XPR VERSION 12
Requested task is SYSNOISE sequential computation.
Working directory on server is C:\Users\VEHICL~1\AppData\Local\Temp
Checking that the SYSNOISE launch script (D:\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\VEHICL~1\AppData\Local\Temp\vehicle_tm-650482-sysnoise.log.
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System for Computational Vibro-Acoustics
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SYSNOISE Rev 5.6 Windows_x86_64 MAR2003 DATE: 28-MAR-2017 13:15:48
PATCH LEVEL P (Build Date: 03-JUN-2013)
READING THE SET-UP FILE: D:\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= 504500000
FREE MEMORY = 503700000
CREATING DEFAULT SYSNOISE MODEL FILE default.sdb
SYSNOISE ANALYSIS OPTION :
BEM INDIRECT VARIATIONAL UNBAFFLED FREQUENCY FLUID
SYSNOISE> SCL> ENVIRONMENT SECTION SETUP USRDIR 'C:\Users\VEHICL~1\AppData\Local\Temp\' RETURN
SYSNOISE> SCL> ENVIRONMENT SECTION SETUP TMPDIR 'C:\Users\VEHICL~1\AppData\Local\Temp\' RETURN
SYSNOISE> SCL> Open Model 1 File vehicle_tm-650482-Structure.sdb Original Return
OPENING SYSNOISE MODEL FILE vehicle_tm-650482-Structure.sdb
LOADING MODEL Exported VLModel
WARNING: There are 30006 3-Dimensional Elements
SYSNOISE> SCL> Open Model 2 File vehicle_tm-650482-Acoustic.sdb Original Return
OPENING SYSNOISE MODEL FILE vehicle_tm-650482-Acoustic.sdb
LOADING MODEL Exported VLModel
SYSNOISE> SCL> Extract Summary Return
SYSNOISE ANALYSIS OPTION :
FEM VARIATIONAL FREQUENCY FLUID
SYSNOISE SUMMARY INFORMATION
------------------------------------------------------------------------
Title...Exported VLModel
Date....28-MAR-2017 13:15:48
Number of dimensions...................... 3
Number of nodes........................... 13524
Number of elements........................ 11880
Number of material characteristics........ 1
Number of load cases...................... 1
Number of faces with velocity B.C.'s...... 132
Number of faces with admit/imped B.C.'s... 132
------------------------------------------------------------------------
SYSNOISE> SCL> Environment Section SETUP GEO_TOLERANCE '1E-006' Return
SYSNOISE> SCL> Environment Section SETUP BELL 'on' Return
SYSNOISE> SCL> Environment Section SETUP STABLEFEM TRUE Return
SYSNOISE> SCL> Parameter Model 2
PARAMETER> SCL> Physical
PARAMETER> SCL> Save Potentials Step 1
PARAMETER> SCL> Save Results none
PARAMETER> SCL> Store Results none
STORE RESULTS> SCL> Return
PARAMETER> SCL> NoFlow
PARAMETER> SCL> Return
Updating Model Parameters
SYSNOISE> SCL> Activate Model 2 return
SYSNOISE> SCL> Solve
SOLVE> SCL> Frequency 100 To 4000 LinStep 100
SOLVE> SCL> Return
========================================================================
FREQUENCY RESPONSE MODULE
------------------------------------------------------------------------
FOR 40 FREQUENCIES FROM 100.000 TO 4000.000 HZ
ANALYSIS # 1 FREQUENCY = 100.000 HZ TYPE = NORMAL
ANALYSIS # 2 FREQUENCY = 200.000 HZ TYPE = NORMAL
ANALYSIS # 3 FREQUENCY = 300.000 HZ TYPE = NORMAL
ANALYSIS # 4 FREQUENCY = 400.000 HZ TYPE = NORMAL
ANALYSIS # 5 FREQUENCY = 500.000 HZ TYPE = NORMAL
ANALYSIS # 6 FREQUENCY = 600.000 HZ TYPE = NORMAL
ANALYSIS # 7 FREQUENCY = 700.000 HZ TYPE = NORMAL
ANALYSIS # 8 FREQUENCY = 800.000 HZ TYPE = NORMAL
ANALYSIS # 9 FREQUENCY = 900.000 HZ TYPE = NORMAL
ANALYSIS # 10 FREQUENCY = 1000.000 HZ TYPE = NORMAL
ANALYSIS # 11 FREQUENCY = 1100.000 HZ TYPE = NORMAL
ANALYSIS # 12 FREQUENCY = 1200.000 HZ TYPE = NORMAL
ANALYSIS # 13 FREQUENCY = 1300.000 HZ TYPE = NORMAL
ANALYSIS # 14 FREQUENCY = 1400.000 HZ TYPE = NORMAL
ANALYSIS # 15 FREQUENCY = 1500.000 HZ TYPE = NORMAL
ANALYSIS # 16 FREQUENCY = 1600.000 HZ TYPE = NORMAL
ANALYSIS # 17 FREQUENCY = 1700.000 HZ TYPE = NORMAL
ANALYSIS # 18 FREQUENCY = 1800.000 HZ TYPE = NORMAL
ANALYSIS # 19 FREQUENCY = 1900.000 HZ TYPE = NORMAL
ANALYSIS # 20 FREQUENCY = 2000.000 HZ TYPE = NORMAL
ANALYSIS # 21 FREQUENCY = 2100.000 HZ TYPE = NORMAL
ANALYSIS # 22 FREQUENCY = 2200.000 HZ TYPE = NORMAL
ANALYSIS # 23 FREQUENCY = 2300.000 HZ TYPE = NORMAL
ANALYSIS # 24 FREQUENCY = 2400.000 HZ TYPE = NORMAL
ANALYSIS # 25 FREQUENCY = 2500.000 HZ TYPE = NORMAL
ANALYSIS # 26 FREQUENCY = 2600.000 HZ TYPE = NORMAL
ANALYSIS # 27 FREQUENCY = 2700.000 HZ TYPE = NORMAL
ANALYSIS # 28 FREQUENCY = 2800.000 HZ TYPE = NORMAL
ANALYSIS # 29 FREQUENCY = 2900.000 HZ TYPE = NORMAL
ANALYSIS # 30 FREQUENCY = 3000.000 HZ TYPE = NORMAL
ANALYSIS # 31 FREQUENCY = 3100.000 HZ TYPE = NORMAL
ANALYSIS # 32 FREQUENCY = 3200.000 HZ TYPE = NORMAL
ANALYSIS # 33 FREQUENCY = 3300.000 HZ TYPE = NORMAL
ANALYSIS # 34 FREQUENCY = 3400.000 HZ TYPE = NORMAL
ANALYSIS # 35 FREQUENCY = 3500.000 HZ TYPE = NORMAL
ANALYSIS # 36 FREQUENCY = 3600.000 HZ TYPE = NORMAL
ANALYSIS # 37 FREQUENCY = 3700.000 HZ TYPE = NORMAL
ANALYSIS # 38 FREQUENCY = 3800.000 HZ TYPE = NORMAL
ANALYSIS # 39 FREQUENCY = 3900.000 HZ TYPE = NORMAL
ANALYSIS # 40 FREQUENCY = 4000.000 HZ TYPE = NORMAL
------------------------------------------------------------------------
SOLVE PARAMETERS
MODEL: 1 - Exported VLModel
------------------------------------------------------------------------
PHYSICAL Coordinates
Saving DISPLACEMENTS every 1 steps
Energy Calculation Enabled
Surface post-processing on positive side
------------------------------------------------------------------------
SOLVE PARAMETERS
MODEL: 2 - Exported VLModel
------------------------------------------------------------------------
PHYSICAL Coordinates
Saving POTENTIALS every 1 steps
No saving of RESULTS
Energy Calculation Enabled
Surface post-processing on positive side
------------------------------------------------------------------------
LAUNCHING COUPLED FEM-FEM (Physical Coords - Freq) ANALYSIS
Number of coupled load cases = 1
NO SUPERIMPOSED NODES WITH TOLERANCE= 9.20000E-07
NO ISOLATED NODES
CHECKING ELEMENT TOPOLOGY AND DISTORTION
NO SUPERIMPOSED ELEMENTS WITH TOLERANCE= 9.20000E-07
Checking MESH Connectivity...
2 Part(s) and 2 Sub-Domain(s) found
1504 ENVELOPE FACE(S) REMAINING FOR PART 1
1814 ENVELOPE FACE(S) REMAINING FOR PART 2
Occupied space: 10 Mb ( 0.51 %)
COMPUTING PART INFORMATION:
Part 1 Volume: 3.12010E-03
Part 2 Volume: 3.90013E-03
THIS MODEL SEEMS SUITABLE FOR A FEM FLUID APPROACH
CPU Stats --- Delta: 0:00:01 ( 1.15) Total: 0:00:01 ( 1.15)
Building FLUID / STRUCTURE interface
Using Model 1 as STRUCTURAL Model
Using Model 2 as FLUID Model
There are 294 interface node(s) on the FEM FLUID side
There are 714 interface node(s) on the FEM STRUCTURE side
Generating INTERFACE mesh
Structural INTERFACE MESH contains 648 elements
Fluid INTERFACE MESH contains 132 elements
Generating INTERFACE mesh
Structural INTERFACE MESH contains 648 elements
Fluid INTERFACE MESH contains 132 elements
Computing FLUID Element System Matrices
Computing MASS and STIFFNESS elements matrices
using HIGH PRECISION STABILIZED scheme for linear elements
CPU Stats --- Delta: 0:00:00 ( 0.06) Total: 0:00:01 ( 1.21)
Computing VELOCITY matrices on elements faces
CPU Stats --- Delta: 0:00:00 ( 0.01) Total: 0:00:01 ( 1.22)
Computing ADMITTANCE matrices on elements faces
CPU Stats --- Delta: 0:00:00 ( 0.00) Total: 0:00:01 ( 1.22)
CPU Stats --- Delta: 0:00:00 ( 0.00) Total: 0:00:01 ( 1.22)
CPU Stats --- Delta: 0:00:00 ( 0.00) Total: 0:00:01 ( 1.22)
Running Bacon and Dynam ...
CPU Stats --- Delta: 0:00:05 ( 4.84) Total: 0:00:06 ( 6.06)
ERROR *** END OF FILE: ONLY 0 OVER 30006 ELEMENTS ARE READ FROM u60 FILE
**** ERROR has occurred during computation ****
You may try to compute the solution in manual mode and try to attach the results afterwards.
Aborting Coupled Direct Response procedure due to error...
>> ERROR : Aborting Coupled Direct Response procedure due to error...
**** ERROR has occurred during computation ****
You may try to compute the solution in manual mode and try to attach the results afterwards.
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 2017-3-28 13:28
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