CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Software User Forums > ANSYS > CFX

Pressure distribution on a wall

Register Blogs Members List Search Today's Posts Mark Forums Read

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   October 26, 2013, 09:35
Default Pressure distribution on a wall
  #1
New Member
 
Darázs Bence
Join Date: Feb 2013
Posts: 16
Rep Power: 13
darazsbence is on a distinguished road
Hello Everyone,

I'd like to display the pressure distribution along a wall. How can i do this? I want to make a chart and not a contour plot, the x axis would be the angle from 0 to 360 degrees and the y axis the pressure.

Thank you guys in advance
darazsbence is offline   Reply With Quote

Old   October 27, 2013, 05:22
Default
  #2
Super Moderator
 
Glenn Horrocks
Join Date: Mar 2009
Location: Sydney, Australia
Posts: 17,830
Rep Power: 144
ghorrocks is just really niceghorrocks is just really niceghorrocks is just really niceghorrocks is just really nice
Pressure distribution on a wall - just plot pressure on the wall object.

You want to make a chart? If x is rotation angle - angle from what? Averaged or sampled how?
ghorrocks is offline   Reply With Quote

Old   October 3, 2015, 04:14
Default
  #3
Member
 
Attique Javaid
Join Date: Apr 2015
Location: Pakistan
Posts: 66
Rep Power: 11
attiquejavaid08 is on a distinguished road
My objective is to get pressure distribution over the wall. geometry is not axisymmetric. using k-epsilon with scalable wall function. system is at high pressure and temperature and i'm using average flow properties for a range. just before where it's crashing, i stopped the run and got this:




Looking at v-mom imbalance and specifically monitoring the boundary flow variables at blockage, i couldn't understand that why i'm getting this issue at this position. i've posted yplus contours and mesh of that region.

Kindly have a look at it please. I'll be thankful for your help.

regards,
AJ
attiquejavaid08 is offline   Reply With Quote

Old   October 3, 2015, 04:15
Default
  #4
Member
 
Attique Javaid
Join Date: Apr 2015
Location: Pakistan
Posts: 66
Rep Power: 11
attiquejavaid08 is on a distinguished road
Out file:
Setting up CFX Solver run ...

+--------------------------------------------------------------------+
| |
| CFX Command Language for Run |
| |
+--------------------------------------------------------------------+
LIBRARY:
MATERIAL: Water
Material Description = Water (liquid)
Material Group = Water Data,Constant Property Liquids
Option = Pure Substance
Thermodynamic State = Liquid
PROPERTIES:
Option = General Material
EQUATION OF STATE:
Density = 725.9386 [kg m^-3]
Molar Mass = 18.02 [kg kmol^-1]
Option = Value
END
SPECIFIC HEAT CAPACITY:
Option = Value
Specific Heat Capacity = 5468.89207 [J kg^-1 K^-1]
Specific Heat Type = Constant Pressure
END
REFERENCE STATE:
Option = Automatic
END
DYNAMIC VISCOSITY:
Dynamic Viscosity = 8.84E-05 [kg m^-1 s^-1]
Option = Value
END
THERMAL CONDUCTIVITY:
Option = Value
Thermal Conductivity = 0.561845291 [W m^-1 K^-1]
END
ABSORPTION COEFFICIENT:
Absorption Coefficient = 1.0 [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 = Steady State
EXTERNAL SOLVER COUPLING:
Option = None
END
END
DOMAIN: Default Domain
Coord Frame = Coord 0
Domain Type = Fluid
Location = UPPER_BLOCKING
BOUNDARY: block
Boundary Type = WALL
Location = BLOCKAGES
BOUNDARY CONDITIONS:
HEAT TRANSFER:
Option = Adiabatic
END
MASS AND MOMENTUM:
Option = No Slip Wall
END
WALL ROUGHNESS:
Option = Smooth Wall
END
END
END
BOUNDARY: in1
Boundary Type = INLET
Location = IN1
BOUNDARY CONDITIONS:
FLOW REGIME:
Option = Subsonic
END
HEAT TRANSFER:
Option = Static Temperature
Static Temperature = 228.5 [C]
END
MASS AND MOMENTUM:
Normal Speed = 23.9643 [m s^-1]
Option = Normal Speed
END
TURBULENCE:
Option = Medium Intensity and Eddy Viscosity Ratio
END
END
END
BOUNDARY: in2
Boundary Type = INLET
Location = IN2
BOUNDARY CONDITIONS:
FLOW REGIME:
Option = Subsonic
END
HEAT TRANSFER:
Option = Static Temperature
Static Temperature = 228.5 [C]
END
MASS AND MOMENTUM:
Normal Speed = 23.9643 [m s^-1]
Option = Normal Speed
END
TURBULENCE:
Option = Medium Intensity and Eddy Viscosity Ratio
END
END
END
BOUNDARY: inwall
Boundary Type = WALL
Location = INWALL
BOUNDARY CONDITIONS:
HEAT TRANSFER:
Option = Adiabatic
END
MASS AND MOMENTUM:
Option = No Slip Wall
END
WALL ROUGHNESS:
Option = Smooth Wall
END
END
END
BOUNDARY: outlet
Boundary Type = OUTLET
Location = OUTLET
BOUNDARY CONDITIONS:
FLOW REGIME:
Option = Subsonic
END
MASS AND MOMENTUM:
Option = Average Static Pressure
Pressure Profile Blend = 0.05
Relative Pressure = 0.08 [MPa]
END
PRESSURE AVERAGING:
Option = Average Over Whole Outlet
END
END
END
BOUNDARY: outwall
Boundary Type = WALL
Location = OUTWALL
BOUNDARY CONDITIONS:
HEAT TRANSFER:
Option = Adiabatic
END
MASS AND MOMENTUM:
Option = No Slip Wall
END
WALL ROUGHNESS:
Option = Smooth Wall
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 = 15 [MPa]
END
END
FLUID DEFINITION: Fluid 1
Material = Water
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
INITIALISATION:
Option = Automatic
INITIAL CONDITIONS:
Velocity Type = Cartesian
CARTESIAN VELOCITY COMPONENTS:
Option = Automatic
END
STATIC PRESSURE:
Option = Automatic
END
TEMPERATURE:
Option = Automatic
END
TURBULENCE INITIAL CONDITIONS:
Option = Medium Intensity and Eddy Viscosity Ratio
END
END
END
END
OUTPUT CONTROL:
RESULTS:
File Compression Level = Default
Option = Standard
END
END
SOLVER CONTROL:
Turbulence Numerics = First Order
ADVECTION SCHEME:
Blend Factor = 0.75
Option = Specified Blend Factor
END
CONVERGENCE CONTROL:
Local Timescale Factor = 1
Maximum Number of Iterations = 10000
Minimum Number of Iterations = 1
Timescale Control = Local Timescale Factor
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 = 16.2
Results Version = 16.2
END
SIMULATION CONTROL:
EXECUTION CONTROL:
EXECUTABLE SELECTION:
Double Precision = Yes
END
INTERPOLATOR STEP CONTROL:
Runtime Priority = Standard
MEMORY CONTROL:
Memory Allocation Factor = 1.0
END
END
PARALLEL HOST LIBRARY:
HOST DEFINITION: attiquepc
Remote Host Name = ATTIQUE-PC
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
EXECUTABLE SELECTION:
Use Large Problem Partitioner = Off
END
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
Partition Weight Factors = 0.25000, 0.25000, 0.25000, 0.25000
END
END
RUN DEFINITION:
Run Mode = Full
Solver Input File = C:\Users\attique\Desktop\New folder\100315-7.def
Solver Results File = C:\Users\attique\Desktop\New \
folder\100315-7_002.res
END
SOLVER STEP CONTROL:
Runtime Priority = Standard
MEMORY CONTROL:
Memory Allocation Factor = 1.0
END
PARALLEL ENVIRONMENT:
Number of Processes = 4
Start Method = Platform MPI Local Parallel
Parallel Host List = attiquepc*4
END
END
END
END

+--------------------------------------------------------------------+
| |
| Partitioning |
| |
+--------------------------------------------------------------------+


+--------------------------------------------------------------------+
| |
| ANSYS(R) CFX(R) Partitioner |
| |
| Release 16.2 |
| Build 16.2 2015.06.29-10.01-134376 |
| Mon Jun 29 11:05:17 GMTDT 2015 |
| |
| Executable Attributes |
| |
| double-64bit-int32-supfort-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: partitioning run
Host computer: ATTIQUE-PC (PID:5844)
Job started: Sat Oct 03 10:48:19 2015

+--------------------------------------------------------------------+
| Memory Allocated for Run (Actual usage may be less) |
+--------------------------------------------------------------------+
| Real | Integer | Character | Logical | Double
----------+------------+------------+-----------+----------+----------
Mwords | 6.09 | 50.56 | 3.31 | 0.12 | 0.00
Mbytes | 46.49 | 192.86 | 3.16 | 0.46 | 0.00
----------+------------+------------+-----------+----------+----------

+--------------------------------------------------------------------+
| Host Memory Information (Mbytes) |
+--------------------------------------------------------------------+
| Host | System | Allocated | % |
+-------------------------+----------------+----------------+--------+
| ATTIQUE-PC | 8135.03 | 242.97 | 2.99 |
+-------------------------+----------------+----------------+--------+
+--------------------------------------------------------------------+
| The MeTiS partitioning method allocates additional memory. |
| Total memory usage will therefore exceed the values shown above. |
+--------------------------------------------------------------------+
+--------------------------------------------------------------------+
| Mesh Statistics |
+--------------------------------------------------------------------+
Domain Name : Default Domain
Total Number of Nodes = 1214938
Total Number of Elements = 1175412
Total Number of Hexahedrons = 1175412
Total Number of Faces = 78144
+--------------------------------------------------------------------+
| Vertex Based Partitioning |
+--------------------------------------------------------------------+
Partitioning of domain: Default Domain
- Partitioning tool: MeTiS multilevel k-way algorithm
- Number of partitions: 4
- Number of graph-nodes: 1214938
- Number of graph-edges: 7209672
+--------------------------------------------------------------------+
| Iso-Partition Connection Statistics |
+--------------------------------------------------------------------+
| Domains in Group | | Vertices |
| | Smooth +---------+----------+----------+
| | Sweeps | Moves | <25% | <50% |
+---------------------------+--------+---------+----------+----------+
| Default Domain | 3 | 35 | 0 | 0 |
+---------------------------+--------+---------+----------+----------+
+--------------------------------------------------------------------+
| Partitioning Information |
+--------------------------------------------------------------------+
Partitioning information for domain: Default Domain
+------------------+------------------------+-----------------+
| Elements | Vertices | Faces |
+------+------------------+------------------------+-----------------+
| Part | Number % | Number % %Ovlp | Number % |
+------+------------------+------------------------+-----------------+
| Full | 1175412 | 1214938 | 78144 |
+------+------------------+------------------------+-----------------+
| 1 | 298379 25.0 | 312403 25.0 2.6 | 19834 25.1 |
| 2 | 298274 25.0 | 312524 25.0 2.7 | 19921 25.2 |
| 3 | 297233 24.9 | 311301 24.9 2.8 | 19356 24.5 |
| 4 | 297681 25.0 | 311990 25.0 2.7 | 19995 25.3 |
+------+------------------+------------------------+-----------------+
| Min | 297233 24.9 | 311301 24.9 2.6 | 19356 24.5 |
|(part)| ( 3)| ( 3 1)| ( 3)|
+------+------------------+------------------------+-----------------+
| Max | 298379 25.0 | 312524 25.0 2.8 | 19995 25.3 |
|(part)| ( 1)| ( 2 3)| ( 4)|
+------+------------------+------------------------+-----------------+
| Ave | 297892 25.0 | 312055 25.0 2.7 | 19777 25.0 |
+------+------------------+------------------------+-----------------+
| Sum | 1191567 100.0 | 1248218 100.0 | 79106 100.0 |
+------+------------------+------------------------+-----------------+
+--------------------------------------------------------------------+
| Partitioning CPU-Time Requirements |
+--------------------------------------------------------------------+

- Preparations 2.810E-01 seconds
- Low-level mesh partitioning 6.240E-01 seconds
- Global partitioning information 3.100E-02 seconds
- Element and face partitioning information 9.400E-02 seconds
- Vertex partitioning information 3.100E-02 seconds
- Partitioning Smoothing 3.120E-01 seconds
- Partitioning information compression 0.000E+00 seconds
- Summed CPU-time for mesh partitioning 1.404E+00 seconds
+--------------------------------------------------------------------+
| Job Information at End of Run |
+--------------------------------------------------------------------+
Host computer: ATTIQUE-PC (PID:5844)
Job finished: Sat Oct 03 10:48:21 2015
Total wall clock time: 1.982E+00 seconds
or: ( 0: 0: 0: 1.982 )
( Days: Hours: Minutes: Seconds )

+--------------------------------------------------------------------+
| |
| Solver |
| |
+--------------------------------------------------------------------+


+--------------------------------------------------------------------+
| |
| ANSYS(R) CFX(R) Solver |
| |
| Release 16.2 |
| Build 16.2 2015.06.29-10.01-134376 |
| Mon Jun 29 11:05:17 GMTDT 2015 |
| |
| Executable Attributes |
| |
| double-64bit-int32-supfort-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: parallel run (Platform MPI)
Job started: Sat Oct 03 10:48:21 2015
+--------------------------------------------------------------------+
| License Information |
+--------------------------------------------------------------------+

License Cap: ANSYS CFX Solver (> 512K Nodes)
License Cap: Parallel
License ID: attique-PC-attique-5548-009925

+--------------------------------------------------------------------+
| Memory Allocated for Run (Actual usage may be less) |
+--------------------------------------------------------------------+
Allocated storage in: Mwords
Mbytes
Partition | Real | Integer | Character | Logical | Double
----------+------------+------------+-----------+----------+----------
Minimum | 71.27 | 20.83 | 3.76 | 0.12 | 0.01
( 3) | 543.77 | 79.47 | 3.59 | 0.11 | 0.06
----------+------------+------------+-----------+----------+----------
Maximum | 71.63 | 20.92 | 3.76 | 0.12 | 0.01
( 1) | 546.53 | 79.81 | 3.59 | 0.11 | 0.06
----------+------------+------------+-----------+----------+----------
Average | 71.51 | 20.89 | 3.76 | 0.12 | 0.01
| 545.61 | 79.68 | 3.59 | 0.11 | 0.06
----------+------------+------------+-----------+----------+----------
Total | 286.06 | 83.56 | 15.04 | 0.48 | 0.03
| 2182.43 | 318.74 | 14.34 | 0.46 | 0.24
----------+------------+------------+-----------+----------+----------

+--------------------------------------------------------------------+
| Host Memory Information (Mbytes) |
+--------------------------------------------------------------------+
| Host | Npart | System | Allocated | % |
+------------------------+-------+-------------+-------------+-------+
| ATTIQUE-PC | 4 | 8135.03 | 2516.21 | 30.93 |
+------------------------+-------+-------------+-------------+-------+

+--------------------------------------------------------------------+
| ****** Notice ****** |
| The Wall Heat Transfer Coefficient written to the results file for |
| any turbulent phase with heat transfer is based on the turbulent |
| wall function coefficient. It is consistent with the Wall Heat Flux|
| the wall temperature, and the Wall Adjacent Temperature |
| (near-wall temperature). If you would like it to be based on a |
| user-specified bulk temperature instead, please set the expert |
| parameter "tbulk for htc = <value>". |
+--------------------------------------------------------------------+
+--------------------------------------------------------------------+
| Mesh Statistics |
+--------------------------------------------------------------------+
| Domain Name | Orthog. Angle | Exp. Factor | Aspect Ratio |
+----------------------+---------------+--------------+--------------+
| | Minimum [deg] | Maximum | Maximum |
+----------------------+---------------+--------------+--------------+
| Default Domain | 8.7 ! | 76 ! | 85383 ok |
+----------------------+---------------+--------------+--------------+
| | %! %ok %OK | %! %ok %OK | %! %ok %OK |
+----------------------+---------------+--------------+--------------+
| Default Domain | <1 4 96 | <1 3 97 | 0 10 90 |
+----------------------+---------------+--------------+--------------+
Domain Name : Default Domain
Total Number of Nodes = 1214938
Total Number of Elements = 1175412
Total Number of Hexahedrons = 1175412
Total Number of Faces = 78144
+--------------------------------------------------------------------+
| Average Scale Information |
+--------------------------------------------------------------------+
Domain Name : Default Domain
Global Length = 2.6095E+00
Minimum Extent = 5.8540E+00
Maximum Extent = 1.5531E+01
Density = 7.2594E+02
Dynamic Viscosity = 8.8400E-05
attiquejavaid08 is offline   Reply With Quote

Old   October 3, 2015, 04:17
Default
  #5
Member
 
Attique Javaid
Join Date: Apr 2015
Location: Pakistan
Posts: 66
Rep Power: 11
attiquejavaid08 is on a distinguished road
Velocity = 7.2832E+00
Advection Time = 3.5829E-01
Reynolds Number = 1.5607E+08
Thermal Conductivity = 5.6185E-01
Specific Heat Capacity at Constant Pressure = 5.4689E+03
Prandtl Number = 8.6047E-01
+--------------------------------------------------------------------+
| Checking for Isolated Fluid Regions |
+--------------------------------------------------------------------+

No isolated fluid regions were found.
+--------------------------------------------------------------------+
| The Equations Solved in This Calculation |
+--------------------------------------------------------------------+
Subsystem : Momentum and Mass
U-Mom
V-Mom
W-Mom
P-Mass
Subsystem : Heat Transfer
H-Energy
Subsystem : TurbKE and Diss.K
K-TurbKE
E-Diss.K

CFD Solver started: Sat Oct 03 10:48:31 2015

+--------------------------------------------------------------------+
| Convergence History |
+--------------------------------------------------------------------+
================================================== ====================
OUTER LOOP ITERATION = 1 CPU SECONDS = 3.887E+01
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| U-Mom | 0.00 | 1.2E-06 | 5.9E-05 | 1.6E+02 F |
| V-Mom | 0.00 | 6.7E-03 | 8.8E-02 | 6.4E-03 OK|
| W-Mom | 0.00 | 1.6E-06 | 3.4E-05 | 7.8E+01 F |
| P-Mass | 0.00 | 2.5E-04 | 1.0E-02 | 9.0 6.2E-01 ok|
+----------------------+------+---------+---------+------------------+
| H-Energy | 0.00 | 4.2E-04 | 5.0E-03 | 5.9 1.3E-05 OK|
+----------------------+------+---------+---------+------------------+
| K-TurbKE | 0.00 | 9.0E-02 | 1.3E+00 | 5.9 6.0E-11 OK|
| E-Diss.K | 0.00 | 5.3E-02 | 1.8E+00 | 7.7 2.0E-11 OK|
+----------------------+------+---------+---------+------------------+
================================================== ====================
OUTER LOOP ITERATION = 2 CPU SECONDS = 2.223E+02
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| U-Mom |99.99 | 8.0E-03 | 1.9E-01 | 1.8E-03 OK|
| V-Mom | 5.50 | 3.7E-02 | 2.8E-01 | 9.4E-04 OK|
| W-Mom |99.99 | 6.1E-03 | 1.3E-01 | 1.9E-03 OK|
| P-Mass | 0.48 | 1.2E-04 | 1.6E-02 | 33.1 8.5E-02 OK|
+----------------------+------+---------+---------+------------------+
| H-Energy |19.93 | 8.4E-03 | 3.8E-01 | 5.9 1.0E-06 OK|
+----------------------+------+---------+---------+------------------+
| K-TurbKE | 0.41 | 3.7E-02 | 1.3E+00 | 5.9 5.1E-08 OK|
| E-Diss.K | 0.62 | 3.3E-02 | 1.1E+00 | 8.1 7.1E-12 OK|
+----------------------+------+---------+---------+------------------+
================================================== ====================
OUTER LOOP ITERATION = 3 CPU SECONDS = 4.214E+02
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| U-Mom | 2.19 | 1.8E-02 | 4.2E-01 | 6.7E-04 OK|
| V-Mom | 1.09 | 4.0E-02 | 2.5E-01 | 2.1E-03 OK|
| W-Mom | 1.92 | 1.2E-02 | 3.0E-01 | 7.3E-04 OK|
| P-Mass | 2.33 | 2.8E-04 | 1.2E-02 | 29.1 8.0E-02 OK|
+----------------------+------+---------+---------+------------------+
| H-Energy | 1.61 | 1.3E-02 | 5.2E-01 | 6.2 2.9E-06 OK|
+----------------------+------+---------+---------+------------------+
| K-TurbKE | 0.80 | 3.0E-02 | 8.3E-01 | 6.2 2.8E-06 OK|
| E-Diss.K | 0.51 | 1.7E-02 | 5.1E-01 | 8.3 5.9E-11 OK|
+----------------------+------+---------+---------+------------------+
================================================== ====================
OUTER LOOP ITERATION = 4 CPU SECONDS = 6.151E+02
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| U-Mom | 1.12 | 2.0E-02 | 3.7E+00 | 1.0E-04 OK|
| V-Mom | 0.45 | 1.8E-02 | 1.3E-01 | 3.3E-04 OK|
| W-Mom | 0.86 | 1.0E-02 | 1.5E+00 | 1.1E-04 OK|
| P-Mass | 1.47 | 4.1E-04 | 2.8E-02 | 33.1 8.8E-02 OK|
+----------------------+------+---------+---------+------------------+
| H-Energy | 0.62 | 8.4E-03 | 2.0E-01 | 6.2 4.5E-06 OK|
+----------------------+------+---------+---------+------------------+
| K-TurbKE | 1.07 | 3.2E-02 | 8.8E-01 | 6.2 5.3E-06 OK|
| E-Diss.K | 0.43 | 7.3E-03 | 2.5E-01 | 8.5 2.5E-10 OK|
+----------------------+------+---------+---------+------------------+
================================================== ====================
OUTER LOOP ITERATION = 5 CPU SECONDS = 8.134E+02
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| U-Mom | 0.70 | 1.4E-02 | 2.2E-01 | 8.4E-04 OK|
| V-Mom | 0.36 | 6.4E-03 | 1.3E-01 | 2.8E-03 OK|
| W-Mom | 0.64 | 6.4E-03 | 9.8E-02 | 9.4E-04 OK|
| P-Mass | 0.94 | 3.9E-04 | 2.5E-02 | 25.1 4.4E-01 ok|
+----------------------+------+---------+---------+------------------+
| H-Energy | 0.63 | 5.3E-03 | 1.4E-01 | 6.2 3.8E-06 OK|
+----------------------+------+---------+---------+------------------+
| K-TurbKE | 0.90 | 2.9E-02 | 9.2E-01 | 6.2 8.2E-06 OK|
| E-Diss.K | 0.97 | 7.1E-03 | 2.4E-01 | 8.7 2.3E-09 OK|
+----------------------+------+---------+---------+------------------+
================================================== ====================
OUTER LOOP ITERATION = 6 CPU SECONDS = 1.002E+03
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| U-Mom | 0.63 | 8.5E-03 | 9.3E-02 | 1.3E-03 OK|
| V-Mom | 0.95 | 6.1E-03 | 1.0E-01 | 4.0E-03 OK|
| W-Mom | 0.67 | 4.3E-03 | 8.6E-02 | 1.2E-03 OK|
| P-Mass | 0.88 | 3.4E-04 | 1.9E-02 | 29.1 9.3E-02 OK|
+----------------------+------+---------+---------+------------------+
| H-Energy | 1.57 | 8.3E-03 | 2.5E-01 | 6.1 6.6E-06 OK|
+----------------------+------+---------+---------+------------------+
| K-TurbKE | 0.70 | 2.0E-02 | 8.8E-01 | 6.2 1.1E-05 OK|
| E-Diss.K | 1.68 | 1.2E-02 | 3.6E-01 | 7.4 1.1E-08 OK|
+----------------------+------+---------+---------+------------------+
================================================== ====================
OUTER LOOP ITERATION = 7 CPU SECONDS = 1.196E+03
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| U-Mom | 0.54 | 4.6E-03 | 1.1E-01 | 1.3E-03 OK|
| V-Mom | 0.97 | 6.0E-03 | 2.3E-01 | 3.5E-03 OK|
| W-Mom | 0.70 | 3.0E-03 | 9.4E-02 | 1.1E-03 OK|
| P-Mass | 0.44 | 1.5E-04 | 6.3E-03 | 33.1 9.1E-02 OK|
+----------------------+------+---------+---------+------------------+
| H-Energy | 1.21 | 1.0E-02 | 3.0E-01 | 6.1 8.7E-06 OK|
+----------------------+------+---------+---------+------------------+
| K-TurbKE | 0.70 | 1.4E-02 | 6.1E-01 | 6.1 1.4E-05 OK|
| E-Diss.K | 1.34 | 1.6E-02 | 6.8E-01 | 7.4 3.3E-08 OK|
+----------------------+------+---------+---------+------------------+
================================================== ====================
OUTER LOOP ITERATION = 8 CPU SECONDS = 1.396E+03
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| U-Mom | 0.85 | 3.9E-03 | 1.1E-01 | 1.1E-03 OK|
| V-Mom | 0.85 | 5.1E-03 | 2.3E-01 | 3.1E-03 OK|
| W-Mom | 0.81 | 2.5E-03 | 1.4E-01 | 9.2E-04 OK|
| P-Mass | 0.65 | 9.8E-05 | 3.5E-03 | 25.1 8.4E-02 OK|
+----------------------+------+---------+---------+------------------+
| H-Energy | 0.84 | 8.4E-03 | 2.3E-01 | 6.1 1.0E-05 OK|
+----------------------+------+---------+---------+------------------+
| K-TurbKE | 0.77 | 1.1E-02 | 5.1E-01 | 6.1 1.6E-05 OK|
| E-Diss.K | 0.69 | 1.1E-02 | 1.6E+00 | 7.4 1.1E-07 OK|
+----------------------+------+---------+---------+------------------+
================================================== ====================
OUTER LOOP ITERATION = 9 CPU SECONDS = 1.584E+03
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| U-Mom | 1.06 | 4.1E-03 | 1.6E-01 | 5.8E-04 OK|
| V-Mom | 0.91 | 4.6E-03 | 3.4E-01 | 1.3E-03 OK|
| W-Mom | 0.93 | 2.3E-03 | 1.1E-01 | 4.7E-04 OK|
| P-Mass | 0.91 | 8.9E-05 | 3.7E-03 | 21.1 8.0E-02 OK|
+----------------------+------+---------+---------+------------------+
| H-Energy | 0.74 | 6.2E-03 | 1.4E-01 | 6.0 1.1E-05 OK|
+----------------------+------+---------+---------+------------------+
| K-TurbKE | 0.87 | 9.5E-03 | 5.4E-01 | 6.0 1.9E-05 OK|
| E-Diss.K | 0.80 | 8.8E-03 | 1.6E+00 | 7.4 2.7E-07 OK|
+----------------------+------+---------+---------+------------------+
================================================== ====================
OUTER LOOP ITERATION = 10 CPU SECONDS = 1.766E+03
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| U-Mom | 1.01 | 4.1E-03 | 4.5E-01 | 5.7E-04 OK|
| V-Mom | 1.25 | 5.8E-03 | 9.4E-01 | 1.1E-03 OK|
| W-Mom | 1.07 | 2.5E-03 | 3.2E-01 | 6.1E-04 OK|
| P-Mass | 0.90 | 8.0E-05 | 3.6E-03 | 21.1 8.0E-02 OK|
+----------------------+------+---------+---------+------------------+
| H-Energy | 0.71 | 4.4E-03 | 8.9E-02 | 6.0 1.0E-05 OK|
+----------------------+------+---------+---------+------------------+
| K-TurbKE | 0.98 | 9.3E-03 | 9.1E-01 | 6.0 2.0E-05 OK|
| E-Diss.K | 0.97 | 8.5E-03 | 1.5E+00 | 7.4 2.4E-07 OK|
+----------------------+------+---------+---------+------------------+
================================================== ====================
OUTER LOOP ITERATION = 11 CPU SECONDS = 1.952E+03
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| U-Mom | 1.08 | 4.5E-03 | 6.6E-01 | 1.1E-03 OK|
| V-Mom | 1.58 | 9.2E-03 | 1.3E+00 | 8.7E-04 OK|
| W-Mom | 1.40 | 3.4E-03 | 5.1E-01 | 1.1E-03 OK|
| P-Mass | 0.95 | 7.6E-05 | 1.2E-02 | 21.1 9.6E-02 OK|
+----------------------+------+---------+---------+------------------+
| H-Energy | 0.77 | 3.4E-03 | 1.2E-01 | 6.0 8.1E-06 OK|
+----------------------+------+---------+---------+------------------+
| K-TurbKE | 0.73 | 6.8E-03 | 1.3E+00 | 6.0 1.9E-05 OK|
| E-Diss.K | 0.80 | 6.8E-03 | 1.5E+00 | 7.4 6.0E-08 OK|
+----------------------+------+---------+---------+------------------+
================================================== ====================
OUTER LOOP ITERATION = 12 CPU SECONDS = 2.142E+03
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| U-Mom | 0.72 | 3.2E-03 | 4.3E-01 | 1.4E-03 OK|
| V-Mom | 0.78 | 7.1E-03 | 7.4E-01 | 6.9E-04 OK|
| W-Mom | 0.81 | 2.8E-03 | 3.8E-01 | 1.2E-03 OK|
| P-Mass | 1.25 | 9.6E-05 | 1.8E-02 | 21.1 9.7E-02 OK|
+----------------------+------+---------+---------+------------------+
| H-Energy | 0.91 | 3.1E-03 | 1.6E-01 | 6.0 7.2E-06 OK|
+----------------------+------+---------+---------+------------------+
| K-TurbKE | 0.93 | 6.4E-03 | 9.4E-01 | 6.0 9.2E-06 OK|
| E-Diss.K | 0.92 | 6.3E-03 | 1.7E+00 | 7.4 1.1E-08 OK|
+----------------------+------+---------+---------+------------------+
================================================== ====================
OUTER LOOP ITERATION = 13 CPU SECONDS = 2.330E+03
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| U-Mom | 1.13 | 3.6E-03 | 7.5E-01 | 1.1E-03 OK|
| V-Mom | 1.09 | 7.8E-03 | 1.4E+00 | 3.7E-04 OK|
| W-Mom | 1.19 | 3.3E-03 | 5.9E-01 | 7.9E-04 OK|
| P-Mass | 1.70 | 1.6E-04 | 2.8E-02 | 17.1 8.7E-02 OK|
+----------------------+------+---------+---------+------------------+
| H-Energy | 1.05 | 3.2E-03 | 2.7E-01 | 5.9 6.4E-06 OK|
+----------------------+------+---------+---------+------------------+
| K-TurbKE | 0.69 | 4.4E-03 | 8.2E-01 | 5.9 4.7E-06 OK|
| E-Diss.K | 0.87 | 5.4E-03 | 1.3E+00 | 7.4 3.4E-09 OK|
+----------------------+------+---------+---------+------------------+
================================================== ====================
OUTER LOOP ITERATION = 14 CPU SECONDS = 2.515E+03
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| U-Mom | 0.95 | 3.5E-03 | 5.1E-01 | 1.5E-03 OK|
| V-Mom | 0.90 | 7.0E-03 | 8.4E-01 | 4.4E-04 OK|
| W-Mom | 1.04 | 3.5E-03 | 4.4E-01 | 8.2E-04 OK|
| P-Mass | 0.60 | 9.8E-05 | 1.3E-02 | 5.0 7.2E-02 OK|
+----------------------+------+---------+---------+------------------+
| H-Energy | 1.72 | 5.5E-03 | 9.8E-01 | 5.9 3.6E-06 OK|
+----------------------+------+---------+---------+------------------+
| K-TurbKE | 0.57 | 2.5E-03 | 4.9E-01 | 5.9 6.5E-06 OK|
| E-Diss.K | 0.37 | 2.0E-03 | 2.9E-01 | 7.4 4.1E-09 OK|
+----------------------+------+---------+---------+------------------+
================================================== ====================
OUTER LOOP ITERATION = 15 CPU SECONDS = 2.687E+03
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| U-Mom | 1.21 | 4.2E-03 | 5.6E-01 | 1.2E-03 OK|
| V-Mom | 1.07 | 7.5E-03 | 7.5E-01 | 5.8E-04 OK|
| W-Mom | 1.20 | 4.2E-03 | 4.4E-01 | 7.0E-04 OK|
| P-Mass | 0.66 | 6.5E-05 | 1.0E-02 | 5.0 9.0E-02 OK|
+----------------------+------+---------+---------+------------------+
| H-Energy | 1.05 | 5.8E-03 | 1.2E+00 | 5.9 1.3E-06 OK|
+----------------------+------+---------+---------+------------------+
| K-TurbKE | 1.48 | 3.7E-03 | 1.0E+00 | 5.9 1.4E-06 OK|
| E-Diss.K | 1.22 | 2.4E-03 | 5.8E-01 | 7.4 1.5E-09 OK|
+----------------------+------+---------+---------+------------------+
================================================== ====================
OUTER LOOP ITERATION = 16 CPU SECONDS = 2.851E+03
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| U-Mom | 0.87 | 3.6E-03 | 8.9E-01 | 4.4E-04 OK|
| V-Mom | 0.80 | 6.0E-03 | 1.2E+00 | 1.8E-04 OK|
| W-Mom | 0.68 | 2.9E-03 | 6.1E-01 | 5.8E-04 OK|
| P-Mass | 0.50 | 3.2E-05 | 6.3E-03 | 5.0 4.3E-02 OK|
+----------------------+------+---------+---------+------------------+
| H-Energy | 0.94 | 5.4E-03 | 9.0E-01 | 5.9 1.9E-07 OK|
+----------------------+------+---------+---------+------------------+
| K-TurbKE | 2.14 | 7.9E-03 | 1.6E+00 | 5.9 4.8E-08 OK|
| E-Diss.K | 2.90 | 7.0E-03 | 1.9E+00 | 7.5 3.1E-11 OK|
+----------------------+------+---------+---------+------------------+
================================================== ====================
OUTER LOOP ITERATION = 17 CPU SECONDS = 3.013E+03
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| U-Mom | 1.00 | 3.6E-03 | 9.3E-01 | 2.4E-04 OK|
| V-Mom | 1.03 | 6.2E-03 | 1.3E+00 | 1.6E-04 OK|
| W-Mom | 1.03 | 2.9E-03 | 6.4E-01 | 5.0E-04 OK|
| P-Mass | 1.81 | 5.9E-05 | 1.3E-02 | 5.0 6.0E-02 OK|
+----------------------+------+---------+---------+------------------+
| H-Energy | 0.82 | 4.5E-03 | 6.9E-01 | 5.9 4.5E-08 OK|
+----------------------+------+---------+---------+------------------+
| K-TurbKE | 0.72 | 5.7E-03 | 1.3E+00 | 5.9 3.6E-09 OK|
| E-Diss.K | 0.96 | 6.7E-03 | 1.9E+00 | 7.5 7.8E-13 OK|
+----------------------+------+---------+---------+------------------+
================================================== ====================
OUTER LOOP ITERATION = 18 CPU SECONDS = 3.174E+03
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| U-Mom | 0.83 | 3.0E-03 | 5.4E-01 | 2.0E-04 OK|
| V-Mom | 0.88 | 5.5E-03 | 6.9E-01 | 1.5E-04 OK|
| W-Mom | 0.91 | 2.7E-03 | 4.0E-01 | 3.9E-04 OK|
| P-Mass | 0.98 | 5.8E-05 | 1.4E-02 | 5.0 2.0E-02 OK|
+----------------------+------+---------+---------+------------------+
| H-Energy | 2.36 | 1.1E-02 | 2.3E+00 | 5.9 8.2E-09 OK|
+----------------------+------+---------+---------+------------------+
| K-TurbKE | 0.61 | 3.5E-03 | 4.9E-01 | 5.9 3.0E-09 OK|
| E-Diss.K | 0.51 | 3.4E-03 | 7.9E-01 | 7.5 3.6E-13 OK|
+----------------------+------+---------+---------+------------------+
================================================== ====================
OUTER LOOP ITERATION = 19 CPU SECONDS = 3.336E+03
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| U-Mom | 1.74 | 5.2E-03 | 9.3E-01 | 2.1E-04 OK|
| V-Mom | 1.29 | 7.1E-03 | 1.0E+00 | 2.2E-04 OK|
| W-Mom | 1.52 | 4.1E-03 | 6.4E-01 | 4.4E-04 OK|
| P-Mass | 1.16 | 6.7E-05 | 9.5E-03 | 5.0 1.9E-02 OK|
+----------------------+------+---------+---------+------------------+
| H-Energy | 0.77 | 8.1E-03 | 1.4E+00 | 5.9 2.3E-09 OK|
+----------------------+------+---------+---------+------------------+
| K-TurbKE | 1.51 | 5.3E-03 | 1.2E+00 | 5.9 4.9E-10 OK|
| E-Diss.K | 1.30 | 4.4E-03 | 1.3E+00 | 7.5 6.9E-14 OK|
+----------------------+------+---------+---------+------------------+
================================================== ====================
OUTER LOOP ITERATION = 20 CPU SECONDS = 3.499E+03
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| U-Mom | 0.72 | 3.8E-03 | 8.6E-01 | 3.3E-04 OK|
| V-Mom | 0.61 | 4.3E-03 | 8.4E-01 | 2.0E-04 OK|
| W-Mom | 0.63 | 2.6E-03 | 5.2E-01 | 8.1E-04 OK|
| P-Mass | 0.22 | 1.5E-05 | 3.3E-03 | 5.0 6.1E-02 OK|
+----------------------+------+---------+---------+------------------+
| H-Energy | 0.67 | 5.5E-03 | 9.5E-01 | 5.9 1.7E-09 OK|
+----------------------+------+---------+---------+------------------+
| K-TurbKE | 1.23 | 6.5E-03 | 1.5E+00 | 5.9 2.0E-11 OK|
| E-Diss.K | 1.38 | 6.1E-03 | 1.9E+00 | 7.4 2.5E-15 OK|
+----------------------+------+---------+---------+------------------+

Execution terminating: STP file found.

attiquejavaid08 is offline   Reply With Quote

Old   October 3, 2015, 04:17
Default
  #6
Member
 
Attique Javaid
Join Date: Apr 2015
Location: Pakistan
Posts: 66
Rep Power: 11
attiquejavaid08 is on a distinguished road
CFD Solver finished: Sat Oct 03 11:03:36 2015
CFD Solver wall clock seconds: 9.0584E+02
================================================== ====================
Termination and Interrupt Condition Summary
================================================== ====================

CFD Solver: Stop instruction received
================================================== ====================
Boundary Flow and Total Source Term Summary
================================================== ====================
+--------------------------------------------------------------------+
| U-Mom |
+--------------------------------------------------------------------+
Boundary : block 2.2237E+03
Boundary : in1 -2.0765E+05
Boundary : in2 2.1187E+05
Boundary : inwall -1.7517E+03
Boundary : outlet 6.4734E+02
Boundary : outwall -2.2986E+03
-----------
Domain Imbalance : 3.0427E+03
+--------------------------------------------------------------------+
| V-Mom |
+--------------------------------------------------------------------+
Boundary : block -1.2568E+05
Boundary : in1 1.3418E-04
Boundary : in2 1.3378E-04
Boundary : inwall -1.5951E+05
Boundary : outlet 2.8835E+05
Boundary : outwall -5.6425E+05
-----------
Domain Imbalance : -5.6109E+05
+--------------------------------------------------------------------+
| W-Mom |
+--------------------------------------------------------------------+
Boundary : block -1.2866E+03
Boundary : in1 -1.3647E+05
Boundary : in2 1.3925E+05
Boundary : inwall -8.9143E+03
Boundary : outlet -2.3447E+00
Boundary : outwall 5.8704E+03
-----------
Domain Imbalance : -1.5580E+03
+--------------------------------------------------------------------+
| P-Mass |
+--------------------------------------------------------------------+
Boundary : in1 6.6884E+03
Boundary : in2 6.6884E+03
Boundary : outlet -1.3381E+04
-----------
Domain Imbalance : -4.5354E+00
+--------------------------------------------------------------------+
| H-Energy |
+--------------------------------------------------------------------+
Boundary : in1 7.5847E+09
Bnd Src/Visc Work: in1 -3.8741E-04
Boundary : in2 7.5849E+09
Bnd Src/Visc Work: in2 -3.8593E-04
Boundary : outlet -1.5169E+10
Bnd Src/Visc Work: outlet -2.4713E-05
Domain Src (Neg) : Default Domain -2.0512E+10
Domain Src (Pos) : Default Domain 2.0512E+10
-----------
Domain Imbalance : 4.7423E+05

+--------------------------------------------------------------------+
| Normalised Imbalance Summary |
+--------------------------------------------------------------------+
| Equation | Maximum Flow | Imbalance (%) |
+--------------------------------------------------------------------+
| U-Mom | 5.6425E+05 | 0.5393 |
| V-Mom | 5.6425E+05 | -99.4394 |
| W-Mom | 5.6425E+05 | -0.2761 |
| P-Mass | 1.3381E+04 | -0.0339 |
+----------------------+-----------------------+---------------------+
| H-Energy | 2.0512E+10 | 0.0023 |
+----------------------+-----------------------+---------------------+
================================================== ====================
Wall Force and Moment Summary
================================================== ====================

Notes:
1. Pressure integrals exclude the reference pressure. To include
it, set the expert parameter 'include pref in forces = t'.

+--------------------------------------------------------------------+
| Pressure Force On Walls |
+--------------------------------------------------------------------+
X-Comp. Y-Comp. Z-Comp.
Domain Group: Default Domain
block -2.2182E+03 1.2570E+05 1.2815E+03
inwall 1.7779E+03 1.5617E+05 8.9011E+03
outwall 2.2346E+03 5.6885E+05 -5.9112E+03
----------- ----------- -----------
Domain Group Totals : 1.7942E+03 8.5072E+05 4.2715E+03

+--------------------------------------------------------------------+
| Viscous Force On Walls |
+--------------------------------------------------------------------+
X-Comp. Y-Comp. Z-Comp.
Domain Group: Default Domain
block -5.4715E+00 -2.0507E+01 5.0247E+00
inwall -2.6183E+01 3.3400E+03 1.3137E+01
outwall 6.3988E+01 -4.5994E+03 4.0715E+01
----------- ----------- -----------
Domain Group Totals : 3.2333E+01 -1.2798E+03 5.8877E+01

+--------------------------------------------------------------------+
| Pressure Moment On Walls |
+--------------------------------------------------------------------+
X-Comp. Y-Comp. Z-Comp.
Domain Group: Default Domain
block 1.1891E+04 -3.8765E+03 6.9287E+03
inwall 4.4601E+04 -1.2711E+01 -3.3111E+04
outwall -3.2175E+04 5.2149E+05 1.9172E+04
----------- ----------- -----------
Domain Group Totals : 2.4318E+04 5.1760E+05 -7.0105E+03

+--------------------------------------------------------------------+
| Viscous Moment On Walls |
+--------------------------------------------------------------------+
X-Comp. Y-Comp. Z-Comp.
Domain Group: Default Domain
block 5.7439E+01 -3.2706E+00 1.3736E+01
inwall 1.0823E+02 6.2429E+03 8.4841E+01
outwall 1.1748E+02 -5.2535E+03 -2.8897E+02
----------- ----------- -----------
Domain Group Totals : 2.8315E+02 9.8616E+02 -1.9040E+02

+--------------------------------------------------------------------+
| Locations of Maximum Residuals |
+--------------------------------------------------------------------+
| Equation | Domain Name | Node Number |
+--------------------------------------------------------------------+
| U-Mom | Default Domain | 414563 |
| V-Mom | Default Domain | 414527 |
| W-Mom | Default Domain | 414527 |
| P-Mass | Default Domain | 423396 |
+----------------------+-----------------------+---------------------+
| H-Energy | Default Domain | 414538 |
+----------------------+-----------------------+---------------------+
| K-TurbKE | Default Domain | 423395 |
| E-Diss.K | Default Domain | 423394 |
+----------------------+-----------------------+---------------------+
+--------------------------------------------------------------------+
| Average Scale Information |
+--------------------------------------------------------------------+
Domain Name : Default Domain
Global Length = 2.6095E+00
Minimum Extent = 5.8540E+00
Maximum Extent = 1.5531E+01
Density = 7.2594E+02
Dynamic Viscosity = 8.8400E-05
Velocity = 2.4291E+01
Advection Time = 1.0743E-01
Reynolds Number = 5.2053E+08
Thermal Conductivity = 5.6185E-01
Specific Heat Capacity at Constant Pressure = 5.4689E+03
Prandtl Number = 8.6047E-01
Temperature Range = 6.5129E+02
+--------------------------------------------------------------------+
| Variable Range Information |
+--------------------------------------------------------------------+
Domain Name : Default Domain
+--------------------------------------------------------------------+
| Variable Name | min | max |
+--------------------------------------------------------------------+
| Density | 7.26E+02 | 7.26E+02 |
| Specific Heat Capacity at Constant Pressure| 5.47E+03 | 5.47E+03 |
| Dynamic Viscosity | 8.84E-05 | 8.84E-05 |
| Thermal Conductivity | 5.62E-01 | 5.62E-01 |
| Static Entropy | -4.09E+05 | 4.27E+03 |
| Velocity u | -3.14E+03 | 3.19E+03 |
| Velocity v | -3.50E+03 | 5.95E+02 |
| Velocity w | -1.80E+03 | 1.82E+03 |
| Pressure | -7.57E+07 | 2.55E+08 |
| Turbulence Kinetic Energy | 5.51E-11 | 3.39E+06 |
| Turbulence Eddy Dissipation | 4.18E-07 | 6.50E+14 |
| Eddy Viscosity | 8.03E-14 | 9.99E+01 |
| Temperature | 0.00E+00 | 6.51E+02 |
| Static Enthalpy | -1.58E+06 | 2.26E+06 |
| Total Enthalpy | 5.69E+05 | 2.60E+06 |
+--------------------------------------------------------------------+
+--------------------------------------------------------------------+
| CPU Requirements of Numerical Solution - Total |
+--------------------------------------------------------------------+
Subsystem Name Discretization Linear Solution
(secs. %total) (secs. %total)
----------------------------------------------------------------------
Momentum and Mass 1.80E+03 48.6 % 5.16E+02 14.0 %
Heat Transfer 5.35E+02 14.5 % 6.64E+01 1.8 %
TurbKE and Diss.K 4.31E+02 11.7 % 1.43E+02 3.9 %
-------- ------- -------- ------
Subsystem Summary 2.76E+03 74.8 % 7.25E+02 19.6 %
Variable Updates 1.21E+02 3.3 %
File Reading 1.33E+00 0.0 %
File Writing 2.21E+01 0.6 %
Miscellaneous 6.22E+01 1.7 %
--------
Total 3.70E+03
+--------------------------------------------------------------------+
| Job Information at End of Run |
+--------------------------------------------------------------------+
Job finished: Sat Oct 03 11:03:45 2015
Total wall clock time: 9.238E+02 seconds
or: ( 0: 0: 15: 23.825 )
( Days: Hours: Minutes: Seconds )

--> Final synchronization point reached by all partitions.
End of solution stage.
+--------------------------------------------------------------------+
| The results from this run of the ANSYS CFX Solver have been |
| written to C:\Users\attique\Desktop\New folder\100315-7_002.res |
+--------------------------------------------------------------------+

This run of the ANSYS CFX Solver has finished.

================================================

cfx generated output file:
https://drive.google.com/file/d/0B4Y...ew?usp=sharing

Last edited by attiquejavaid08; October 3, 2015 at 08:11. Reason: addition of cfx output file link.
attiquejavaid08 is offline   Reply With Quote

Old   October 5, 2015, 04:45
Default
  #7
Senior Member
 
Join Date: Feb 2011
Posts: 496
Rep Power: 18
Antanas is on a distinguished road
Post sketch of your problem.
Antanas is offline   Reply With Quote

Old   October 5, 2015, 11:23
Default
  #8
Member
 
Attique Javaid
Join Date: Apr 2015
Location: Pakistan
Posts: 66
Rep Power: 11
attiquejavaid08 is on a distinguished road
Quote:
Originally Posted by Antanas View Post
Post sketch of your problem.
here it is, sir.

attiquejavaid08 is offline   Reply With Quote

Old   October 5, 2015, 17:49
Default
  #9
Super Moderator
 
Glenn Horrocks
Join Date: Mar 2009
Location: Sydney, Australia
Posts: 17,830
Rep Power: 144
ghorrocks is just really niceghorrocks is just really niceghorrocks is just really niceghorrocks is just really nice
Have you looked at the FAQs?
http://www.cfd-online.com/Wiki/Ansys...gence_criteria
http://www.cfd-online.com/Wiki/Ansys..._inaccurate.3F
ghorrocks is offline   Reply With Quote

Old   October 6, 2015, 02:02
Default
  #10
Senior Member
 
Join Date: Feb 2011
Posts: 496
Rep Power: 18
Antanas is on a distinguished road
Quote:
Originally Posted by attiquejavaid08 View Post
here it is, sir.
Is this fluid domain?
Antanas is offline   Reply With Quote

Old   October 6, 2015, 02:22
Default
  #11
Member
 
Attique Javaid
Join Date: Apr 2015
Location: Pakistan
Posts: 66
Rep Power: 11
attiquejavaid08 is on a distinguished road
i'm looking into it sir.

Quote:
Originally Posted by Antanas View Post
Is this fluid domain?
yes, it's fluid domain. inlet from pipe sides. and outlet at bottom of the larger cylinder.
attiquejavaid08 is offline   Reply With Quote

Old   October 6, 2015, 04:44
Default
  #12
Member
 
Attique Javaid
Join Date: Apr 2015
Location: Pakistan
Posts: 66
Rep Power: 11
attiquejavaid08 is on a distinguished road
Describing here my approach (which I’ve conceived by going through a lot of topics in this forum).
I'm using k-epsilon model. I’m not intended to use k-omega because it needs so finer mesh near wall which lead to very high cell count and I’ve maximum 16 GB memory at the moment. So looking at Re~1.38e8, apparently very thin boundary layer, keeping memory limit in view, I decided to go for scalable wall function first.
----------------------------
y+ & first cell height (m)
11 & 2.9e-6
----------------------------
for this first cell height, i got very low orthogonal quality of mesh. FLUENT didn't accept it and i switched to standard wall function with this intention that i should get first my simulation going on with broad range setup having convergence. i can narrow down the y+ later.
Now for standard wall function y+ range i got:
----------------------------
y+ & first cell height (m)
30 & 8e-6
300 & 7.98e-5
----------------------------
i've been using FLUENT that's why i tried to make things work first in FLUENT. using 7.98e-5 m spacing, at connection of inlet pipes to larger cylindrical domain (at curvature) i got velocities higher than average inlet velocity (as expected). here, y+ was much more greater than 300. so i kept decreasing first cell height.

Now, i've reached from 7.98e-5 m to 1.1e-5 m. This is where i'm unable to simulate my problem in FLUENT further. Because orthogonal quality goes lower than 0.01 for mesh with first cell spacing lower than 1.1e-5 m because of this issue, it's not acceptable in FLUENT. Other parameters like min angle, skewness, determinant criterion were in acceptable ranges (which I learnt through this forum). So I tried to check this domain in CFX.

The only reason I’ve mentioned my approach is, i need guidance and things to be pointed out if I’m doing anything wrong in the method I’m going through. I understand it’s not a single-sitting-one-attempt-problem-solving job. After getting back to my PC, I’ll surely post figures related to my concerns described above.

AJ
attiquejavaid08 is offline   Reply With Quote

Old   October 6, 2015, 05:39
Default
  #13
Senior Member
 
Join Date: Feb 2011
Posts: 496
Rep Power: 18
Antanas is on a distinguished road
Got some results.
Attached Images
File Type: jpg res.jpg (61.2 KB, 36 views)
File Type: jpg solve.jpg (116.2 KB, 33 views)
Antanas is offline   Reply With Quote

Old   October 6, 2015, 06:22
Default
  #14
Member
 
Attique Javaid
Join Date: Apr 2015
Location: Pakistan
Posts: 66
Rep Power: 11
attiquejavaid08 is on a distinguished road
Quote:
Originally Posted by Antanas View Post
Got some results.
looking at results, mass flow rate at outlet seems quite right. imbalances are low enough. pressure distribution seems as it was supposed to be. did you check y+ sir?
any advice(s) about what was there wrong? please.

P.S. btw i've learnt today a better way to arrange monitors in a windows. TY ^_^
I assume that you've geometry and blocking file from meshing thread.
attiquejavaid08 is offline   Reply With Quote

Old   October 6, 2015, 07:41
Default
  #15
Senior Member
 
Join Date: Feb 2011
Posts: 496
Rep Power: 18
Antanas is on a distinguished road
Quote:
Originally Posted by attiquejavaid08 View Post
looking at results, mass flow rate at outlet seems quite right. imbalances are low enough. pressure distribution seems as it was supposed to be. did you check y+ sir?
any advice(s) about what was there wrong? please.

P.S. btw i've learnt today a better way to arrange monitors in a windows. TY ^_^
I assume that you've geometry and blocking file from meshing thread.
Catch

Last edited by Antanas; October 6, 2015 at 09:54.
Antanas is offline   Reply With Quote

Old   October 6, 2015, 08:44
Default
  #16
Member
 
Attique Javaid
Join Date: Apr 2015
Location: Pakistan
Posts: 66
Rep Power: 11
attiquejavaid08 is on a distinguished road
It's really helpful. to be honest, i never read it before.

Quote:
Originally Posted by Antanas View Post
Catch

will you share please about what did:
what y+ you achieved? did you change the meshing params? or whatever you think is worth sharing.

It's a steady state case. i need to move to transient simulation onwards for almost similar case but with a little modification with extra pipes added. that's why i'm concerned about it sir.

EDIT: I'm sorry. I didn't know that CATCH was a link itself.
got it.

I'll look into it. and will update soon.

Last edited by attiquejavaid08; October 6, 2015 at 10:09.
attiquejavaid08 is offline   Reply With Quote

Old   October 6, 2015, 10:11
Default
  #17
Senior Member
 
Join Date: Feb 2011
Posts: 496
Rep Power: 18
Antanas is on a distinguished road
Quote:
Originally Posted by attiquejavaid08 View Post
will you share please about what
There's a link in my prev. post. Download and see.

1. I used your geo and blocking. Just genereted mesh.
2. I changed solver settings. First I used Upwind advection scheme with auto timescale, then switched to High Res and used prev. results as initial guess. Though I didn't try to use High Res at first. Why did you try to use Specified Blend Factor and Local Timescale Factor? Defaults suit at most cases. Always try to advance from the simple to the complex.
3. I changed Total Energy HT model to Thermal Energy. I didn't investigate its influence on convergence, but are you sure that you need Total Energy? Do kinetic energy effects considerable in your case?
Antanas is offline   Reply With Quote

Old   October 6, 2015, 10:38
Default
  #18
Member
 
Attique Javaid
Join Date: Apr 2015
Location: Pakistan
Posts: 66
Rep Power: 11
attiquejavaid08 is on a distinguished road
Quote:
Originally Posted by Antanas View Post
There's a link in my prev. post. Download and see.

1. I used your geo and blocking. Just genereted mesh.
2. I changed solver settings. First I used Upwind advection scheme with auto timescale, then switched to High Res and used prev. results as initial guess. Though I didn't try to use High Res at first. Why did you try to use Specified Blend Factor and Local Timescale Factor? Defaults suit at most cases. Always try to advance from the simple to the complex.
3. I changed Total Energy HT model to Thermal Energy. I didn't investigate its influence on convergence, but are you sure that you need Total Energy? Do kinetic energy effects considerable in your case?
1. Okay
2. I'll take that advice.
I was not sure, just read somewhere that blend factor helps in convergence in CFX. Can you explain a little in what conditions a blend factor and local timescale factor to be used? it may be make it more clear to me to cross check my case.
3. I've not involved heating zone in this domain yet. (partially following your advice @ 2) But considering it, i chose total energy.
attiquejavaid08 is offline   Reply With Quote

Reply

Tags
chart, plot, post, pressure distribution

Thread Tools Search this Thread
Search this Thread:

Advanced Search
Display Modes

Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are Off
Pingbacks are On
Refbacks are On


Similar Threads
Thread Thread Starter Forum Replies Last Post
Radiation interface hinca CFX 15 January 26, 2014 17:11
Strange pressure distribution with a rotating cylinder HiF OpenFOAM Running, Solving & CFD 0 July 17, 2010 00:06
Multicomponent fluid Andrea CFX 2 October 11, 2004 05:12
Gas pressure question Dan Moskal Main CFD Forum 0 October 24, 2002 22:02
Hydrostatic pressure in 2-phase flow modeling (long) DS & HB Main CFD Forum 0 January 8, 2000 15:00


All times are GMT -4. The time now is 07:58.