声振论坛

 找回密码
 我要加入

QQ登录

只需一步,快速开始

查看: 1799|回复: 4

[Virtual.Lab] 这个错误是耦合出了问题吗?

[复制链接]
发表于 2017-3-28 13:28 | 显示全部楼层 |阅读模式

马上注册,结交更多好友,享用更多功能,让你轻松玩转社区。

您需要 登录 才可以下载或查看,没有账号?我要加入

x
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.
xxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxx
xxxxxxxxxxxx  JOB EXECUTION START
xxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxx

                System for Computational Vibro-Acoustics
------------------------------------------------------------------------
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.
回复
分享到:

使用道具 举报

 楼主| 发表于 2017-3-28 13:28 | 显示全部楼层
ERROR :  Aborting Coupled Direct Response  procedure due to error...
 楼主| 发表于 2017-3-28 16:01 | 显示全部楼层
有没有同学能指导问题出在哪吗
发表于 2017-3-29 16:50 | 显示全部楼层
墨倾于池 发表于 2017-3-28 16:01
有没有同学能指导问题出在哪吗

从日志看不出来。
仔细检查下模型,材料,单元属性这类有没有定义错误。
 楼主| 发表于 2017-4-15 11:48 | 显示全部楼层
lengxuef 发表于 2017-3-29 16:50
从日志看不出来。
仔细检查下模型,材料,单元属性这类有没有定义错误。

不知道到为什么,重新启动lms又可以了,好像改变重新计算结果要出现一个弹窗,没有出现的话就会报错
您需要登录后才可以回帖 登录 | 我要加入

本版积分规则

QQ|小黑屋|Archiver|手机版|联系我们|声振论坛

GMT+8, 2024-12-26 00:23 , Processed in 0.067346 second(s), 17 queries , Gzip On.

Powered by Discuz! X3.4

Copyright © 2001-2021, Tencent Cloud.

快速回复 返回顶部 返回列表