forked from 1b-agent/fieldcraft-upstream
jyvikoandClaude Opus 5.5
6d9452ad84
The oracle binary (modelcraft-testkit) runs each case's recipe through the command engine, measures its quantities by JSON pointers into step outputs or commands, compares them with the cited references and the frozen fixtures, and writes docs/oracle.md. 20 theory cases (patch tests of every solid element, Timoshenko cantilevers, Lame, Kirsch, beam frequencies, torsion and bending through couplings, explicit waves and impact, CDT invariants), 8 published benchmarks (MacNeal-Harder patch, straight and curved cantilevers, thick cylinder, Scordelis-Lo with solids, NAFEMS LE1, LE10, FV32) and 10 pending cases with citations. Co-Authored-By: Claude Opus 5.5 <[email protected]> Claude-Session: https://claude.ai/code/session_01NmAttHhUZTokgPeEJia8sm
86 lines
2.8 KiB
JSON
86 lines
2.8 KiB
JSON
{
|
||
"title": "NAFEMS FV32 cantilevered tapered membrane, free vibration (hex20 plane stress layer)",
|
||
"kind": "benchmark",
|
||
"source": "NAFEMS, The Standard NAFEMS Benchmarks, TNSB Rev. 3, October 1990, test FV32 (frequencies 44.623, 130.03, 162.70, 246.05, 379.90, 391.44 Hz); as reproduced in the Abaqus 2017 Benchmarks Guide, 'FV32: Cantilevered tapered membrane'",
|
||
"quantities": [
|
||
{
|
||
"id": "f1",
|
||
"quantity": "frequency of mode 1 (Hz)",
|
||
"measure": {
|
||
"from": "modes",
|
||
"pointer": "/modes/0/frequency"
|
||
},
|
||
"value": 44.623,
|
||
"tolerance": {
|
||
"relative": 0.01
|
||
},
|
||
"reason": "targets published to five figures for 2D plane stress; a thin solid layer with a free face differs from plane stress by O((t/L)²) and the 16 × 8 quadratic mesh is converged to about 0.1%"
|
||
},
|
||
{
|
||
"id": "f2",
|
||
"quantity": "frequency of mode 2 (Hz)",
|
||
"measure": {
|
||
"from": "modes",
|
||
"pointer": "/modes/1/frequency"
|
||
},
|
||
"value": 130.03,
|
||
"tolerance": {
|
||
"relative": 0.01
|
||
},
|
||
"reason": "targets published to five figures for 2D plane stress; a thin solid layer with a free face differs from plane stress by O((t/L)²) and the 16 × 8 quadratic mesh is converged to about 0.1%"
|
||
},
|
||
{
|
||
"id": "f3",
|
||
"quantity": "frequency of mode 3 (Hz)",
|
||
"measure": {
|
||
"from": "modes",
|
||
"pointer": "/modes/2/frequency"
|
||
},
|
||
"value": 162.7,
|
||
"tolerance": {
|
||
"relative": 0.01
|
||
},
|
||
"reason": "targets published to five figures for 2D plane stress; a thin solid layer with a free face differs from plane stress by O((t/L)²) and the 16 × 8 quadratic mesh is converged to about 0.1%"
|
||
},
|
||
{
|
||
"id": "f4",
|
||
"quantity": "frequency of mode 4 (Hz)",
|
||
"measure": {
|
||
"from": "modes",
|
||
"pointer": "/modes/3/frequency"
|
||
},
|
||
"value": 246.05,
|
||
"tolerance": {
|
||
"relative": 0.01
|
||
},
|
||
"reason": "targets published to five figures for 2D plane stress; a thin solid layer with a free face differs from plane stress by O((t/L)²) and the 16 × 8 quadratic mesh is converged to about 0.1%"
|
||
},
|
||
{
|
||
"id": "f5",
|
||
"quantity": "frequency of mode 5 (Hz)",
|
||
"measure": {
|
||
"from": "modes",
|
||
"pointer": "/modes/4/frequency"
|
||
},
|
||
"value": 379.9,
|
||
"tolerance": {
|
||
"relative": 0.01
|
||
},
|
||
"reason": "targets published to five figures for 2D plane stress; a thin solid layer with a free face differs from plane stress by O((t/L)²) and the 16 × 8 quadratic mesh is converged to about 0.1%"
|
||
},
|
||
{
|
||
"id": "f6",
|
||
"quantity": "frequency of mode 6 (Hz)",
|
||
"measure": {
|
||
"from": "modes",
|
||
"pointer": "/modes/5/frequency"
|
||
},
|
||
"value": 391.44,
|
||
"tolerance": {
|
||
"relative": 0.01
|
||
},
|
||
"reason": "targets published to five figures for 2D plane stress; a thin solid layer with a free face differs from plane stress by O((t/L)²) and the 16 × 8 quadratic mesh is converged to about 0.1%"
|
||
}
|
||
]
|
||
}
|