Files
OneCAD-Simulation/crates/decks/tests/abaqus/cantilever.inp
T
a71f85eb58 Abaqus input writer and deck.write (M3) (#22)
* decks: Abaqus input writer with golden decks, read-back, Jacobian and unsupported tests

Co-Authored-By: Claude Opus 5.5 <noreply@anthropic.com>
Claude-Session: https://claude.ai/code/session_01NmAttHhUZTokgPeEJia8sm

* engine: deck.write command (format dispatch, atomic file write), docs

Co-Authored-By: Claude Opus 5.5 <noreply@anthropic.com>
Claude-Session: https://claude.ai/code/session_01NmAttHhUZTokgPeEJia8sm

* decks: format table, one resolve per write, direct buffer writes; engine: shared path parameter

Co-Authored-By: Claude Opus 5.5 <noreply@anthropic.com>
Claude-Session: https://claude.ai/code/session_01NmAttHhUZTokgPeEJia8sm

---------

Co-authored-by: jyviko <2501648+jyviko@users.noreply.github.com>
Co-authored-by: Claude Opus 5.5 <noreply@anthropic.com>
2026-10-13 17:27:44 -04:00

76 lines
1.4 KiB
Plaintext

*HEADING
ModelCraft model, units mm-t-s-N-MPa
** Written by ModelCraft. The numbers are in one consistent unit system and are not converted.
** Nodes
*NODE
1, 0.0, 0.0, 0.0
2, 0.0, 0.0, 10.0
3, 0.0, 10.0, 0.0
4, 0.0, 10.0, 10.0
5, 25.0, 0.0, 0.0
6, 25.0, 0.0, 10.0
7, 25.0, 10.0, 0.0
8, 25.0, 10.0, 10.0
9, 50.0, 0.0, 0.0
10, 50.0, 0.0, 10.0
11, 50.0, 10.0, 0.0
12, 50.0, 10.0, 10.0
13, 75.0, 0.0, 0.0
14, 75.0, 0.0, 10.0
15, 75.0, 10.0, 0.0
16, 75.0, 10.0, 10.0
17, 100.0, 0.0, 0.0
18, 100.0, 0.0, 10.0
19, 100.0, 10.0, 0.0
20, 100.0, 10.0, 10.0
** Elements
*ELEMENT, TYPE=C3D8I
1, 1, 5, 7, 3, 2, 6, 8, 4
2, 5, 9, 11, 7, 6, 10, 12, 8
3, 9, 13, 15, 11, 10, 14, 16, 12
4, 13, 17, 19, 15, 14, 18, 20, 16
** Sets
*NSET, NSET=all
1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16
17, 18, 19, 20
*ELSET, ELSET=all
1, 2, 3, 4
*NSET, NSET=root
1, 2, 3, 4
*SURFACE, TYPE=ELEMENT, NAME=root
1, S6
*NSET, NSET=tip
17, 18, 19, 20
*SURFACE, TYPE=ELEMENT, NAME=tip
4, S4
** Materials
*MATERIAL, NAME=Steel
*ELASTIC, TYPE=ISOTROPIC
210000.0, 0.3
*DENSITY
7.85E-9
** Sections
** section beam
*SOLID SECTION, ELSET=all, MATERIAL=Steel
,
** Initial state: boundary conditions active in every step
*BOUNDARY
** boundary condition clamp
root, ENCASTRE
** Step Bend
*STEP, NAME=Bend, NLGEOM=NO
*STATIC
1.0, 1.0
** boundary conditions: as in the base state
*CLOAD, OP=NEW
17, 3, -25.0
18, 3, -25.0
19, 3, -25.0
20, 3, -25.0
*OUTPUT, FIELD, OP=NEW
*NODE OUTPUT
U, RF
*ELEMENT OUTPUT
S, E
*END STEP