Structuralists,
I am transitioning from OpenVSP 2 and SAM. Main current problem: ORIENTATION statements in simple Wing CalculiX .inp files (prior to adding the Vspaero loads). Specifics in Bold below.
These "ORIENTATION" errors are listed in the Command Prompt window (upon submitting the .inp file (excerpted below) to Calculix:
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on a Windows 8 machine, nodename LENOVOLAPTOP, release 6, version 6.2 9200, machine 8664
parameters:3 arguments:2
GL_MAX_EVAL_ORDER:8
Try to read ccx input
******************************************************************************
* read ccx input 4.4.2002 wi *
* *
* *
* -only free-format is supported. fixed format might cause a prg-crash. *
* *
* *
******************************************************************************
ignore statement: *NODEFILE
ignore statement: *NODEPRINT
8740 nodes reallocated
17564 elements reallocated
WARNING: option:ORIENTATION=OSkin_WingGeom_Struct0_0 not supported, keyword ignored
WARNING: *ORIENTATION not known. Data ignored.
WARNING: option:ORIENTATION=OSkin_WingGeom_Struct0_1 not supported, keyword ignored
WARNING: *ORIENTATION not known. Data ignored.
WARNING: *ELFILE not known. Data ignored.
WARNING: *ENDSTEP not known. Data ignored.
generate node-values for set:+dlo_ds0
fill dataset:0 name= +dlo
ncomps:2
Elements: 17564 Nodes:8740 Datasets:1 MinElemNr: 9002 MaxElemNr: 26565 MinNodNr:1 MaxNodNr:8740 read in 0.184000 sec
found elements of type 1: 0
found elements of type 2: 0
found elements of type 3: 0
found elements of type 4: 0
found elements of type 5: 0
found elements of type 6: 0
found elements of type 7: 17564
found elements of type 8: 0
found elements of type 9: 0
found elements of type 10: 0
found elements of type 11: 0
found elements of type 12: 0
ERROR in set:+dlo, face:2 of element:9002 does not exist.
ERROR in set:+dlo, face:2 of element:9003 does not exist.
ERROR in set:+dlo, face:2 of element:9004 does not exist.
ERROR in set:+dlo, face:2 of element:9005 does not exist.
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** Calculix structure data file generated from OpenVSP 3.43.0
** WingGeom_Struct0
** Num_Nodes: 8740
** Num_Els: 17564
** Num_Tris: 17564
** Num_Quads: 0
** Num_Beams: 0
** Node_Offset: 0
** Element_Offset: 9000
** Skin WingGeom_Struct0
*NODE, NSET=NSkin_WingGeom_Struct0
1,0.272982,0.000000,-0.000000
2,0.267240,0.000000,-0.133735
3,0.393504,0.000000,-0.000000
4,0.183007,0.000000,-0.000000
5,0.176764,0.000000,-0.112480
6,0.389627,0.000000,-0.154618
7,0.555346,0.000000,-0.000000
...
...
...
26562,6811,6813,8734
26563,8735,8634,6811
26564,8740,8642,8634
26565,8733,7060,8739
** Properties WingGeom_Struct0
*SHELL SECTION, ELSET=ESkin_WingGeom_Struct0_0, MATERIAL=Aluminum_7075-T6, ORIENTATION=OSkin_WingGeom_Struct0_0
0.00275
*ORIENTATION, NAME=OSkin_WingGeom_Struct0_0, SYSTEM=RECTANGULAR
0.311479,0.950253,-0.000000,0.0,0.0,1.0
*SHELL SECTION, ELSET=ESkin_WingGeom_Struct0_1, MATERIAL=Aluminum_7075-T6, ORIENTATION=OSkin_WingGeom_Struct0_1
0.00275
*ORIENTATION, NAME=OSkin_WingGeom_Struct0_1, SYSTEM=RECTANGULAR
0.311479,-0.950253,-0.000000,0.0,0.0,1.0
** Materials
*MATERIAL, NAME=Aluminum_7075-T6
*DENSITY
5.4245
*ELASTIC, TYPE=ISO
1.4832e+09, 0.33
*EXPANSION, TYPE=ISO
1.28e-05
[eof]
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[Environment: OpenVSP 3.43 on Win 11. CalculiX Version 2.10 from download of CalculiX-GE-OSS-2.10-win-x64.zip from Cesare Guardino's GE site. Same results with OpenVSP 3.3x,3.40 and earlier CalculiX's; and on Win 10 on another machine.]
[Goal: Structural analyses of varying wing skin thicknesses and rib/spar layouts for light-sport size traditional config aircraft.]
Thanks,
Peter Schwenn