*** ERROR # 827 ***
FEM model for eigenvalue analysis was created with Femap with NASTRAN.
The file extension is dat.
However, the analysis at NASTRAN took a very long time.
So, I want to import this into HyperMesh, and perform eigenvalue analysis with Optistruct.
When I operated as shown, I got the following error:
<?xml version="1.0" encoding="UTF-8"?>
*** ERROR # 827 ***
Invalid ASET run, PARAM,EXTOUT,DMIGPCH or
PARAM,EXTOUT,DMIGBIN must be specified for DMIG output.
How do I resolve the error?
Reference documents are more helpful.
Also, I want to perform frequency response analysis with Optistruct on the same model too.
The following is an excerpt of dat data.
INIT MASTER(S)
NASTRAN SYSTEM(319)=1
ID Neo66B,Femap
SOL SEMODES
TIME 10000
CEND
TITLE = MSC/MD Nastran モード 解析セット
ECHO = NONE
MFLUID = 1
DISPLACEMENT(PLOT) = ALL
METHOD = 1
BEGIN BULK
$ ***************************************************************************
$ Written by : Femap with NX Nastran
$ Version : 11.1.1
$ Translator : MSC/MD Nastran
$ From Model : \Neo66BC_Hull-vibration_Standard.modfem
$ Date : Mon Jul 14 08:00:18 2014
$ ***************************************************************************
$
PARAM,POST,-1
PARAM,OGEOM,NO
PARAM,AUTOSPC,YES
PARAM,GRDPNT,0
EIGRL 1 .5 30. 0 MASS
CORD2C 1 0 0. 0. 0. 0. 0. 1.+FEMAPC1
+FEMAPC1 1. 0. 1.
CORD2S 2 0 0. 0. 0. 0. 0. 1.+FEMAPC2
+FEMAPC2 1. 0. 1.
$ Femap with NX Nastran Constraint Set 1 : ASET
ASET 3 123
...
ASET 50126 123
$ Femap with NX Nastran Property 20108000 : Mat01_t8.0
PSHELL 20108000 1 8. 1 1 0.
...
ELIST 1 200001 200002 200003 200004 200005 200006 200007+
...
+ 208872 208873 208874 208875 208876 208877
$ Femap with NX Nastran Region 1 : 無題
MFLUID 1 0 5375. 1.025-9 1 N N
ENDDATA
Answers
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NX Nastran (Femap) has some different card comparing to Altair's Optistruct. So you have to do attention to this conversion.
0 -
Hey,
Try to import your *.dat file using :
Then redefine your configuration : Eigenvalues solver ..... and then solve them with OptiStruct.
If the model is large (you have a lot dof), try to use AMSES solver instead of Lanczos
Cheers,
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Tank you reply.
Import *.dat file and save as test.hm file
Add cmsmesh
Save as test.fem file and solve with optistruct
<?xml version="1.0" encoding="UTF-8"?>
So, this fatal error appeared
How do I resolve the error?
The following is an excerpt of fem data.
$$
$$ Optistruct Input Deck Generated by HyperMesh Version : 2017.2.0.16
$$ Generated using HyperMesh-Optistruct Template Version : 2017.2
$$
$$ Template: optistruct
$$
$$
$$ optistruct
$
TITLE = MSC/MD Nastran [ h Z b g
METHOD(STRUCTURE) = 1
MFLUID = 1
DISPLACEMENT(PLOT) = ALL
$$------------------------------------------------------------------------------$
$$ Case Control Cards $
$$------------------------------------------------------------------------------$
INIT MASTER(S)
NASTRAN SYSTEM(319)=1
ID Neo66B,Femap
SOL SEMODES
TIME 10000
CEND
ECHO = NONE
$$--------------------------------------------------------------
$$ HYPERMESH TAGS
$$--------------------------------------------------------------
$$BEGIN TAGS
$$END TAGS
$
BEGIN BULK
$$
$$ Stacking Information for Ply-Based Composite Definition
$$...
...
...
ASET 50109 123
ASET 50126 123
$$
$$ MFLUID cards
$$
$HMNAME LOADCOL 2'MFLUID2'
$HWCOLOR LOADCOL 2 4
$$
MFLUID 2 0 5375.0 1.025-9 1 N N
+ 1.0+10
$
$$
$$ CMSMETH cards
$$
$HMNAME LOADCOL 4'CMSMETH'
$HWCOLOR LOADCOL 4 4
$$
CMSMETH 4 CB 30.0 AMSES$
ENDDATA
$$
$$------------------------------------------------------------------------------$$
$$ Data Definition for AutoDV $$
$$------------------------------------------------------------------------------$$
$$
$$-----------------------------------------------------------------------------$$
$$ Design Variables Card for Control Perturbations $$
$$-----------------------------------------------------------------------------$$
$$
$$------------------------------------------------------------------------------$
$$ Domain Element Definitions $
$$------------------------------------------------------------------------------$
$$
$$------------------------------------------------------------------------------$$
$$ Control Perturbation $$
$$------------------------------------------------------------------------------$$0 -
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