTOpen Release 17.0
NX Release 17.0
Parasolid Release 17.0
Creo Parametric (formerly Pro/ENGINEER) Release 17.0
Solid Edge Release 17.0
SolidWorks Release 17.0
ANSYS, Inc. License Manager Release 17.0
ANSYS Customization Files for User Programmable Features Release 17.0
ANSYS CFD-Post only Release 17.0
Catia, Version 5 Release 17.0
Setting up CFX Solver run ...
+------+
| |
| CFX Command Language for Run |
| |
+------+
LIBRARY:
MATERIAL: Air Ideal Gas
Material Description = Air Ideal Gas (constant Cp)
Material Group = Air Data, Calorically Perfect Ideal Gases
Option = Pure Substance
Thermodynamic State = Gas
PROPERTIES:
Option = General Material
EQUATION OF STATE:
Molar Mass = 28.96 [kg kmol^-1]
Option = Ideal Gas
END
SPECIFIC HEAT CAPACITY:
Option = Value
Specific Heat Capacity = 1.0044E+03 [J kg^-1 K^-1]
Specific Heat Type = Constant Pressure
END
REFERENCE STATE:
Option = Specified Point
Reference Pressure = 1 [atm]
Reference Specific Enthalpy = 0. [J/kg]
Reference Specific Entropy = 0. [J/kg/K]
Reference Temperature = 25 [C]
END
DYNAMIC VISCOSITY:
Dynamic Viscosity = 1.831E-05 [kg m^-1 s^-1]
Option = Value
END
THERMAL CONDUCTIVITY:
Option = Value
Thermal Conductivity = 2.61E-2 [W m^-1 K^-1]
END
ABSORPTION COEFFICIENT:
Absorption Coefficient = 0.01 [m^-1]
Option = Value
END
SCATTERING COEFFICIENT:
Option = Value
Scattering Coefficient = 0.0 [m^-1]
END
REFRACTIVE INDEX:
Option = Value
Refractive Index = 1.0 [m m^-1]
END
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 = Transient Blade Row
EXTERNAL SOLVER COUPLING:
Option = None
END
INITIAL TIME:
Option = Automatic with Value
Time = 0 [s]
END
END
DOMAIN: R1
Coord Frame = Coord 0
Domain Type = Fluid
Location = Entire Passage 2
BOUNDARY: R1 Blade
Boundary Type = WALL
Frame Type = Rotating
Location = BLADE 2,BLADE 2 2
BOUNDARY CONDITIONS:
HEAT TRANSFER:
Option = Adiabatic
END
MASS AND MOMENTUM:
Option = No Slip Wall
END
WALL ROUGHNESS:
Option = Smooth Wall
END
END
END
BOUNDARY: R1 Hub
Boundary Type = WALL
Coord Frame = Coord 0
Frame Type = Rotating
Location = HUB 2,HUB 2 2
BOUNDARY CONDITIONS:
HEAT TRANSFER:
Option = Adiabatic
END
MASS AND MOMENTUM:
Option = No Slip Wall
END
WALL ROUGHNESS:
Option = Smooth Wall
END
END
END
BOUNDARY: R1 Internal Interface 1 Side 1
Boundary Type = INTERFACE
Location = PER1 2 2
BOUNDARY CONDITIONS:
HEAT TRANSFER:
Option = Conservative Interface Flux
END
MASS AND MOMENTUM:
Option = Conservative Interface Flux
END
TURBULENCE:
Option = Conservative Interface Flux
END
END
END
BOUNDARY: R1 Internal Interface 1 Side 2
Boundary Type = INTERFACE
Location = PER2 2
BOUNDARY CONDITIONS:
HEAT TRANSFER:
Option = Conservative Interface Flux
END
MASS AND MOMENTUM:
Option = Conservative Interface Flux
END
TURBULENCE:
Option = Conservative Interface Flux
END
END
END
BOUNDARY: R1 Outlet
Boundary Type = OUTLET
Frame Type = Stationary
Location = OUTFLOW 2,OUTFLOW 2 2
BOUNDARY CONDITIONS:
FLOW REGIME:
Option = Subsonic
END
MASS AND MOMENTUM:
Normal Speed = 185 [m s^-1]
Option = Normal Speed
END
END
END
BOUNDARY: R1 Shroud
Boundary Type = WALL
Coord Frame = Coord 0
Frame Type = Rotating
Location = SHROUD 2,SHROUD 2 2
BOUNDARY CONDITIONS:
HEAT TRANSFER:
Option = Adiabatic
END
MASS AND MOMENTUM:
Option = No Slip Wall
WALL VELOCITY:
Option = Counter Rotating Wall
END
END
WALL ROUGHNESS:
Option = Smooth Wall
END
END
END
BOUNDARY: R1 to R1 Internal 2 Side 1
Boundary Type = INTERFACE
Location = SHROUD TIP GGI SIDE 1 2
BOUNDARY CONDITIONS:
HEAT TRANSFER:
Option = Conservative Interface Flux
END
MASS AND MOMENTUM:
Option = Conservative Interface Flux
END
TURBULENCE:
Option = Conservative Interface Flux
END
END
END
BOUNDARY: R1 to R1 Internal 2 Side 2
Boundary Type = INTERFACE
Location = SHROUD TIP GGI SIDE 2 2
BOUNDARY CONDITIONS:
HEAT TRANSFER:
Option = Conservative Interface Flux
END
MASS AND MOMENTUM:
Option = Conservative Interface Flux
END
TURBULENCE:
Option = Conservative Interface Flux
END
END
END
BOUNDARY: R1 to R1 Internal Side 1
Boundary Type = INTERFACE
Location = SHROUD TIP GGI SIDE 1
BOUNDARY CONDITIONS:
HEAT TRANSFER:
Option = Conservative Interface Flux
END
MASS AND MOMENTUM:
Option = Conservative Interface Flux
END
TURBULENCE:
Option = Conservative Interface Flux
END
END
END
BOUNDARY: R1 to R1 Internal Side 2
Boundary Type = INTERFACE
Location = SHROUD TIP GGI SIDE 2
BOUNDARY CONDITIONS:
HEAT TRANSFER:
Option = Conservative Interface Flux
END
MASS AND MOMENTUM:
Option = Conservative Interface Flux
END
TURBULENCE:
Option = Conservative Interface Flux
END
END
END
BOUNDARY: R1 to R1 Periodic 1 Side 1
Boundary Type = INTERFACE
Location = PER1 2
BOUNDARY CONDITIONS:
HEAT TRANSFER:
Option = Conservative Interface Flux
END
MASS AND MOMENTUM:
Option = Conservative Interface Flux
END
TURBULENCE:
Option = Conservative Interface Flux
END
END
END
BOUNDARY: R1 to R1 Periodic 1 Side 2
Boundary Type = INTERFACE
Location = PER2 2 2
BOUNDARY CONDITIONS:
HEAT TRANSFER:
Option = Conservative Interface Flux
END
MASS AND MOMENTUM:
Option = Conservative Interface Flux
END
TURBULENCE:
Option = Conservative Interface Flux
END
END
END
BOUNDARY: R1 to S1 Side 1
Boundary Type = INTERFACE
Location = INFLOW 2,INFLOW 2 2
BOUNDARY CONDITIONS:
HEAT TRANSFER:
Option = Conservative Interface Flux
END
MASS AND MOMENTUM:
Option = Conservative Interface Flux
END
TURBULENCE:
Option = Conservative Interface Flux
END
END
END
DOMAIN MODELS:
BUOYANCY MODEL:
Option = Non Buoyant
END
DOMAIN MOTION:
Alternate Rotation Model = true
Angular Velocity = 41500 [rev min^-1]
Option = Rotating
AXIS DEFINITION:
Option = Coordinate Axis
Rotation Axis = Coord 0.3
END
END
MESH DEFORMATION:
Option = None
END
PASSAGE DEFINITION:
Number of Passages in 360 = 16
Number of Passages in Component = 2
END
REFERENCE PRESSURE:
Reference Pressure = 0 [atm]
END
END
FLUID DEFINITION: Air Ideal Gas
Material = Air Ideal Gas
Option = Material Library
MORPHOLOGY:
Option = Continuous Fluid
END
END
FLUID MODELS:
COMBUSTION MODEL:
Option = None
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
DOMAIN: S1
Coord Frame = Coord 0
Domain Type = Fluid
Location = Entire Passage
BOUNDARY: R1 to S1 Side 2
Boundary Type = INTERFACE
Location = OUTFLOW,OUTFLOW 3
BOUNDARY CONDITIONS:
HEAT TRANSFER:
Option = Conservative Interface Flux
END
MASS AND MOMENTUM:
Option = Conservative Interface Flux
END
TURBULENCE:
Option = Conservative Interface Flux
END
END
END
BOUNDARY: S1 Blade
Boundary Type = WALL
Location = BLADE,BLADE 3
BOUNDARY CONDITIONS:
HEAT TRANSFER:
Option = Adiabatic
END
MASS AND MOMENTUM:
Option = No Slip Wall
END
WALL ROUGHNESS:
Option = Smooth Wall
END
END
END
BOUNDARY: S1 Hub
Boundary Type = WALL
Location = HUB,HUB 3
BOUNDARY CONDITIONS:
HEAT TRANSFER:
Option = Adiabatic
END
MASS AND MOMENTUM:
Option = No Slip Wall
END
WALL ROUGHNESS:
Option = Smooth Wall
END
END
END
BOUNDARY: S1 Inlet
Boundary Type = INLET
Location = INFLOW,INFLOW 3
BOUNDARY CONDITIONS:
FLOW REGIME:
Blend Mach Number Type = Normal Speed
Option = Mixed
END
HEAT TRANSFER:
Option = Total Temperature
Total Temperature = 1273 [K]
END
MASS AND MOMENTUM:
Normal Speed = 177 [m s^-1]
Option = Normal Speed and Total Pressure
Relative Total Pressure = 693000 [Pa]
END
TURBULENCE:
Option = Medium Intensity and Eddy Viscosity Ratio
END
END
END
BOUNDARY: S1 Internal Interface 2 Side 1
Boundary Type = INTERFACE
Location = PER1 3
BOUNDARY CONDITIONS:
HEAT TRANSFER:
Option = Conservative Interface Flux
END
MASS AND MOMENTUM:
Option = Conservative Interface Flux
END
TURBULENCE:
Option = Conservative Interface Flux
END
END
END
BOUNDARY: S1 Internal Interface 2 Side 2
Boundary Type = INTERFACE
Location = PER2
BOUNDARY CONDITIONS:
HEAT TRANSFER:
Option = Conservative Interface Flux
END
MASS AND MOMENTUM:
Option = Conservative Interface Flux
END
TURBULENCE:
Option = Conservative Interface Flux
END
END
END
BOUNDARY: S1 Shroud
Boundary Type = WALL
Location = SHROUD,SHROUD 3
BOUNDARY CONDITIONS:
HEAT TRANSFER:
Option = Adiabatic
END
MASS AND MOMENTUM:
Option = No Slip Wall
END
WALL ROUGHNESS:
Option = Smooth Wall
END
END
END
BOUNDARY: S1 to S1 Periodic 1 Side 1
Boundary Type = INTERFACE
Location = PER1
BOUNDARY CONDITIONS:
HEAT TRANSFER:
Option = Conservative Interface Flux
END
MASS AND MOMENTUM:
Option = Conservative Interface Flux
END
TURBULENCE:
Option = Conservative Interface Flux
END
END
END
BOUNDARY: S1 to S1 Periodic 1 Side 2
Boundary Type = INTERFACE
Location = PER2 3
BOUNDARY CONDITIONS:
HEAT TRANSFER:
Option = Conservative Interface Flux
END
MASS AND MOMENTUM:
Option = Conservative Interface Flux
END
TURBULENCE:
Option = Conservative Interface Flux
END
END
END
DOMAIN MODELS:
BUOYANCY MODEL:
Option = Non Buoyant
END
DOMAIN MOTION:
Option = Stationary
END
MESH DEFORMATION:
Option = None
END
PASSAGE DEFINITION:
Number of Passages in 360 = 14
Number of Passages in Component = 2
END
REFERENCE PRESSURE:
Reference Pressure = 0 [atm]
END
END
FLUID DEFINITION: Air Ideal Gas
Material = Air Ideal Gas
Option = Material Library
MORPHOLOGY:
Option = Continuous Fluid
END
END
FLUID MODELS:
COMBUSTION MODEL:
Option = None
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
DOMAIN INTERFACE: R1 Internal Interface 1
Boundary List1 = R1 Internal Interface 1 Side 1
Boundary List2 = R1 Internal Interface 1 Side 2
Interface Type = Fluid Fluid
INTERFACE MODELS:
Option = General Connection
FRAME CHANGE:
Option = None
END
MASS AND MOMENTUM:
Option = Conservative Interface Flux
MOMENTUM INTERFACE MODEL:
Option = None
END
END
PITCH CHANGE:
Option = None
END
END
MESH CONNECTION:
Option = Automatic
END
END
DOMAIN INTERFACE: R1 to R1 Internal
Boundary List1 = R1 to R1 Internal Side 1
Boundary List2 = R1 to R1 Internal Side 2
Interface Type = Fluid Fluid
INTERFACE MODELS:
Option = General Connection
FRAME CHANGE:
Option = None
END
MASS AND MOMENTUM:
Option = Conservative Interface Flux
MOMENTUM INTERFACE MODEL:
Option = None
END
END
PITCH CHANGE:
Option = None
END
END
MESH CONNECTION:
Option = GGI
END
END
DOMAIN INTERFACE: R1 to R1 Internal 2
Boundary List1 = R1 to R1 Internal 2 Side 1
Boundary List2 = R1 to R1 Internal 2 Side 2
Interface Type = Fluid Fluid
INTERFACE MODELS:
Option = General Connection
FRAME CHANGE:
Option = None
END
MASS AND MOMENTUM:
Option = Conservative Interface Flux
MOMENTUM INTERFACE MODEL:
Option = None
END
END
PITCH CHANGE:
Option = None
END
END
MESH CONNECTION:
Option = GGI
END
END
DOMAIN INTERFACE: R1 to R1 Periodic 1
Boundary List1 = R1 to R1 Periodic 1 Side 1
Boundary List2 = R1 to R1 Periodic 1 Side 2
Interface Type = Fluid Fluid
INTERFACE MODELS:
Option = Rotational Periodicity
AXIS DEFINITION:
Option = Coordinate Axis
Rotation Axis = Coord 0.3
END
END
MESH CONNECTION:
Option = GGI
END
END
DOMAIN INTERFACE: R1 to S1
Boundary List1 = R1 to S1 Side 1
Boundary List2 = R1 to S1 Side 2
Interface Type = Fluid Fluid
INTERFACE MODELS:
Option = General Connection
FRAME CHANGE:
Option = Transient Rotor Stator
END
MASS AND MOMENTUM:
Option = Conservative Interface Flux
MOMENTUM INTERFACE MODEL:
Option = None
END
END
PITCH CHANGE:
Option = Automatic
END
END
MESH CONNECTION:
Option = GGI
END
END
DOMAIN INTERFACE: S1 Internal Interface 2
Boundary List1 = S1 Internal Interface 2 Side 1
Boundary List2 = S1 Internal Interface 2 Side 2
Interface Type = Fluid Fluid
INTERFACE MODELS:
Option = General Connection
FRAME CHANGE:
Option = None
END
MASS AND MOMENTUM:
Option = Conservative Interface Flux
MOMENTUM INTERFACE MODEL:
Option = None
END
END
PITCH CHANGE:
Option = None
END
END
MESH CONNECTION:
Option = Automatic
END
END
DOMAIN INTERFACE: S1 to S1 Periodic 1
Boundary List1 = S1 to S1 Periodic 1 Side 1
Boundary List2 = S1 to S1 Periodic 1 Side 2
Interface Type = Fluid Fluid
INTERFACE MODELS:
Option = Rotational Periodicity
AXIS DEFINITION:
Option = Coordinate Axis
Rotation Axis = Coord 0.3
END
END
MESH CONNECTION:
Option = GGI
END
END
OUTPUT CONTROL:
MONITOR OBJECTS:
EFFICIENCY OUTPUT:
Efficiency Calculation Method = Total to Total
Efficiency Type = Both Compression and Expansion
Inflow Boundary = S1 Inlet
Option = Output To Solver Monitor
Outflow Boundary = R1 Outlet
END
MONITOR BALANCES:
Option = Full
END
MONITOR FORCES:
Option = Full
END
MONITOR PARTICLES:
Option = Full
END
MONITOR RESIDUALS:
Option = Full
END
MONITOR TOTALS:
Option = Full
END
END
RESULTS:
File Compression Level = Default
Option = Standard
END
TRANSIENT BLADE ROW OUTPUT:
File Compression Level = Default
Option = Selected Variables
Output Variables List = Pressure,Velocity
DATA COMPRESSION:
Number of Fourier Coefficients = 7
Option = Fourier Series
Start Accumulation Period = Moving Averages
END
END
END
SOLVER CONTROL:
Turbulence Numerics = First Order
ADVECTION SCHEME:
Option = High Resolution
END
CONVERGENCE CONTROL:
Maximum Number of Coefficient Loops = 10
Minimum Number of Coefficient Loops = 1
Timescale Control = Coefficient Loops
END
CONVERGENCE CRITERIA:
Residual Target = 1.E-4
Residual Type = RMS
END
TRANSIENT SCHEME:
Option = Second Order Backward Euler
TIMESTEP INITIALISATION:
Option = Automatic
END
END
END
TRANSIENT BLADE ROW MODELS:
Option = Fourier Transformation
FOURIER TRANSFORMATION: Fourier Transformation 1
Domain Interface = R1 to S1
Option = Rotor Stator
FOURIER TRANSFORMATION SIDE 1:
Option = Phase Corrected
Phase Corrected Interface = R1 to R1 Periodic 1
Sampling Domain Interface = R1 Internal Interface 1
END
FOURIER TRANSFORMATION SIDE 2:
Option = None
END
END
TRANSIENT METHOD:
Option = Time Integration
TIME DURATION:
Number of Periods per Run = 15
Option = Number of Periods per Run
END
TIME PERIOD:
Computed Passing Period = 0.00010327[s]
Domain = S1
Minimum Number of Timesteps per Period = 8
Option = Automatic
END
TIME STEPS:
Computed Timestep = 6.45438e-006[s]
Option = Timestep Multiplier
Timestep Multiplier = 2
END
END
END
END
COMMAND FILE:
Version = 17.0
Results Version = 17.0
END
SIMULATION CONTROL:
EXECUTION CONTROL:
EXECUTABLE SELECTION:
Double Precision = No
Large Problem = No
END
INTERPOLATOR STEP CONTROL:
Runtime Priority = Standard
MEMORY CONTROL:
Memory Allocation Factor = 1.0
END
END
PARALLEL HOST LIBRARY:
HOST DEFINITION: wsnt02
Remote Host Name = WS-NT-02
Host Architecture String = winnt-amd64
Installation Root = C:\Program Files\ANSYS Inc\v%v\CFX
END
END
PARTITIONER STEP CONTROL:
Multidomain Option = Automatic
Runtime Priority = Standard
MEMORY CONTROL:
Memory Allocation Factor = 1.0
END
PARTITION SMOOTHING:
Maximum Partition Smoothing Sweeps = 100
Option = Smooth
END
PARTITIONING TYPE:
MeTiS Type = k-way
Option = MeTiS
Partition Size Rule = Automatic
END
END
RUN DEFINITION:
Run Mode = Full
Solver Input File = \
D:\PROJECT_04\04_Cases\1st_State_TBR_FT\1st_stage_TBR_FT_.def
Solver Results File = \
D:\PROJECT_04\04_Cases\1st_State_TBR_FT\1st_stage_TBR_FT__002.res
INITIAL VALUES SPECIFICATION:
INITIAL VALUES CONTROL:
Use Mesh From = Solver Input File
END
INITIAL VALUES: Initial Values 1
File Name = \
D:/PROJECT_04/04_Cases/1st_Stage_SST/1st_stage_ST__001.res
Option = Results File
END
END
END
SOLVER STEP CONTROL:
Runtime Priority = Standard
MEMORY CONTROL:
Memory Allocation Factor = 1.0
END
PARALLEL ENVIRONMENT:
Number of Processes = 1
Start Method = Serial
END
END
END
END
+------+
| |
| Interpolation of Initial Values |
| |
+------+
+------+
| |
| ANSYS(R) CFX(R) Interpolator |
| |
| Release 17.0 |
| Build 17.0 2015.11.30-15.46-135354 |
| Mon Nov 30 15:53:59 GMTST 2015 |
| |
| Executable Attributes |
| |
| single-64bit-int32-archfort-optimised-noprof-lcomp |
| |
| (C) 2015 ANSYS, Inc. |
| |
| All rights reserved. Unauthorized use, distribution or duplication |
| is prohibited. This product is subject to U.S. laws governing |
| export and re-export. For full Legal Notice, see documentation. |
+------+
+------+
| Job Information at Start of Run |
+------+
Run mode: serial run
Host computer: WS-NT-02 (PID:9028)
Job started: Thu Apr 28 12:11:03 2016
+------+
| Memory Allocated for Run (Actual usage may be less) |
+------+
| Real | Integer | Character | Logical | Double
------+------+------+------+------+------
Mwords | 39.39 | 29.54 | 0.20 | 0.01 | 0.30
Mbytes | 150.26 | 112.69 | 0.19 | 0.04 | 2.29
------+------+------+------+------+------
+------+
| Host Memory Information (Mbytes) |
+------+
| Host | System | Allocated | % |
+------+------+------+------+
| WS-NT-02 | 8124.02 | 265.47 | 3.27 |
+------+------+------+------+
======
Interpolating Onto Domain "R1"
======
Total Number of Nodes in the Target Domain = 1203684
Bounding Box Volume of the Target Mesh = 1.00857E-04
Checking all source domains from the source file:
Target mesh is different from domain "R1".
Target domain motion is different from domain "S1".
Searching for Candidate Source Domains:
Domain "R1"
Number of Mapped Nodes = 607722 ( 50.5%)
Bounding Box Overlap Volume = 6.16408E-05 ( 61.1%)
Setting Up Unmapped Nodes:
Number of Unmapped Nodes = 595962 ( 49.5%)
Start interpolation of variables:
Source Domain Name Mapped Nodes
R1 607722 ( 50.5%)
Note: Some candidate domains may not be used.
+------+
| Variable Range Information |
+------+
+------+
| Variable Name | min | max |
+------+
| Isothermal Compressibility | 1.75E-06 | 4.98E-06 |
| Thermal Conductivity | 2.61E-02 | 2.61E-02 |
| Courant Number | 8.69E-02 | 1.31E+03 |
| Density | 5.99E-01 | 1.65E+00 |
| Density Derivative wrt Pressure at Constant| 2.63E-06 | 3.60E-06 |
| Static Enthalpy | 6.72E+05 | 1.03E+06 |
| Rothalpy | 8.38E+05 | 9.80E+05 |
| Total Enthalpy | 8.78E+05 | 1.05E+06 |
| Static Entropy | 9.03E+02 | 1.17E+03 |
| Pressure | 2.01E+05 | 5.73E+05 |
| Rotational Energy | 2.97E+04 | 6.74E+04 |
| Specific Heat Capacity at Constant Pressure| 1.00E+03 | 1.00E+03 |
| Turbulence Eddy Dissipation | 3.09E+04 | 3.84E+10 |