主任，我计算其他的正常工作，但是其中一个就出现错误，代码是：
XPR VERSION 11-SL2
Requested task is SYSNOISE sequential computation.
Working directory on server is C:\Users\ADMINI~1\AppData\Local\Temp
Checking that the SYSNOISE launch script (D:\Program Files\LMS\LMS Virtual.Lab 11-SL2\VirtualLab\Sysnoise\5.6\bin\sysnoise_nogui.bat) exists on server...
OK
SYSNOISE log file on server is C:\Users\ADMINI~1\AppData\Local\Temp\Administrator-1623225-sysnoise.log.
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xxxxxxxxxxxx JOB EXECUTION START
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System for Computational Vibro-Acoustics
------------------------------------------------------------------------
SYSNOISE Rev 5.6 Windows_x86_64 MAR2003 DATE: 07-JUL-2013 20:26:33
PATCH LEVEL O (Build Date: 18-FEB-2013)
READING THE SET-UP FILE: D:\Program Files\LMS\LMS Virtual.Lab 11-SL2\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= 494500000
FREE MEMORY = 493700000
CREATING DEFAULT SYSNOISE MODEL FILE default.sdb
SYSNOISE ANALYSIS OPTION :
BEM INDIRECT VARIATIONAL UNBAFFLED FREQUENCY FLUID
SYSNOISE> SCL> ENVIRONMENT SECTION SETUP USRDIR 'C:\Users\ADMINI~1\AppData\Local\Temp\' RETURN
SYSNOISE> SCL> ENVIRONMENT SECTION SETUP TMPDIR 'C:\Users\ADMINI~1\AppData\Local\Temp\' RETURN
SYSNOISE> SCL> Open Model 1 File Administrator-1623225-Structure.sdb Original Return
OPENING SYSNOISE MODEL FILE Administrator-1623225-Structure.sdb
LOADING MODEL Exported VLModel
WARNING: There are 1201686 3-Dimensional Elements
SYSNOISE> SCL> Open Model 2 File Administrator-1623225-Acoustic.sdb Original Return
OPENING SYSNOISE MODEL FILE Administrator-1623225-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....07-JUL-2013 20:26:35
Number of dimensions...................... 3
Number of nodes........................... 9589
Number of elements........................ 41435
Number of AML faces....................... 6432
Number of AML Kirchhoff faces............. 4224
Number of material characteristics........ 1
Number of load cases...................... 1
Number of defined sources................. 1
------------------------------------------------------------------------
SYSNOISE> SCL> Environment Section SETUP GEO_TOLERANCE '1E-006' Return
SYSNOISE> SCL> Return 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 AML LAYERNUM 5 Return
SYSNOISE> SCL> ENVIRONMENT SECTION AML WAVELENGTH_RATIO 0.160000 Return
SYSNOISE> SCL> Parameter Model 2
PARAMETER> SCL> Physical
PARAMETER> SCL> Save Potentials Step 1
PARAMETER> SCL> Save Results none
PARAMETER> SCL> Store Potentials none
STORE POTENTIALS> SCL> Return
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 250 To 3000 LinStep 250
SOLVE> SCL> Return
========================================================================
FREQUENCY RESPONSE MODULE
------------------------------------------------------------------------
FOR 12 FREQUENCIES FROM 250.000 TO 3000.000 HZ
ANALYSIS # 1 FREQUENCY = 250.000 HZ TYPE = NORMAL
ANALYSIS # 2 FREQUENCY = 500.000 HZ TYPE = NORMAL
ANALYSIS # 3 FREQUENCY = 750.000 HZ TYPE = NORMAL
ANALYSIS # 4 FREQUENCY = 1000.000 HZ TYPE = NORMAL
ANALYSIS # 5 FREQUENCY = 1250.000 HZ TYPE = NORMAL
ANALYSIS # 6 FREQUENCY = 1500.000 HZ TYPE = NORMAL
ANALYSIS # 7 FREQUENCY = 1750.000 HZ TYPE = NORMAL
ANALYSIS # 8 FREQUENCY = 2000.000 HZ TYPE = NORMAL
ANALYSIS # 9 FREQUENCY = 2250.000 HZ TYPE = NORMAL
ANALYSIS # 10 FREQUENCY = 2500.000 HZ TYPE = NORMAL
ANALYSIS # 11 FREQUENCY = 2750.000 HZ TYPE = NORMAL
ANALYSIS # 12 FREQUENCY = 3000.000 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= 5.56000E-06
NO ISOLATED NODES
CHECKING ELEMENT TOPOLOGY AND DISTORTION
NO SUPERIMPOSED ELEMENTS WITH TOLERANCE= 5.56000E-06
Checking MESH Connectivity...
2 Part(s) and 2 Sub-Domain(s) found
3072 ENVELOPE FACE(S) REMAINING FOR PART 1
5088 ENVELOPE FACE(S) REMAINING FOR PART 2
Occupied space: 129 Mb ( 6.55 %)
COMPUTING PART INFORMATION:
Part 1 Volume: 2.48400E+01
Part 2 Volume: 6.62400E+01
THIS MODEL SEEMS SUITABLE FOR A FEM FLUID APPROACH
CPU Stats --- Delta: 0:00:05 ( 4.94) Total: 0:00:05 ( 4.94)
Building FLUID / STRUCTURE interface
Using Model 1 as STRUCTURAL Model
Using Model 2 as FLUID Model
There are 950 interface node(s) on the FEM FLUID side
There are 241402 interface node(s) on the FEM STRUCTURE side
Generating INTERFACE mesh
Structural INTERFACE MESH contains 240000 elements
Fluid INTERFACE MESH contains 864 elements
Generating INTERFACE mesh
Structural INTERFACE MESH contains 240000 elements
Fluid INTERFACE MESH contains 864 elements
Computing FLUID Element System Matrices
Computing MASS and STIFFNESS elements matrices
using HIGH PRECISION STABILIZED scheme for linear elements
CPU Stats --- Delta: 0:00:08 ( 7.91) Total: 0:00:13 ( 12.85)
Computing VELOCITY matrices on elements faces
CPU Stats --- Delta: 0:00:00 ( 0.36) Total: 0:00:13 ( 13.21)
CPU Stats --- Delta: 0:00:00 ( 0.00) Total: 0:00:13 ( 13.21)
CPU Stats --- Delta: 0:00:00 ( 0.00) Total: 0:00:13 ( 13.21)
Running Bacon and Dynam ...
Terminaison anormale du shell. Exit status: 1
CPU Stats --- Delta: 0:44:19 ( 2658.57) Total: 0:44:32 ( 2671.78)
Reverse Cuthill McKee Ordering :
Old maximum bandwidth: 6050
New maximum bandwidth: 1199
Occupied space: 761 Mb ( 38.51 %)
Computing STRUCTURAL Element System Matrices
Reading Graph File ...
CPU Stats --- Delta: 0:01:25 ( 84.58) Total: 0:45:56 ( 2756.36)
Occupied space: 858 Mb ( 43.40 %)
CPU Stats --- Delta: 0:00:02 ( 1.78) Total: 0:45:58 ( 2758.14)
Occupied space: 858 Mb ( 43.42 %)
Computing COUPLING matrices for FLUID-STRUCTURE interface elements
****Interpolation between non-matching meshes:****
=== Coupling relation # 1
*The structural interface contained 240000
faces or elements (one or two-sided). 646
acoustic faces have been coupled to the structure.
*There were 115 orphaned nodes out of the 475 nodes of the interpolating
surface.
*There were 0 points interpolated with a nodal distance-based algorithm and 960000 points interpolated with an element-based algorithm.
*There were 0 structural faces with TRIM coupled to 0
acoustic faces.
=================
=== Coupling relation # 2
*The structural interface contained 240000
faces or elements (one or two-sided). 661
acoustic faces have been coupled to the structure.
*There were 106 orphaned nodes out of the 475 nodes of the interpolating
surface.
*There were 0 points interpolated with a nodal distance-based algorithm and 960000 points interpolated with an element-based algorithm.
*There were 0 structural faces with TRIM coupled to 0
acoustic faces.
=================
****End of interpolation information:****
CPU Stats --- Delta: 0:05:39 ( 338.86) Total: 0:51:37 ( 3097.00)
NOT ENOUGH MEMORY AVAILABLE
PLEASE RESIZE THE MEMORY ENVIRONMENT VARIABLE
AND RESTART YOUR APPLICATION
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 2013-7-5 14:17
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发表于 2013-7-5 22:27
