XPR VERSION 12
Requested task is SYSNOISE parallel computation.
Working directory on server is C:\Users\zhangfan\AppData\Local\Temp
Checking that the SYSNOISE launch script (C:\Program Files\LMS\LMS Virtual.Lab 12\VirtualLab\Sysnoise\5.6\bin\sysnoise_nogui.bat) exists on server...
OK
SYSNOISE log file on server is C:\Users\zhangfan\AppData\Local\Temp\zhangfan-195188-sysnoise.log.
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System for Computational Vibro-Acoustics
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SYSNOISE Rev 5.6 Windows_x86_64 MAR2003 DATE: 26-MAY-2017 11:23:08
PATCH LEVEL P (Build Date: 03-JUN-2013)
READING THE SET-UP FILE: C:\Program Files\LMS\LMS Virtual.Lab 12\VirtualLab\Sysnoise\5.6\bin\\..\res\SYSNOISE.STP
THE SYSNOISE PROFILE FILE NAME HAS NOT BEEN DEFINED.
STANDARD GRAPHIC DEVICE SET TO DEFAULT
PLOTTING GRAPHIC DEVICE SET TO SCREENDUMP
MEMORY IN USE = 800000
AVAILABLE MEMORY= 174475006
FREE MEMORY = 173675006
CREATING DEFAULT SYSNOISE MODEL FILE default.sdb
SYSNOISE ANALYSIS OPTION :
BEM INDIRECT VARIATIONAL UNBAFFLED FREQUENCY FLUID
SYSNOISE> SCL> ENVIRONMENT SECTION SETUP USRDIR 'C:\Users\zhangfan\AppData\Local\Temp\' RETURN
SYSNOISE> SCL> ENVIRONMENT SECTION SETUP TMPDIR 'C:\Users\zhangfan\AppData\Local\Temp\' RETURN
SYSNOISE> SCL> ENVIRONMENT DISTRIBUTED=TRUE RETURN
SYSNOISE> SCL> ENVIRONMENT DISTRILEVEL=FREQUENCY RETURN
SYSNOISE> SCL> Open Model 1 File zhangfan-195188-Acoustic.sdb Original Return
OPENING SYSNOISE MODEL FILE zhangfan-195188-Acoustic.sdb.0
LOADING MODEL Exported VLModel
SYSNOISE> SCL> Extract Summary Return
SYSNOISE ANALYSIS OPTION :
FEM VARIATIONAL FREQUENCY FLUID
SYSNOISE SUMMARY INFORMATION
------------------------------------------------------------------------
Title...Exported VLModel
Date....26-MAY-2017 11:23:08
Number of dimensions...................... 3
Number of nodes........................... 12715
Number of elements........................ 59273
Number of tables.......................... 6
Number of material characteristics........ 2
Number of transfer admittance relations... 1
Number of faces with transfer admittance.. 3192
Number of load cases...................... 1
Number of faces with velocity B.C.'s...... 43
Number of faces with admit/imped B.C.'s... 62
------------------------------------------------------------------------
SYSNOISE> SCL> Option FEM Frequency Fluid Return
SYSNOISE ANALYSIS OPTION :
FEM VARIATIONAL FREQUENCY FLUID
SYSNOISE> SCL> Environment Section SETUP BELL 'on' Return
SYSNOISE> SCL> Environment Section SETUP SOLVITER 0 Return
SYSNOISE> SCL> Environment Section SETUP STABLEFEM TRUE Return
SYSNOISE> SCL> Environment Section SETUP GEO_TOLERANCE '1E-006' Return
SYSNOISE> SCL> ENVIRONMENT SECTION PFEM STRATEGY 0 RETURN
SYSNOISE> SCL> Parameter Model 1 Physical
PARAMETER> SCL> Save Potentials Step 1
PARAMETER> SCL> Save Results none
PARAMETER> SCL> NoFlow
PARAMETER> SCL> Return
Updating Model Parameters
SYSNOISE> SCL> Solve
SOLVE> SCL> Frequency 100 To 1000 LinStep 25
SOLVE> SCL> Return
========================================================================
FREQUENCY RESPONSE MODULE
------------------------------------------------------------------------
FOR 37 FREQUENCIES FROM 100.000 TO 1000.000 HZ
ANALYSIS # 1 FREQUENCY = 100.000 HZ TYPE = NORMAL
ANALYSIS # 2 FREQUENCY = 125.000 HZ TYPE = NORMAL
ANALYSIS # 3 FREQUENCY = 150.000 HZ TYPE = NORMAL
ANALYSIS # 4 FREQUENCY = 175.000 HZ TYPE = NORMAL
ANALYSIS # 5 FREQUENCY = 200.000 HZ TYPE = NORMAL
ANALYSIS # 6 FREQUENCY = 225.000 HZ TYPE = NORMAL
ANALYSIS # 7 FREQUENCY = 250.000 HZ TYPE = NORMAL
ANALYSIS # 8 FREQUENCY = 275.000 HZ TYPE = NORMAL
ANALYSIS # 9 FREQUENCY = 300.000 HZ TYPE = NORMAL
ANALYSIS # 10 FREQUENCY = 325.000 HZ TYPE = NORMAL
ANALYSIS # 11 FREQUENCY = 350.000 HZ TYPE = NORMAL
ANALYSIS # 12 FREQUENCY = 375.000 HZ TYPE = NORMAL
ANALYSIS # 13 FREQUENCY = 400.000 HZ TYPE = NORMAL
ANALYSIS # 14 FREQUENCY = 425.000 HZ TYPE = NORMAL
ANALYSIS # 15 FREQUENCY = 450.000 HZ TYPE = NORMAL
ANALYSIS # 16 FREQUENCY = 475.000 HZ TYPE = NORMAL
ANALYSIS # 17 FREQUENCY = 500.000 HZ TYPE = NORMAL
ANALYSIS # 18 FREQUENCY = 525.000 HZ TYPE = NORMAL
ANALYSIS # 19 FREQUENCY = 550.000 HZ TYPE = NORMAL
ANALYSIS # 20 FREQUENCY = 575.000 HZ TYPE = NORMAL
ANALYSIS # 21 FREQUENCY = 600.000 HZ TYPE = NORMAL
ANALYSIS # 22 FREQUENCY = 625.000 HZ TYPE = NORMAL
ANALYSIS # 23 FREQUENCY = 650.000 HZ TYPE = NORMAL
ANALYSIS # 24 FREQUENCY = 675.000 HZ TYPE = NORMAL
ANALYSIS # 25 FREQUENCY = 700.000 HZ TYPE = NORMAL
ANALYSIS # 26 FREQUENCY = 725.000 HZ TYPE = NORMAL
ANALYSIS # 27 FREQUENCY = 750.000 HZ TYPE = NORMAL
ANALYSIS # 28 FREQUENCY = 775.000 HZ TYPE = NORMAL
ANALYSIS # 29 FREQUENCY = 800.000 HZ TYPE = NORMAL
ANALYSIS # 30 FREQUENCY = 825.000 HZ TYPE = NORMAL
ANALYSIS # 31 FREQUENCY = 850.000 HZ TYPE = NORMAL
ANALYSIS # 32 FREQUENCY = 875.000 HZ TYPE = NORMAL
ANALYSIS # 33 FREQUENCY = 900.000 HZ TYPE = NORMAL
ANALYSIS # 34 FREQUENCY = 925.000 HZ TYPE = NORMAL
ANALYSIS # 35 FREQUENCY = 950.000 HZ TYPE = NORMAL
ANALYSIS # 36 FREQUENCY = 975.000 HZ TYPE = NORMAL
ANALYSIS # 37 FREQUENCY = 1000.000 HZ TYPE = NORMAL
------------------------------------------------------------------------
SOLVE PARAMETERS
MODEL: 1 - Exported VLModel
------------------------------------------------------------------------
PHYSICAL Coordinates
Saving POTENTIALS every 1 steps
No saving of RESULTS
Energy Calculation Enabled
Surface post-processing on positive side
------------------------------------------------------------------------
LAUNCHING UNCOUPLED ACOUSTIC FEM (Physical Coords - Freq) ANALYSIS
NO SUPERIMPOSED NODES WITH TOLERANCE= 6.29000E-07
NO ISOLATED NODES
CHECKING ELEMENT TOPOLOGY AND DISTORTION
NO SUPERIMPOSED ELEMENTS WITH TOLERANCE= 6.29000E-07
Checking MESH Connectivity...
2 Part(s) and 2 Sub-Domain(s) found
4232 ENVELOPE FACE(S) REMAINING FOR PART 1
6866 ENVELOPE FACE(S) REMAINING FOR PART 2
Occupied space: 14 Mb ( 2.06 %)
COMPUTING PART INFORMATION:
Part 1 Volume: 4.84985E-03
Part 2 Volume: 7.73140E-03
THIS MODEL SEEMS SUITABLE FOR A FEM FLUID APPROACH
CPU Stats --- Delta: 0:00:03 ( 3.12) Total: 0:00:03 ( 3.12)
Computing MASS and STIFFNESS elements matrices
using HIGH PRECISION STABILIZED scheme for linear elements
CPU Stats --- Delta: 0:00:00 ( 0.33) Total: 0:00:03 ( 3.45)
Computing VELOCITY matrices on elements faces
CPU Stats --- Delta: 0:00:00 ( 0.49) Total: 0:00:04 ( 3.94)
Computing ADMITTANCE matrices on elements faces
*****Interpolation between non-matching surfaces with transfer admittance relations:*****
=== Transfer admittance relation # 1
*There were 1596 acoustic faces of surface 1 coupled with 1596
acoustic faces of surface 2. 0 acoustic faces were
excluded from surface 1 for being beyond the tolerance.
There were 0 orphaned nodes (not coupled) out of the 840
nodes of the acoustic surface 2.
There were 0 Gauss points interpolated with a nodal distance-based algorithm and 6384 Gauss points interpolated with an element-based algorithm.
===========
*****End of interpolation information:*****
CPU Stats --- Delta: 0:00:00 ( 0.40) Total: 0:00:04 ( 4.34)
CPU Stats --- Delta: 0:00:00 ( 0.00) Total: 0:00:04 ( 4.34)
Solver is MUMPS solver
Number of equations 12715
------------------------------------------------------------------------
COMPUTATION PROGRESS : 0 / 37 ( 0.00 % )
------------------------------------------------------------------------
ANALYSIS NUMBER 4 / 37 FREQUENCY = 175.000 Hz
------------------------------------------------------------------------
CPU Stats --- Delta: 0:00:00 ( 0.46) Total: 0:00:05 ( 4.80)
Building Matrix of Coefficients
CPU Stats --- Delta: 0:00:00 ( 0.10) Total: 0:00:05 ( 4.90)
CPU Stats --- Delta: 0:00:00 ( 0.01) Total: 0:00:05 ( 4.91)
Occupied space: 13 Mb ( 1.93 %)
Solving system of equations by direct solver
Analysis Phase ...
A FATAL ERROR OCCURRED. PROGRAM STOPPED
**** ERROR has occurred during computation ****
You may try to compute the solution in manual mode and try to attach the results afterwards.
发表于 2017-5-26 11:28
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