This Run of the CFX Release 17.0 Solver Started at 12:11:01 on 28 Apr

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

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

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

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

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

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

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

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

WALL ROUGHNESS:

Option = Smooth Wall

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

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

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

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

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

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

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

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

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

FLUID DEFINITION: Air Ideal Gas

Material = Air Ideal Gas

Option = Material Library

MORPHOLOGY:

Option = Continuous Fluid

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

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

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

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

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

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

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

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

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

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

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

FLUID DEFINITION: Air Ideal Gas

Material = Air Ideal Gas

Option = Material Library

MORPHOLOGY:

Option = Continuous Fluid

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

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

PITCH CHANGE:

Option = None

END

MESH CONNECTION:

Option = Automatic

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

PITCH CHANGE:

Option = None

END

MESH CONNECTION:

Option = GGI

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

PITCH CHANGE:

Option = None

END

MESH CONNECTION:

Option = GGI

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

MESH CONNECTION:

Option = GGI

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

PITCH CHANGE:

Option = Automatic

END

MESH CONNECTION:

Option = GGI

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

PITCH CHANGE:

Option = None

END

MESH CONNECTION:

Option = Automatic

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

MESH CONNECTION:

Option = GGI

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

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

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

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

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

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

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

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

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

SOLVER STEP CONTROL:

Runtime Priority = Standard

MEMORY CONTROL:

Memory Allocation Factor = 1.0

END

PARALLEL ENVIRONMENT:

Number of Processes = 1

Start Method = Serial

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 |

| |

| 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) |

+------+

------+------+------+------+------+------

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) |

+------+

+------+------+------+------+

| 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 |