task_id stringlengths 12 28 | track stringclasses 2
values | tier stringclasses 2
values | family stringlengths 11 26 | title stringlengths 26 73 | physics listlengths 1 3 | prompt stringlengths 1.14k 5.87k | inputs listlengths 0 6 | outputs listlengths 1 6 | complexity unknown | source unknown | status stringclasses 1
value | engineering_family stringlengths 11 26 | readiness dict | required_artifacts listlengths 8 8 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
A-AGENTFEM-fresh_test_000 | A | source_backed_pilot | agentfem-bracket | AgentFEM bracket fresh_test_000 (10000 N seat load) | [
"linear static"
] | Support bracket (one member of a parametric double-arm bracket family). geometry.step holds one solid in millimetres (height 189 mm).
Material: linear isotropic elastic, E = 70 GPa, Poisson ratio 0.33 (density 2700 kg/m^3, gravity not applied).
Supports: the foot undersides, i.e. every face lying in the plane z = 0, a... | [
{
"path": "tasks/A-AGENTFEM-fresh_test_000/geometry.step",
"role": "cad",
"bytes": 229820,
"sha256": "8c1992353e0c433930ea5b5613a8d57ad056093807f5578c9b2c83bf29556914"
}
] | [
{
"key": "seat_mean_displacement_mm",
"unit": "mm",
"definition": "mean of the downward displacement -u_z over the top seat face (z = 189 mm)"
},
{
"key": "max_displacement_mm",
"unit": "mm",
"definition": "maximum displacement magnitude anywhere in the bracket"
}
] | {
"solids": 1,
"faces": 24,
"assembly": false
} | {
"name": "AgentFEM Bracket Elasticity (Haoming Luo, 2026)",
"url": "https://huggingface.co/datasets/HaomingLuo/AgentFEM-Bracket-Elasticity",
"license": "CC BY 4.0",
"redistributable": true
} | active | agentfem-bracket | {
"independently_reproduced": true,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-AGENTFEM-fresh_test_001 | A | source_backed_pilot | agentfem-bracket | AgentFEM bracket fresh_test_001 (10000 N seat load) | [
"linear static"
] | Support bracket (one member of a parametric double-arm bracket family). geometry.step holds one solid in millimetres (height 189 mm).
Material: linear isotropic elastic, E = 70 GPa, Poisson ratio 0.33 (density 2700 kg/m^3, gravity not applied).
Supports: the foot undersides, i.e. every face lying in the plane z = 0, a... | [
{
"path": "tasks/A-AGENTFEM-fresh_test_001/geometry.step",
"role": "cad",
"bytes": 224493,
"sha256": "ede5a95bef714b253cd0ed56aef9c987d3ef7b42270ae26b645010b73f79eb5d"
}
] | [
{
"key": "seat_mean_displacement_mm",
"unit": "mm",
"definition": "mean of the downward displacement -u_z over the top seat face (z = 189 mm)"
},
{
"key": "max_displacement_mm",
"unit": "mm",
"definition": "maximum displacement magnitude anywhere in the bracket"
}
] | {
"solids": 1,
"faces": 24,
"assembly": false
} | {
"name": "AgentFEM Bracket Elasticity (Haoming Luo, 2026)",
"url": "https://huggingface.co/datasets/HaomingLuo/AgentFEM-Bracket-Elasticity",
"license": "CC BY 4.0",
"redistributable": true
} | active | agentfem-bracket | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-AGENTFEM-fresh_test_002 | A | source_backed_pilot | agentfem-bracket | AgentFEM bracket fresh_test_002 (10000 N seat load) | [
"linear static"
] | Support bracket (one member of a parametric double-arm bracket family). geometry.step holds one solid in millimetres (height 189 mm).
Material: linear isotropic elastic, E = 70 GPa, Poisson ratio 0.33 (density 2700 kg/m^3, gravity not applied).
Supports: the foot undersides, i.e. every face lying in the plane z = 0, a... | [
{
"path": "tasks/A-AGENTFEM-fresh_test_002/geometry.step",
"role": "cad",
"bytes": 214936,
"sha256": "cac6f45c64f7af1b4b8a9879810cd463aa7a459e3b09df6309f7913c264b3dbc"
}
] | [
{
"key": "seat_mean_displacement_mm",
"unit": "mm",
"definition": "mean of the downward displacement -u_z over the top seat face (z = 189 mm)"
},
{
"key": "max_displacement_mm",
"unit": "mm",
"definition": "maximum displacement magnitude anywhere in the bracket"
}
] | {
"solids": 1,
"faces": 24,
"assembly": false
} | {
"name": "AgentFEM Bracket Elasticity (Haoming Luo, 2026)",
"url": "https://huggingface.co/datasets/HaomingLuo/AgentFEM-Bracket-Elasticity",
"license": "CC BY 4.0",
"redistributable": true
} | active | agentfem-bracket | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-AGENTFEM-fresh_test_003 | A | source_backed_pilot | agentfem-bracket | AgentFEM bracket fresh_test_003 (10000 N seat load) | [
"linear static"
] | Support bracket (one member of a parametric double-arm bracket family). geometry.step holds one solid in millimetres (height 189 mm).
Material: linear isotropic elastic, E = 70 GPa, Poisson ratio 0.33 (density 2700 kg/m^3, gravity not applied).
Supports: the foot undersides, i.e. every face lying in the plane z = 0, a... | [
{
"path": "tasks/A-AGENTFEM-fresh_test_003/geometry.step",
"role": "cad",
"bytes": 229956,
"sha256": "d630a0f4091bf4e1db5f17bd9e48321925ea45fe5dac740a57830e6c437bc549"
}
] | [
{
"key": "seat_mean_displacement_mm",
"unit": "mm",
"definition": "mean of the downward displacement -u_z over the top seat face (z = 189 mm)"
},
{
"key": "max_displacement_mm",
"unit": "mm",
"definition": "maximum displacement magnitude anywhere in the bracket"
}
] | {
"solids": 1,
"faces": 24,
"assembly": false
} | {
"name": "AgentFEM Bracket Elasticity (Haoming Luo, 2026)",
"url": "https://huggingface.co/datasets/HaomingLuo/AgentFEM-Bracket-Elasticity",
"license": "CC BY 4.0",
"redistributable": true
} | active | agentfem-bracket | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-AGENTFEM-fresh_test_004 | A | source_backed_pilot | agentfem-bracket | AgentFEM bracket fresh_test_004 (10000 N seat load) | [
"linear static"
] | Support bracket (one member of a parametric double-arm bracket family). geometry.step holds one solid in millimetres (height 189 mm).
Material: linear isotropic elastic, E = 70 GPa, Poisson ratio 0.33 (density 2700 kg/m^3, gravity not applied).
Supports: the foot undersides, i.e. every face lying in the plane z = 0, a... | [
{
"path": "tasks/A-AGENTFEM-fresh_test_004/geometry.step",
"role": "cad",
"bytes": 209985,
"sha256": "7fa1cd62b095e6224f61f0b600619a4865c8b760eccfaa2b31074afb659ce06b"
}
] | [
{
"key": "seat_mean_displacement_mm",
"unit": "mm",
"definition": "mean of the downward displacement -u_z over the top seat face (z = 189 mm)"
},
{
"key": "max_displacement_mm",
"unit": "mm",
"definition": "maximum displacement magnitude anywhere in the bracket"
}
] | {
"solids": 1,
"faces": 24,
"assembly": false
} | {
"name": "AgentFEM Bracket Elasticity (Haoming Luo, 2026)",
"url": "https://huggingface.co/datasets/HaomingLuo/AgentFEM-Bracket-Elasticity",
"license": "CC BY 4.0",
"redistributable": true
} | active | agentfem-bracket | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-AGENTFEM-fresh_test_008 | A | source_backed_pilot | agentfem-bracket | AgentFEM bracket fresh_test_008 (10000 N seat load) | [
"linear static"
] | Support bracket (one member of a parametric double-arm bracket family). geometry.step holds one solid in millimetres (height 189 mm).
Material: linear isotropic elastic, E = 70 GPa, Poisson ratio 0.33 (density 2700 kg/m^3, gravity not applied).
Supports: the foot undersides, i.e. every face lying in the plane z = 0, a... | [
{
"path": "tasks/A-AGENTFEM-fresh_test_008/geometry.step",
"role": "cad",
"bytes": 230256,
"sha256": "8557c19c923f034573650e4ff42b73a3f63998dbe95ca3dea7089574fe36fc8e"
}
] | [
{
"key": "seat_mean_displacement_mm",
"unit": "mm",
"definition": "mean of the downward displacement -u_z over the top seat face (z = 189 mm)"
},
{
"key": "max_displacement_mm",
"unit": "mm",
"definition": "maximum displacement magnitude anywhere in the bracket"
}
] | {
"solids": 1,
"faces": 24,
"assembly": false
} | {
"name": "AgentFEM Bracket Elasticity (Haoming Luo, 2026)",
"url": "https://huggingface.co/datasets/HaomingLuo/AgentFEM-Bracket-Elasticity",
"license": "CC BY 4.0",
"redistributable": true
} | active | agentfem-bracket | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-AGENTFEM-fresh_test_013 | A | source_backed_pilot | agentfem-bracket | AgentFEM bracket fresh_test_013 (10000 N seat load) | [
"linear static"
] | Support bracket (one member of a parametric double-arm bracket family). geometry.step holds one solid in millimetres (height 189 mm).
Material: linear isotropic elastic, E = 70 GPa, Poisson ratio 0.33 (density 2700 kg/m^3, gravity not applied).
Supports: the foot undersides, i.e. every face lying in the plane z = 0, a... | [
{
"path": "tasks/A-AGENTFEM-fresh_test_013/geometry.step",
"role": "cad",
"bytes": 235860,
"sha256": "bac801aba7069b0853035bf9a5b2fcd1d6da3aae108a878f3c20a0ecf5454c14"
}
] | [
{
"key": "seat_mean_displacement_mm",
"unit": "mm",
"definition": "mean of the downward displacement -u_z over the top seat face (z = 189 mm)"
},
{
"key": "max_displacement_mm",
"unit": "mm",
"definition": "maximum displacement magnitude anywhere in the bracket"
}
] | {
"solids": 1,
"faces": 24,
"assembly": false
} | {
"name": "AgentFEM Bracket Elasticity (Haoming Luo, 2026)",
"url": "https://huggingface.co/datasets/HaomingLuo/AgentFEM-Bracket-Elasticity",
"license": "CC BY 4.0",
"redistributable": true
} | active | agentfem-bracket | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-AGENTFEM-fresh_test_024 | A | source_backed_pilot | agentfem-bracket | AgentFEM bracket fresh_test_024 (10000 N seat load) | [
"linear static"
] | Support bracket (one member of a parametric double-arm bracket family). geometry.step holds one solid in millimetres (height 189 mm).
Material: linear isotropic elastic, E = 70 GPa, Poisson ratio 0.33 (density 2700 kg/m^3, gravity not applied).
Supports: the foot undersides, i.e. every face lying in the plane z = 0, a... | [
{
"path": "tasks/A-AGENTFEM-fresh_test_024/geometry.step",
"role": "cad",
"bytes": 218128,
"sha256": "5df9d1a04abd5e7f163d472dc9074a08f1be82a3dd62abe2b2fcda8da4297b4e"
}
] | [
{
"key": "seat_mean_displacement_mm",
"unit": "mm",
"definition": "mean of the downward displacement -u_z over the top seat face (z = 189 mm)"
},
{
"key": "max_displacement_mm",
"unit": "mm",
"definition": "maximum displacement magnitude anywhere in the bracket"
}
] | {
"solids": 1,
"faces": 24,
"assembly": false
} | {
"name": "AgentFEM Bracket Elasticity (Haoming Luo, 2026)",
"url": "https://huggingface.co/datasets/HaomingLuo/AgentFEM-Bracket-Elasticity",
"license": "CC BY 4.0",
"redistributable": true
} | active | agentfem-bracket | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-CADWORLD-001 | A | source_backed_pilot | cadworld-freecad-fem | CADWorld: Multi-feature aluminium part, end load | [
"linear static"
] | FreeCAD/CalculiX benchmark part (Multi-feature aluminium part, end load). part.step is the single solid in millimetres (38 faces, bounding box [-130.0, -0.0, -30.0, 130.0, 30.0, 30.0] mm). faces.json describes every face.
Material: AlMg3F24, linear isotropic elastic, E = 70000 MPa, Poisson ratio 0.3.
Analysis: linear ... | [
{
"path": "tasks/A-CADWORLD-001/part.step",
"role": "cad",
"bytes": 135694,
"sha256": "966cf92e8b96f838b6094ad8bf620181aa52c3c8472db843fb2ff3db33e3caef"
},
{
"path": "tasks/A-CADWORLD-001/faces.json",
"role": "spec",
"bytes": 11860,
"sha256": "7a81effce09d4091629f44c92780204b030b... | [
{
"key": "max_displacement_mm",
"unit": "mm",
"definition": "maximum nodal displacement magnitude"
},
{
"key": "max_von_mises_MPa",
"unit": "MPa",
"definition": "maximum nodal von Mises stress"
},
{
"key": "max_shear_stress_MPa",
"unit": "MPa",
"definition": "maximum over... | {
"solids": 1,
"faces": 38,
"assembly": false,
"cad_bbox_mm": [
-130,
0,
-30,
130,
30,
30
]
} | {
"name": "CADWorld FEM benchmark (Zdong104/CADWORLD; HF Zihan1004/CADWORLD)",
"url": "https://github.com/Zdong104/CADWORLD",
"license": "Apache-2.0 (publisher HF metadata)",
"redistributable": true
} | active | cadworld-freecad-fem | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-CYC-Coupler-PETGCF | A | source_backed_pilot | cycloidal-drive-components | Cycloidal drive: output coupler (PETG-CF) | [
"linear static"
] | Component analysis: the output coupler of an open-source, 3D-printable 15:1 cycloidal gearbox. part.step holds the single solid in millimetres (33 faces, volume 2063 mm^3). faces.json lists every face with its index, type, area, centroid and normal/axis; use the geometry, not a CAD system's own face numbering.
Materia... | [
{
"path": "tasks/A-CYC-Coupler-PETGCF/part.step",
"role": "cad",
"bytes": 152731,
"sha256": "6334fd4b5ff639db8269d48725fb280b856f33767ad93f8619375904007797d1"
},
{
"path": "tasks/A-CYC-Coupler-PETGCF/faces.json",
"role": "spec",
"bytes": 11998,
"sha256": "101f4fb7c3c3a2060ecbdca8... | [
{
"key": "max_displacement_mm",
"unit": "mm",
"definition": "maximum nodal displacement magnitude in the part"
}
] | {
"solids": 1,
"faces": 33,
"assembly": false,
"cad_bbox_mm": [
69.0254,
-10,
10.5,
84.0254,
10,
30.5
]
} | {
"name": "3D-printable cycloidal drive FEA (jagathsrujan/3d-printable-cycloidal-drive)",
"url": "https://github.com/jagathsrujan/3d-printable-cycloidal-drive",
"license": "No repository license; FCStd metadata 'All rights reserved'. Local research only.",
"redistributable": false
} | active | cycloidal-drive-components | {
"independently_reproduced": true,
"workflow_scoring": "trusted_review_required",
"tolerances": "convergence_study"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-CYC-Disk-PETGCF | A | source_backed_pilot | cycloidal-drive-components | Cycloidal drive: cycloidal disk (PETG-CF) | [
"linear static"
] | Component analysis: the cycloidal disk of an open-source, 3D-printable 15:1 cycloidal gearbox. part.step holds the single solid in millimetres (20 faces, volume 15595 mm^3). faces.json lists every face with its index, type, area, centroid and normal/axis; use the geometry, not a CAD system's own face numbering.
Materi... | [
{
"path": "tasks/A-CYC-Disk-PETGCF/part.step",
"role": "cad",
"bytes": 261680,
"sha256": "64a4b1671230bac1994617c407075e06a6636f861ab4695e0ae75c7edf6c719e"
},
{
"path": "tasks/A-CYC-Disk-PETGCF/faces.json",
"role": "spec",
"bytes": 7425,
"sha256": "7cc06b9686d21af8424923ae37141a9... | [
{
"key": "max_displacement_mm",
"unit": "mm",
"definition": "maximum nodal displacement magnitude in the part"
}
] | {
"solids": 1,
"faces": 20,
"assembly": false,
"cad_bbox_mm": [
99.0254,
-39.6646,
-17.3105,
104.0254,
39.9431,
61.9946
]
} | {
"name": "3D-printable cycloidal drive FEA (jagathsrujan/3d-printable-cycloidal-drive)",
"url": "https://github.com/jagathsrujan/3d-printable-cycloidal-drive",
"license": "No repository license; FCStd metadata 'All rights reserved'. Local research only.",
"redistributable": false
} | active | cycloidal-drive-components | {
"independently_reproduced": true,
"workflow_scoring": "trusted_review_required",
"tolerances": "convergence_study"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-CYC-FlangeP1-PETGCF | A | source_backed_pilot | cycloidal-drive-components | Cycloidal drive: output flange P1 (PETG-CF) | [
"linear static"
] | Component analysis: the output flange P1 of an open-source, 3D-printable 15:1 cycloidal gearbox. part.step holds the single solid in millimetres (45 faces, volume 16002 mm^3). faces.json lists every face with its index, type, area, centroid and normal/axis; use the geometry, not a CAD system's own face numbering.
Mate... | [
{
"path": "tasks/A-CYC-FlangeP1-PETGCF/part.step",
"role": "cad",
"bytes": 142438,
"sha256": "297c5a6badd991931895ffd502eb2038701e9b3423f1d06bfb82574c87a5b976"
},
{
"path": "tasks/A-CYC-FlangeP1-PETGCF/faces.json",
"role": "spec",
"bytes": 16297,
"sha256": "88680e902954dcaac7f7ff... | [
{
"key": "max_displacement_mm",
"unit": "mm",
"definition": "maximum nodal displacement magnitude in the part"
}
] | {
"solids": 1,
"faces": 45,
"assembly": false,
"cad_bbox_mm": [
85.0254,
-30,
-9.5,
98.0254,
30,
50.5
]
} | {
"name": "3D-printable cycloidal drive FEA (jagathsrujan/3d-printable-cycloidal-drive)",
"url": "https://github.com/jagathsrujan/3d-printable-cycloidal-drive",
"license": "No repository license; FCStd metadata 'All rights reserved'. Local research only.",
"redistributable": false
} | active | cycloidal-drive-components | {
"independently_reproduced": true,
"workflow_scoring": "trusted_review_required",
"tolerances": "convergence_study"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-CYC-FlangeP2-PETGCF | A | source_backed_pilot | cycloidal-drive-components | Cycloidal drive: output flange P2 (PETG-CF) | [
"linear static"
] | Component analysis: the output flange P2 of an open-source, 3D-printable 15:1 cycloidal gearbox. part.step holds the single solid in millimetres (48 faces, volume 18891 mm^3). faces.json lists every face with its index, type, area, centroid and normal/axis; use the geometry, not a CAD system's own face numbering.
Mate... | [
{
"path": "tasks/A-CYC-FlangeP2-PETGCF/part.step",
"role": "cad",
"bytes": 157251,
"sha256": "be8d09fac47699b12b584875665b6b303c3db0ea96375811f37e94e120e26d26"
},
{
"path": "tasks/A-CYC-FlangeP2-PETGCF/faces.json",
"role": "spec",
"bytes": 17395,
"sha256": "537888fd552b0e8791197b... | [
{
"key": "max_displacement_mm",
"unit": "mm",
"definition": "maximum nodal displacement magnitude in the part"
}
] | {
"solids": 1,
"faces": 48,
"assembly": false,
"cad_bbox_mm": [
113.0254,
-30,
-9.5,
129.0254,
30,
50.5
]
} | {
"name": "3D-printable cycloidal drive FEA (jagathsrujan/3d-printable-cycloidal-drive)",
"url": "https://github.com/jagathsrujan/3d-printable-cycloidal-drive",
"license": "No repository license; FCStd metadata 'All rights reserved'. Local research only.",
"redistributable": false
} | active | cycloidal-drive-components | {
"independently_reproduced": true,
"workflow_scoring": "trusted_review_required",
"tolerances": "convergence_study"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-CYC-Mount-PETGCF | A | source_backed_pilot | cycloidal-drive-components | Cycloidal drive: motor mount (PETG-CF) | [
"linear static"
] | Component analysis: the motor mount of an open-source, 3D-printable 15:1 cycloidal gearbox. part.step holds the single solid in millimetres (40 faces, volume 24198 mm^3). faces.json lists every face with its index, type, area, centroid and normal/axis; use the geometry, not a CAD system's own face numbering.
Material:... | [
{
"path": "tasks/A-CYC-Mount-PETGCF/part.step",
"role": "cad",
"bytes": 148631,
"sha256": "e0ba13feb4296462ef7ac3d9dc3e7deb5eb58fc80f474f96260bf5489ff12eff"
},
{
"path": "tasks/A-CYC-Mount-PETGCF/faces.json",
"role": "spec",
"bytes": 13643,
"sha256": "c003001165cfa78eaa021ea4e716... | [
{
"key": "max_displacement_mm",
"unit": "mm",
"definition": "maximum nodal displacement magnitude in the part"
}
] | {
"solids": 1,
"faces": 40,
"assembly": false,
"cad_bbox_mm": [
60.0254,
-37,
-0.5,
84.0254,
37,
41.5
]
} | {
"name": "3D-printable cycloidal drive FEA (jagathsrujan/3d-printable-cycloidal-drive)",
"url": "https://github.com/jagathsrujan/3d-printable-cycloidal-drive",
"license": "No repository license; FCStd metadata 'All rights reserved'. Local research only.",
"redistributable": false
} | active | cycloidal-drive-components | {
"independently_reproduced": true,
"workflow_scoring": "trusted_review_required",
"tolerances": "convergence_study"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-CYC-Ring1x6-PETGCF | A | source_backed_pilot | cycloidal-drive-components | Cycloidal drive: spacer ring 1x6 (PETG-CF) | [
"linear static"
] | Component analysis: the spacer ring 1x6 of an open-source, 3D-printable 15:1 cycloidal gearbox. part.step holds the single solid in millimetres (6 faces, volume 27 mm^3). faces.json lists every face with its index, type, area, centroid and normal/axis; use the geometry, not a CAD system's own face numbering.
Material:... | [
{
"path": "tasks/A-CYC-Ring1x6-PETGCF/part.step",
"role": "cad",
"bytes": 17760,
"sha256": "3e78e14d96f13e8a80f8dd528e1f48c7eaf878391f3395a3b59c7f0a80a69603"
},
{
"path": "tasks/A-CYC-Ring1x6-PETGCF/faces.json",
"role": "spec",
"bytes": 2218,
"sha256": "cfba8410fe1b68c561d6995002... | [
{
"key": "max_displacement_mm",
"unit": "mm",
"definition": "maximum nodal displacement magnitude in the part"
}
] | {
"solids": 1,
"faces": 6,
"assembly": false,
"cad_bbox_mm": [
98.0254,
15.2683,
31.174,
99.0254,
23.6683,
39.574
]
} | {
"name": "3D-printable cycloidal drive FEA (jagathsrujan/3d-printable-cycloidal-drive)",
"url": "https://github.com/jagathsrujan/3d-printable-cycloidal-drive",
"license": "No repository license; FCStd metadata 'All rights reserved'. Local research only.",
"redistributable": false
} | active | cycloidal-drive-components | {
"independently_reproduced": true,
"workflow_scoring": "trusted_review_required",
"tolerances": "convergence_study"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-CYC-Ring4x6-PETGCF | A | source_backed_pilot | cycloidal-drive-components | Cycloidal drive: spacer ring 4x6 (PETG-CF) | [
"linear static"
] | Component analysis: the spacer ring 4x6 of an open-source, 3D-printable 15:1 cycloidal gearbox. part.step holds the single solid in millimetres (6 faces, volume 81 mm^3). faces.json lists every face with its index, type, area, centroid and normal/axis; use the geometry, not a CAD system's own face numbering.
Material:... | [
{
"path": "tasks/A-CYC-Ring4x6-PETGCF/part.step",
"role": "cad",
"bytes": 17760,
"sha256": "fa325d5673247ba3b5e94c3542f35b06e3b6fc10e42747466b971e376b06031d"
},
{
"path": "tasks/A-CYC-Ring4x6-PETGCF/faces.json",
"role": "spec",
"bytes": 2242,
"sha256": "aa23e0e48de63c6a42f00e71cd... | [
{
"key": "max_displacement_mm",
"unit": "mm",
"definition": "maximum nodal displacement magnitude in the part"
}
] | {
"solids": 1,
"faces": 6,
"assembly": false,
"cad_bbox_mm": [
104.0254,
15.2683,
31.174,
107.0254,
23.6683,
39.574
]
} | {
"name": "3D-printable cycloidal drive FEA (jagathsrujan/3d-printable-cycloidal-drive)",
"url": "https://github.com/jagathsrujan/3d-printable-cycloidal-drive",
"license": "No repository license; FCStd metadata 'All rights reserved'. Local research only.",
"redistributable": false
} | active | cycloidal-drive-components | {
"independently_reproduced": true,
"workflow_scoring": "trusted_review_required",
"tolerances": "convergence_study"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-CYC-ShaftP1-PETGCF | A | source_backed_pilot | cycloidal-drive-components | Cycloidal drive: input shaft P1 (PETG-CF) | [
"linear static"
] | Component analysis: the input shaft P1 of an open-source, 3D-printable 15:1 cycloidal gearbox. part.step holds the single solid in millimetres (31 faces, volume 2449 mm^3). faces.json lists every face with its index, type, area, centroid and normal/axis; use the geometry, not a CAD system's own face numbering.
Materia... | [
{
"path": "tasks/A-CYC-ShaftP1-PETGCF/part.step",
"role": "cad",
"bytes": 87943,
"sha256": "c4e0a145e34cda5d9d6017c26b7dcddf52a9cd21e6349e34d7872c1d1191aea5"
},
{
"path": "tasks/A-CYC-ShaftP1-PETGCF/faces.json",
"role": "spec",
"bytes": 10679,
"sha256": "9df2092791c549d7c6298cbb9... | [
{
"key": "max_displacement_mm",
"unit": "mm",
"definition": "maximum nodal displacement magnitude in the part"
}
] | {
"solids": 1,
"faces": 31,
"assembly": false,
"cad_bbox_mm": [
-13.2391,
0.8587,
14.7139,
6.7609,
20.8587,
26.7139
]
} | {
"name": "3D-printable cycloidal drive FEA (jagathsrujan/3d-printable-cycloidal-drive)",
"url": "https://github.com/jagathsrujan/3d-printable-cycloidal-drive",
"license": "No repository license; FCStd metadata 'All rights reserved'. Local research only.",
"redistributable": false
} | active | cycloidal-drive-components | {
"independently_reproduced": true,
"workflow_scoring": "trusted_review_required",
"tolerances": "convergence_study"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-FCVM-Bar_buckling | A | source_backed_pilot | fcvm-buckling | fcVM Bar buckling: elastic buckling factor | [
"linear buckling",
"eigenvalue"
] | Linear (eigenvalue) buckling analysis of a steel structure from the fcVM workbench examples (Bar buckling). analysis.step holds the analysis geometry in millimetres (1 solid region(s) that share their interfaces and act as one continuous body, volume 100000 mm^3). faces.json describes every face (index, type, area, cen... | [
{
"path": "tasks/A-FCVM-Bar_buckling/analysis.step",
"role": "cad",
"bytes": 15441,
"sha256": "4ede25e9bc0e598a24c304aa17eafd9ab282d036800963e9e188384ed4db143f"
},
{
"path": "tasks/A-FCVM-Bar_buckling/faces.json",
"role": "spec",
"bytes": 2092,
"sha256": "4ac56fa4d248b2d2cd5a8f99... | [
{
"key": "lambda1",
"unit": "-",
"definition": "first (smallest positive) elastic buckling load factor of the reference load set"
}
] | {
"solids": 1,
"assembly": false
} | {
"name": "fcVM workbench examples (Harry van Langen, HarryvL/fcVM-workbench)",
"url": "https://github.com/HarryvL/fcVM-workbench",
"license": "LGPL-2.1-or-later (repository); example data licence not stated separately. Local research use.",
"redistributable": false
} | active | fcvm-buckling | {
"independently_reproduced": true,
"workflow_scoring": "trusted_review_required",
"tolerances": "convergence_study"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-FCVM-Buckling | A | source_backed_pilot | fcvm-buckling | fcVM Buckling: elastic buckling factor | [
"linear buckling",
"eigenvalue"
] | Linear (eigenvalue) buckling analysis of a steel structure from the fcVM workbench examples (Buckling). analysis.step holds the analysis geometry in millimetres (4 solid region(s) that share their interfaces and act as one continuous body, volume 103000 mm^3). faces.json describes every face (index, type, area, centroi... | [
{
"path": "tasks/A-FCVM-Buckling/analysis.step",
"role": "cad",
"bytes": 67479,
"sha256": "77b587dd963034a52d6c16c6fda424d7a208067498254429a880c9e4d7446082"
},
{
"path": "tasks/A-FCVM-Buckling/faces.json",
"role": "spec",
"bytes": 7298,
"sha256": "acd38669b29315ef4c13fe772636b6f0... | [
{
"key": "lambda1",
"unit": "-",
"definition": "first (smallest positive) elastic buckling load factor of the reference load set"
}
] | {
"solids": 4,
"assembly": true
} | {
"name": "fcVM workbench examples (Harry van Langen, HarryvL/fcVM-workbench)",
"url": "https://github.com/HarryvL/fcVM-workbench",
"license": "LGPL-2.1-or-later (repository); example data licence not stated separately. Local research use.",
"redistributable": false
} | active | fcvm-buckling | {
"independently_reproduced": true,
"workflow_scoring": "trusted_review_required",
"tolerances": "convergence_study"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-FCVM-PL-Wyk_Rohrstoss_ring | A | source_backed_pilot | fcvm-plastic-limit | fcVM Wyk_Rohrstoss_ring: plastic collapse load factor | [
"elastoplastic",
"limit analysis",
"von Mises perfect plasticity"
] | Plastic collapse (limit load) analysis of a steel part from the fcVM workbench examples (Wyk_Rohrstoss_ring). analysis.step holds the analysis geometry in millimetres (12 solid region(s) that share their interfaces and act as one continuous body, volume 2577880 mm^3). faces.json describes every face (index, type, area,... | [
{
"path": "tasks/A-FCVM-PL-Wyk_Rohrstoss_ring/analysis.step",
"role": "cad",
"bytes": 408545,
"sha256": "1544c9abe138b1d179647194e6108250f25ff9abddc022f37ee125f57e9c39cb"
},
{
"path": "tasks/A-FCVM-PL-Wyk_Rohrstoss_ring/faces.json",
"role": "spec",
"bytes": 33996,
"sha256": "5f52... | [
{
"key": "limit_load_factor",
"unit": "-",
"definition": "plastic collapse (limit) load factor of the reference load set"
}
] | {
"solids": 12,
"assembly": true
} | {
"name": "fcVM workbench examples (Harry van Langen, HarryvL/fcVM-workbench)",
"url": "https://github.com/HarryvL/fcVM-workbench",
"license": "LGPL-2.1-or-later (repository); example data licence not stated separately. Local research use.",
"redistributable": false
} | active | fcvm-plastic-limit | {
"independently_reproduced": true,
"workflow_scoring": "trusted_review_required",
"tolerances": "convergence_study"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-FCVM-Plate_girder_EC3 | A | source_backed_pilot | fcvm-buckling | fcVM Plate_girder_EC3: elastic buckling factor | [
"linear buckling",
"eigenvalue"
] | Linear (eigenvalue) buckling analysis of a steel structure from the fcVM workbench examples (Plate_girder_EC3). analysis.step holds the analysis geometry in millimetres (104 solid region(s) that share their interfaces and act as one continuous body, volume 3335612900 mm^3). faces.json describes every face (index, type,... | [
{
"path": "tasks/A-FCVM-Plate_girder_EC3/analysis.step",
"role": "cad",
"bytes": 3271883,
"sha256": "a59fc5f41e8004ec73ff05c83dc77038fbeaff31338cc595e5a56ed263be53e6"
},
{
"path": "tasks/A-FCVM-Plate_girder_EC3/faces.json",
"role": "spec",
"bytes": 217983,
"sha256": "b8320f0f1ba8... | [
{
"key": "lambda1",
"unit": "-",
"definition": "first (smallest positive) elastic buckling load factor of the reference load set"
}
] | {
"solids": 104,
"assembly": true
} | {
"name": "fcVM workbench examples (Harry van Langen, HarryvL/fcVM-workbench)",
"url": "https://github.com/HarryvL/fcVM-workbench",
"license": "LGPL-2.1-or-later (repository); example data licence not stated separately. Local research use.",
"redistributable": false
} | active | fcvm-buckling | {
"independently_reproduced": true,
"workflow_scoring": "trusted_review_required",
"tolerances": "convergence_study"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-FCVM-buckling_U100_3D | A | source_backed_pilot | fcvm-buckling | fcVM buckling_U100_3D: elastic buckling factor | [
"linear buckling",
"eigenvalue"
] | Linear (eigenvalue) buckling analysis of a steel structure from the fcVM workbench examples (buckling_U100_3D). analysis.step holds the analysis geometry in millimetres (1 solid region(s) that share their interfaces and act as one continuous body, volume 1207500 mm^3). faces.json describes every face (index, type, area... | [
{
"path": "tasks/A-FCVM-buckling_U100_3D/analysis.step",
"role": "cad",
"bytes": 32603,
"sha256": "8bc12b6e1e6201b211d59848bf5162e1297e21182594d1a8fe65439400d81f06"
},
{
"path": "tasks/A-FCVM-buckling_U100_3D/faces.json",
"role": "spec",
"bytes": 3846,
"sha256": "1fc00ce3639b15cc... | [
{
"key": "lambda1",
"unit": "-",
"definition": "first (smallest positive) elastic buckling load factor of the reference load set"
}
] | {
"solids": 1,
"assembly": false
} | {
"name": "fcVM workbench examples (Harry van Langen, HarryvL/fcVM-workbench)",
"url": "https://github.com/HarryvL/fcVM-workbench",
"license": "LGPL-2.1-or-later (repository); example data licence not stated separately. Local research use.",
"redistributable": false
} | active | fcvm-buckling | {
"independently_reproduced": true,
"workflow_scoring": "trusted_review_required",
"tolerances": "convergence_study"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-GEOPINO-PLATE-1 | A | source_backed_pilot | geopinonet-holed-plate | Holed plate, GeoPINONet validation case 1 | [
"linear static"
] | Holed steel plate. part.step is one solid in millimetres: a rectangular plate 176.914 mm (x) by 148.475 mm (y) by 10.000 mm (z) with a through hole along z.
Material: ANSYS default Structural Steel, linear isotropic elastic, E = 200 GPa, Poisson ratio 0.3. Linear static, small displacements, no gravity.
Supports: the e... | [
{
"path": "tasks/A-GEOPINO-PLATE-1/part.step",
"role": "cad",
"bytes": 11966,
"sha256": "b8c21f3313c9598e022e39dea167b23f0c3f8ce000cd1de27c6c303ef5b2f024"
}
] | [
{
"key": "max_displacement_compression_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, load case 1"
},
{
"key": "max_displacement_lateral_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, load case 2"
}
] | {
"solids": 1,
"faces": 7,
"assembly": false,
"cad_bbox_mm": [
-88.457056586,
-74.2373112915,
0,
88.457056586,
74.2373112915,
10
],
"geometry_class": "simple"
} | {
"name": "GeoPINONet holed-plate FEM dataset (Urrutia Valdes, La Fe-Perdomo, Rodriguez Soto)",
"url": "https://zenodo.org/records/21483341",
"license": "CC BY 4.0",
"redistributable": true
} | active | geopinonet-holed-plate | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-GEOPINO-PLATE-10 | A | source_backed_pilot | geopinonet-holed-plate | Holed plate, GeoPINONet validation case 10 | [
"linear static"
] | Holed steel plate. part.step is one solid in millimetres: a rectangular plate 103.299 mm (x) by 233.799 mm (y) by 10.000 mm (z) with a through hole along z.
Material: ANSYS default Structural Steel, linear isotropic elastic, E = 200 GPa, Poisson ratio 0.3. Linear static, small displacements, no gravity.
Supports: the e... | [
{
"path": "tasks/A-GEOPINO-PLATE-10/part.step",
"role": "cad",
"bytes": 11958,
"sha256": "39dbff6de5fe723805f05fc2e521ecadc9c73cfada11299c55a5f92e65807562"
}
] | [
{
"key": "max_displacement_compression_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, load case 1"
},
{
"key": "max_displacement_lateral_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, load case 2"
}
] | {
"solids": 1,
"faces": 7,
"assembly": false,
"cad_bbox_mm": [
-51.6492930027,
-116.899500128,
0,
51.6492930027,
116.899500128,
10
],
"geometry_class": "simple"
} | {
"name": "GeoPINONet holed-plate FEM dataset (Urrutia Valdes, La Fe-Perdomo, Rodriguez Soto)",
"url": "https://zenodo.org/records/21483341",
"license": "CC BY 4.0",
"redistributable": true
} | active | geopinonet-holed-plate | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-GEOPINO-PLATE-11 | A | source_backed_pilot | geopinonet-holed-plate | Holed plate, GeoPINONet validation case 11 | [
"linear static"
] | Holed steel plate. part.step is one solid in millimetres: a rectangular plate 178.586 mm (x) by 149.957 mm (y) by 10.000 mm (z) with a through hole along z.
Material: ANSYS default Structural Steel, linear isotropic elastic, E = 200 GPa, Poisson ratio 0.3. Linear static, small displacements, no gravity.
Supports: the e... | [
{
"path": "tasks/A-GEOPINO-PLATE-11/part.step",
"role": "cad",
"bytes": 12025,
"sha256": "904fcfed0ad33b6869d1b7e8f345d376b5421bdfc764453027a134d6e80e2022"
}
] | [
{
"key": "max_displacement_compression_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, load case 1"
},
{
"key": "max_displacement_lateral_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, load case 2"
}
] | {
"solids": 1,
"faces": 7,
"assembly": false,
"cad_bbox_mm": [
-89.2931248292,
-74.9784025526,
0,
89.2931248292,
74.9784025526,
10
],
"geometry_class": "simple"
} | {
"name": "GeoPINONet holed-plate FEM dataset (Urrutia Valdes, La Fe-Perdomo, Rodriguez Soto)",
"url": "https://zenodo.org/records/21483341",
"license": "CC BY 4.0",
"redistributable": true
} | active | geopinonet-holed-plate | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-GEOPINO-PLATE-12 | A | source_backed_pilot | geopinonet-holed-plate | Holed plate, GeoPINONet validation case 12 | [
"linear static"
] | Holed steel plate. part.step is one solid in millimetres: a rectangular plate 106.732 mm (x) by 237.799 mm (y) by 10.000 mm (z) with a through hole along z.
Material: ANSYS default Structural Steel, linear isotropic elastic, E = 200 GPa, Poisson ratio 0.3. Linear static, small displacements, no gravity.
Supports: the e... | [
{
"path": "tasks/A-GEOPINO-PLATE-12/part.step",
"role": "cad",
"bytes": 11999,
"sha256": "724f09bdf490475388e19a7bf69fe12519a6c5a29789a2b3d8d0514fbf1e3b80"
}
] | [
{
"key": "max_displacement_compression_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, load case 1"
},
{
"key": "max_displacement_lateral_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, load case 2"
}
] | {
"solids": 1,
"faces": 7,
"assembly": false,
"cad_bbox_mm": [
-53.3662437065,
-118.8994661769,
0,
53.3662437065,
118.8994661769,
10
],
"geometry_class": "simple"
} | {
"name": "GeoPINONet holed-plate FEM dataset (Urrutia Valdes, La Fe-Perdomo, Rodriguez Soto)",
"url": "https://zenodo.org/records/21483341",
"license": "CC BY 4.0",
"redistributable": true
} | active | geopinonet-holed-plate | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-GEOPINO-PLATE-13 | A | source_backed_pilot | geopinonet-holed-plate | Holed plate, GeoPINONet validation case 13 | [
"linear static"
] | Holed steel plate. part.step is one solid in millimetres: a rectangular plate 159.971 mm (x) by 190.179 mm (y) by 10.000 mm (z) with a through hole along z.
Material: ANSYS default Structural Steel, linear isotropic elastic, E = 200 GPa, Poisson ratio 0.3. Linear static, small displacements, no gravity.
Supports: the e... | [
{
"path": "tasks/A-GEOPINO-PLATE-13/part.step",
"role": "cad",
"bytes": 11954,
"sha256": "8da9fc44a544c4eea2789403a3c221d27487f270d52351747108282164fd3db4"
}
] | [
{
"key": "max_displacement_compression_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, load case 1"
},
{
"key": "max_displacement_lateral_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, load case 2"
}
] | {
"solids": 1,
"faces": 7,
"assembly": false,
"cad_bbox_mm": [
-79.9854010875,
-95.0894397155,
0,
79.9854010875,
95.0894397155,
10
],
"geometry_class": "simple"
} | {
"name": "GeoPINONet holed-plate FEM dataset (Urrutia Valdes, La Fe-Perdomo, Rodriguez Soto)",
"url": "https://zenodo.org/records/21483341",
"license": "CC BY 4.0",
"redistributable": true
} | active | geopinonet-holed-plate | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-GEOPINO-PLATE-14 | A | source_backed_pilot | geopinonet-holed-plate | Holed plate, GeoPINONet validation case 14 | [
"linear static"
] | Holed steel plate. part.step is one solid in millimetres: a rectangular plate 100.050 mm (x) by 176.030 mm (y) by 10.000 mm (z) with a through hole along z.
Material: ANSYS default Structural Steel, linear isotropic elastic, E = 200 GPa, Poisson ratio 0.3. Linear static, small displacements, no gravity.
Supports: the e... | [
{
"path": "tasks/A-GEOPINO-PLATE-14/part.step",
"role": "cad",
"bytes": 11918,
"sha256": "f1e06d0aea36ae4b2ca1459de71dffc34a2b7276b388ce7e72a38a98755218f7"
}
] | [
{
"key": "max_displacement_compression_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, load case 1"
},
{
"key": "max_displacement_lateral_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, load case 2"
}
] | {
"solids": 1,
"faces": 7,
"assembly": false,
"cad_bbox_mm": [
-50.0247670108,
-88.0150345351,
0,
50.0247670108,
88.0150345351,
10
],
"geometry_class": "simple"
} | {
"name": "GeoPINONet holed-plate FEM dataset (Urrutia Valdes, La Fe-Perdomo, Rodriguez Soto)",
"url": "https://zenodo.org/records/21483341",
"license": "CC BY 4.0",
"redistributable": true
} | active | geopinonet-holed-plate | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-GEOPINO-PLATE-5 | A | source_backed_pilot | geopinonet-holed-plate | Holed plate, GeoPINONet validation case 5 | [
"linear static"
] | Holed steel plate. part.step is one solid in millimetres: a rectangular plate 178.029 mm (x) by 167.627 mm (y) by 10.000 mm (z) with a through hole along z.
Material: ANSYS default Structural Steel, linear isotropic elastic, E = 200 GPa, Poisson ratio 0.3. Linear static, small displacements, no gravity.
Supports: the e... | [
{
"path": "tasks/A-GEOPINO-PLATE-5/part.step",
"role": "cad",
"bytes": 12021,
"sha256": "9ea6e3b00b8142262f1343839c60e0746fa8f4e3f019bf277ac1c3da55bd1d22"
}
] | [
{
"key": "max_displacement_compression_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, load case 1"
},
{
"key": "max_displacement_lateral_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, load case 2"
}
] | {
"solids": 1,
"faces": 7,
"assembly": false,
"cad_bbox_mm": [
-89.0145980614,
-83.8134080268,
0,
89.0145980614,
83.8134080268,
10
],
"geometry_class": "simple"
} | {
"name": "GeoPINONet holed-plate FEM dataset (Urrutia Valdes, La Fe-Perdomo, Rodriguez Soto)",
"url": "https://zenodo.org/records/21483341",
"license": "CC BY 4.0",
"redistributable": true
} | active | geopinonet-holed-plate | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-GEOPINO-PLATE-7 | A | source_backed_pilot | geopinonet-holed-plate | Holed plate, GeoPINONet validation case 7 | [
"linear static"
] | Holed steel plate. part.step is one solid in millimetres: a rectangular plate 102.621 mm (x) by 237.880 mm (y) by 10.000 mm (z) with a through hole along z.
Material: ANSYS default Structural Steel, linear isotropic elastic, E = 200 GPa, Poisson ratio 0.3. Linear static, small displacements, no gravity.
Supports: the e... | [
{
"path": "tasks/A-GEOPINO-PLATE-7/part.step",
"role": "cad",
"bytes": 11966,
"sha256": "8b1716d885b4753b73d618be1c4d9e6a4051ab2b15403eb30dc1f03aa9d02a18"
}
] | [
{
"key": "max_displacement_compression_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, load case 1"
},
{
"key": "max_displacement_lateral_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, load case 2"
}
] | {
"solids": 1,
"faces": 7,
"assembly": false,
"cad_bbox_mm": [
-51.3104925297,
-118.9400399846,
0,
51.3104925297,
118.9400399846,
10
],
"geometry_class": "simple"
} | {
"name": "GeoPINONet holed-plate FEM dataset (Urrutia Valdes, La Fe-Perdomo, Rodriguez Soto)",
"url": "https://zenodo.org/records/21483341",
"license": "CC BY 4.0",
"redistributable": true
} | active | geopinonet-holed-plate | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-MORPHWING-Test1 | A | source_backed_pilot | morphing-wing-plates | Morphing-wing cantilever plate, Test 1 | [
"modal"
] | Cantilever plate specimen for an active-camber morphing-wing study (FDM-printed PLA): a uniform 4 mm plate. part.step is one solid in millimetres, 109 x 50 x 4 mm, with a 19 mm clamping grip at x = 0-19 mm (the scalloped clamp region).
Model the vibrating structure only: the free part x >= 19 mm, clamped (all displacem... | [
{
"path": "tasks/A-MORPHWING-Test1/part.step",
"role": "cad",
"bytes": 41253,
"sha256": "bb4f17c5068167e576c23d22a532f3294b3d0e54f502bd86803636ee33eb54c1"
}
] | [
{
"key": "f_1B_Hz",
"unit": "Hz",
"definition": "first out-of-plane bending mode"
},
{
"key": "f_1T_Hz",
"unit": "Hz",
"definition": "first torsion mode about the span (x) axis"
},
{
"key": "f_2B_Hz",
"unit": "Hz",
"definition": "second out-of-plane bending mode"
}
] | {
"solids": 1,
"faces": 16,
"assembly": false,
"cad_bbox_mm": [
0,
0,
0,
109,
50,
4
]
} | {
"name": "Experimental and numerical data of candidate structural models for active camber morphing wings (Huang & Zhang)",
"url": "https://data.mendeley.com/datasets/8jxw5533py/1",
"license": "CC BY 4.0",
"redistributable": true
} | active | morphing-wing-plates | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-MORPHWING-Test2 | A | source_backed_pilot | morphing-wing-plates | Morphing-wing cantilever plate, Test 2 | [
"modal"
] | Cantilever plate specimen for an active-camber morphing-wing study (FDM-printed PLA): a uniform 4 mm plate. part.step is one solid in millimetres, 144 x 50 x 4 mm, with a 19 mm clamping grip at x = 0-19 mm (the scalloped clamp region).
Model the vibrating structure only: the free part x >= 19 mm, clamped (all displacem... | [
{
"path": "tasks/A-MORPHWING-Test2/part.step",
"role": "cad",
"bytes": 41262,
"sha256": "e9c816732a3a8b511dc2a68c473516a2d2deaf7fc5f1a89d0693855cd669c6f2"
}
] | [
{
"key": "f_1B_Hz",
"unit": "Hz",
"definition": "first out-of-plane bending mode"
},
{
"key": "f_1T_Hz",
"unit": "Hz",
"definition": "first torsion mode about the span (x) axis"
},
{
"key": "f_2B_Hz",
"unit": "Hz",
"definition": "second out-of-plane bending mode"
}
] | {
"solids": 1,
"faces": 16,
"assembly": false,
"cad_bbox_mm": [
0,
0,
0,
144,
50,
4
]
} | {
"name": "Experimental and numerical data of candidate structural models for active camber morphing wings (Huang & Zhang)",
"url": "https://data.mendeley.com/datasets/8jxw5533py/1",
"license": "CC BY 4.0",
"redistributable": true
} | active | morphing-wing-plates | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-MORPHWING-Test3 | A | source_backed_pilot | morphing-wing-plates | Morphing-wing cantilever plate, Test 3 | [
"modal"
] | Cantilever plate specimen for an active-camber morphing-wing study (FDM-printed PLA): a uniform 4 mm plate. part.step is one solid in millimetres, 269 x 50 x 4 mm, with a 19 mm clamping grip at x = 0-19 mm (the scalloped clamp region).
Model the vibrating structure only: the free part x >= 19 mm, clamped (all displacem... | [
{
"path": "tasks/A-MORPHWING-Test3/part.step",
"role": "cad",
"bytes": 41284,
"sha256": "9130625285e7db444e10070ae9aaf61c1c379132a08332e8c94fadd56f6f5188"
}
] | [
{
"key": "f_1B_Hz",
"unit": "Hz",
"definition": "first out-of-plane bending mode"
},
{
"key": "f_1T_Hz",
"unit": "Hz",
"definition": "first torsion mode about the span (x) axis"
},
{
"key": "f_2B_Hz",
"unit": "Hz",
"definition": "second out-of-plane bending mode"
}
] | {
"solids": 1,
"faces": 16,
"assembly": false,
"cad_bbox_mm": [
0,
0,
0,
269,
50,
4
]
} | {
"name": "Experimental and numerical data of candidate structural models for active camber morphing wings (Huang & Zhang)",
"url": "https://data.mendeley.com/datasets/8jxw5533py/1",
"license": "CC BY 4.0",
"redistributable": true
} | active | morphing-wing-plates | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-MORPHWING-Test5 | A | source_backed_pilot | morphing-wing-plates | Morphing-wing cantilever plate, Test 5 | [
"modal"
] | Cantilever plate specimen for an active-camber morphing-wing study (FDM-printed PLA): a 4 mm plate with a 1 mm-thick flexible strip (mid-plane z = 2 mm) along part of its width, the stepped plate used for active camber morphing. part.step is one solid in millimetres, 269 x 50 x 4 mm, with a 19 mm clamping grip at x = 0... | [
{
"path": "tasks/A-MORPHWING-Test5/part.step",
"role": "cad",
"bytes": 55021,
"sha256": "0173c75adb03d48b5390f06c2324c3514328d42ffa369e310980a535cd5dd783"
}
] | [
{
"key": "f_1B_Hz",
"unit": "Hz",
"definition": "first out-of-plane bending mode"
},
{
"key": "f_1T_Hz",
"unit": "Hz",
"definition": "first torsion mode about the span (x) axis"
},
{
"key": "f_2B_Hz",
"unit": "Hz",
"definition": "second out-of-plane bending mode"
}
] | {
"solids": 1,
"faces": 22,
"assembly": false,
"cad_bbox_mm": [
0,
0,
0,
269,
50,
4
]
} | {
"name": "Experimental and numerical data of candidate structural models for active camber morphing wings (Huang & Zhang)",
"url": "https://data.mendeley.com/datasets/8jxw5533py/1",
"license": "CC BY 4.0",
"redistributable": true
} | active | morphing-wing-plates | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-MORPHWING-Test6 | A | source_backed_pilot | morphing-wing-plates | Morphing-wing cantilever plate, Test 6 | [
"modal"
] | Cantilever plate specimen for an active-camber morphing-wing study (FDM-printed PLA): a 4 mm plate with a 1 mm-thick flexible strip (mid-plane z = 2 mm) along part of its width, the stepped plate used for active camber morphing. part.step is one solid in millimetres, 269 x 50 x 4 mm, with a 19 mm clamping grip at x = 0... | [
{
"path": "tasks/A-MORPHWING-Test6/part.step",
"role": "cad",
"bytes": 55009,
"sha256": "c94e208191d30352f9e3030424eed547cbb19a9f213383a871c9ff6e99b56f33"
}
] | [
{
"key": "f_1B_Hz",
"unit": "Hz",
"definition": "first out-of-plane bending mode"
},
{
"key": "f_1T_Hz",
"unit": "Hz",
"definition": "first torsion mode about the span (x) axis"
},
{
"key": "f_2B_Hz",
"unit": "Hz",
"definition": "second out-of-plane bending mode"
}
] | {
"solids": 1,
"faces": 22,
"assembly": false,
"cad_bbox_mm": [
0,
0,
0,
269,
50,
4
]
} | {
"name": "Experimental and numerical data of candidate structural models for active camber morphing wings (Huang & Zhang)",
"url": "https://data.mendeley.com/datasets/8jxw5533py/1",
"license": "CC BY 4.0",
"redistributable": true
} | active | morphing-wing-plates | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-MORPHWING-Test7 | A | source_backed_pilot | morphing-wing-plates | Morphing-wing cantilever plate, Test 7 | [
"modal"
] | Cantilever plate specimen for an active-camber morphing-wing study (FDM-printed PLA): a 4 mm plate with a 1 mm-thick flexible strip (mid-plane z = 2 mm) along part of its width, the stepped plate used for active camber morphing. part.step is one solid in millimetres, 319 x 50 x 4 mm, with a 19 mm clamping grip at x = 0... | [
{
"path": "tasks/A-MORPHWING-Test7/part.step",
"role": "cad",
"bytes": 54999,
"sha256": "7e770269694f2e104dd36d4c8fbdcf924e7348c78a1f4d692d2256045aeebc23"
}
] | [
{
"key": "f_1B_Hz",
"unit": "Hz",
"definition": "first out-of-plane bending mode"
},
{
"key": "f_1T_Hz",
"unit": "Hz",
"definition": "first torsion mode about the span (x) axis"
},
{
"key": "f_2B_Hz",
"unit": "Hz",
"definition": "second out-of-plane bending mode"
}
] | {
"solids": 1,
"faces": 22,
"assembly": false,
"cad_bbox_mm": [
0,
0,
0,
319,
50,
4
]
} | {
"name": "Experimental and numerical data of candidate structural models for active camber morphing wings (Huang & Zhang)",
"url": "https://data.mendeley.com/datasets/8jxw5533py/1",
"license": "CC BY 4.0",
"redistributable": true
} | active | morphing-wing-plates | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-MORPHWING-Test8 | A | source_backed_pilot | morphing-wing-plates | Morphing-wing cantilever plate, Test 8 | [
"modal"
] | Cantilever plate specimen for an active-camber morphing-wing study (FDM-printed PLA): a 4 mm plate with a 1 mm-thick flexible strip (mid-plane z = 2 mm) along part of its width, the stepped plate used for active camber morphing. part.step is one solid in millimetres, 219 x 50 x 4 mm, with a 19 mm clamping grip at x = 0... | [
{
"path": "tasks/A-MORPHWING-Test8/part.step",
"role": "cad",
"bytes": 55023,
"sha256": "ade469df6ffc42a5123cfbf0088202cfcc4b2b779aa9028e9ef9719407b6a30d"
}
] | [
{
"key": "f_1B_Hz",
"unit": "Hz",
"definition": "first out-of-plane bending mode"
},
{
"key": "f_1T_Hz",
"unit": "Hz",
"definition": "first torsion mode about the span (x) axis"
},
{
"key": "f_2B_Hz",
"unit": "Hz",
"definition": "second out-of-plane bending mode"
}
] | {
"solids": 1,
"faces": 22,
"assembly": false,
"cad_bbox_mm": [
0,
0,
0,
219,
50,
4
]
} | {
"name": "Experimental and numerical data of candidate structural models for active camber morphing wings (Huang & Zhang)",
"url": "https://data.mendeley.com/datasets/8jxw5533py/1",
"license": "CC BY 4.0",
"redistributable": true
} | active | morphing-wing-plates | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-MORPHWING-Test9 | A | source_backed_pilot | morphing-wing-plates | Morphing-wing cantilever plate, Test 9 | [
"modal"
] | Cantilever plate specimen for an active-camber morphing-wing study (FDM-printed PLA): a 4 mm plate with a 1 mm-thick flexible strip (mid-plane z = 2 mm) along part of its width, the stepped plate used for active camber morphing. part.step is one solid in millimetres, 169 x 50 x 4 mm, with a 19 mm clamping grip at x = 0... | [
{
"path": "tasks/A-MORPHWING-Test9/part.step",
"role": "cad",
"bytes": 55014,
"sha256": "d252462d0032832b90e9f238f52b5ddebfe16f39dadafa184733e8e4fd03f7d1"
}
] | [
{
"key": "f_1B_Hz",
"unit": "Hz",
"definition": "first out-of-plane bending mode"
},
{
"key": "f_1T_Hz",
"unit": "Hz",
"definition": "first torsion mode about the span (x) axis"
},
{
"key": "f_2B_Hz",
"unit": "Hz",
"definition": "second out-of-plane bending mode"
}
] | {
"solids": 1,
"faces": 22,
"assembly": false,
"cad_bbox_mm": [
0,
0,
0,
169,
50,
4
]
} | {
"name": "Experimental and numerical data of candidate structural models for active camber morphing wings (Huang & Zhang)",
"url": "https://data.mendeley.com/datasets/8jxw5533py/1",
"license": "CC BY 4.0",
"redistributable": true
} | active | morphing-wing-plates | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-RIGGING-test1 | A | figure_reference | rigging-plate | Rigging plate, load test 1 | [
"linear static"
] | Hard-anodised 7075-T6 rigging plate, load test 1 of the source's seven ANSYS load cases (Test 1 (2697.7 lbf)). riggingplate.step is the single solid in millimetres (235.58 x 111.90 x 12 mm, 145 faces).
Material: aluminium 7075-T6, linear isotropic elastic (standard handbook values; the source did not publish its card, ... | [
{
"path": "tasks/A-RIGGING-test1/riggingplate.step",
"role": "cad",
"bytes": 334473,
"sha256": "802292a27c3fd074be575a0246fa42bb081b7319581aa7eac7a71f0901d64405"
},
{
"path": "tasks/A-RIGGING-test1/boundary-conditions.png",
"role": "figure",
"bytes": 871431,
"sha256": "0d70646d43... | [
{
"key": "max_von_mises_MPa",
"unit": "MPa",
"definition": "maximum equivalent (von Mises) stress in the plate"
}
] | {
"solids": 1,
"faces": 145,
"assembly": false
} | {
"name": "OpenRiggingPlate (mpangch)",
"url": "https://github.com/mpangch/OpenRiggingPlate",
"license": "CERN-OHL-S-2.0",
"redistributable": true
} | active | rigging-plate | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-RIGGING-test2 | A | figure_reference | rigging-plate | Rigging plate, load test 2 | [
"linear static"
] | Hard-anodised 7075-T6 rigging plate, load test 2 of the source's seven ANSYS load cases (Test 2 (2384.5 lbf)). riggingplate.step is the single solid in millimetres (235.58 x 111.90 x 12 mm, 145 faces).
Material: aluminium 7075-T6, linear isotropic elastic (standard handbook values; the source did not publish its card, ... | [
{
"path": "tasks/A-RIGGING-test2/riggingplate.step",
"role": "cad",
"bytes": 334473,
"sha256": "802292a27c3fd074be575a0246fa42bb081b7319581aa7eac7a71f0901d64405"
},
{
"path": "tasks/A-RIGGING-test2/boundary-conditions.png",
"role": "figure",
"bytes": 884028,
"sha256": "abdbb19010... | [
{
"key": "max_von_mises_MPa",
"unit": "MPa",
"definition": "maximum equivalent (von Mises) stress in the plate"
}
] | {
"solids": 1,
"faces": 145,
"assembly": false
} | {
"name": "OpenRiggingPlate (mpangch)",
"url": "https://github.com/mpangch/OpenRiggingPlate",
"license": "CERN-OHL-S-2.0",
"redistributable": true
} | active | rigging-plate | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-RIGGING-test3 | A | figure_reference | rigging-plate | Rigging plate, load test 3 | [
"linear static"
] | Hard-anodised 7075-T6 rigging plate, load test 3 of the source's seven ANSYS load cases (Test 3 (4768.8 lbf)). riggingplate.step is the single solid in millimetres (235.58 x 111.90 x 12 mm, 145 faces).
Material: aluminium 7075-T6, linear isotropic elastic (standard handbook values; the source did not publish its card, ... | [
{
"path": "tasks/A-RIGGING-test3/riggingplate.step",
"role": "cad",
"bytes": 334473,
"sha256": "802292a27c3fd074be575a0246fa42bb081b7319581aa7eac7a71f0901d64405"
},
{
"path": "tasks/A-RIGGING-test3/boundary-conditions.png",
"role": "figure",
"bytes": 791793,
"sha256": "c45c5592d8... | [
{
"key": "max_von_mises_MPa",
"unit": "MPa",
"definition": "maximum equivalent (von Mises) stress in the plate"
}
] | {
"solids": 1,
"faces": 145,
"assembly": false
} | {
"name": "OpenRiggingPlate (mpangch)",
"url": "https://github.com/mpangch/OpenRiggingPlate",
"license": "CERN-OHL-S-2.0",
"redistributable": true
} | active | rigging-plate | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-RIGGING-test6 | A | figure_reference | rigging-plate | Rigging plate, load test 6 | [
"linear static"
] | Hard-anodised 7075-T6 rigging plate, load test 6 of the source's seven ANSYS load cases (Test 6 (3372.1 lbf)). riggingplate.step is the single solid in millimetres (235.58 x 111.90 x 12 mm, 145 faces).
Material: aluminium 7075-T6, linear isotropic elastic (standard handbook values; the source did not publish its card, ... | [
{
"path": "tasks/A-RIGGING-test6/riggingplate.step",
"role": "cad",
"bytes": 334473,
"sha256": "802292a27c3fd074be575a0246fa42bb081b7319581aa7eac7a71f0901d64405"
},
{
"path": "tasks/A-RIGGING-test6/boundary-conditions.png",
"role": "figure",
"bytes": 949008,
"sha256": "de809e9fc5... | [
{
"key": "max_von_mises_MPa",
"unit": "MPa",
"definition": "maximum equivalent (von Mises) stress in the plate"
}
] | {
"solids": 1,
"faces": 145,
"assembly": false
} | {
"name": "OpenRiggingPlate (mpangch)",
"url": "https://github.com/mpangch/OpenRiggingPlate",
"license": "CERN-OHL-S-2.0",
"redistributable": true
} | active | rigging-plate | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-SIMJEB-analysis-0 | A | source_backed_pilot | simjeb-analysis | GE bracket design 0: four-case static analysis | [
"linear static",
"multi-load-case"
] | Design task: the GE jet engine bracket. Units: millimetres, newtons, MPa. Material: Ti-6Al-4V (E = 113.8 GPa, nu = 0.342, density 4.43 g/cm^3, yield strength 903 MPa). The bracket is bolted to a flat mounting surface, the plane z = 0, with nothing below it, and carries a clevis for a pin.
Interfaces: (a) four vertical ... | [
{
"path": "tasks/A-SIMJEB-analysis-0/bracket.step",
"role": "cad",
"bytes": 1950338,
"sha256": "697b87ca5cd7db4603481e0e03fef1bc779ed166d996d9ba1072ae3818cd6f27"
}
] | [
{
"key": "vertical_max_displacement_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, vertical case"
},
{
"key": "horizontal_max_displacement_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, horizontal case"
},
{
"key": "diagonal_max_displacement_... | {
"solids": 1,
"assembly": false,
"mass_kg": 1.3609
} | {
"name": "SimJEB: simulated jet engine bracket dataset (Whalen, Beyene, Mueller, CGF 2021) / GE bracket challenge",
"url": "https://doi.org/10.7910/DVN/XFUWJG",
"license": "Dataverse CC0 / README ODC-By; GE bracket CAD from GrabCAD (non-commercial). Local research use.",
"redistributable": false
} | active | simjeb-bracket | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-SIMJEB-analysis-10 | A | source_backed_pilot | simjeb-analysis | GE bracket design 10: four-case static analysis | [
"linear static",
"multi-load-case"
] | Design task: the GE jet engine bracket. Units: millimetres, newtons, MPa. Material: Ti-6Al-4V (E = 113.8 GPa, nu = 0.342, density 4.43 g/cm^3, yield strength 903 MPa). The bracket is bolted to a flat mounting surface, the plane z = 0, with nothing below it, and carries a clevis for a pin.
Interfaces: (a) four vertical ... | [
{
"path": "tasks/A-SIMJEB-analysis-10/bracket.step",
"role": "cad",
"bytes": 1566934,
"sha256": "65b6e0e776543f18a9d42860019fe91f6d3616fce11692eb20c3b42d4ce256ce"
}
] | [
{
"key": "vertical_max_displacement_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, vertical case"
},
{
"key": "horizontal_max_displacement_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, horizontal case"
},
{
"key": "diagonal_max_displacement_... | {
"solids": 1,
"assembly": false,
"mass_kg": 0.3972
} | {
"name": "SimJEB: simulated jet engine bracket dataset (Whalen, Beyene, Mueller, CGF 2021) / GE bracket challenge",
"url": "https://doi.org/10.7910/DVN/XFUWJG",
"license": "Dataverse CC0 / README ODC-By; GE bracket CAD from GrabCAD (non-commercial). Local research use.",
"redistributable": false
} | active | simjeb-bracket | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-SIMJEB-analysis-101 | A | source_backed_pilot | simjeb-analysis | GE bracket design 101: four-case static analysis | [
"linear static",
"multi-load-case"
] | Design task: the GE jet engine bracket. Units: millimetres, newtons, MPa. Material: Ti-6Al-4V (E = 113.8 GPa, nu = 0.342, density 4.43 g/cm^3, yield strength 903 MPa). The bracket is bolted to a flat mounting surface, the plane z = 0, with nothing below it, and carries a clevis for a pin.
Interfaces: (a) four vertical ... | [
{
"path": "tasks/A-SIMJEB-analysis-101/bracket.step",
"role": "cad",
"bytes": 1072017,
"sha256": "932392d73590e41fdd532eb451fd4d9b3089197339dfad45c780bc247097db73"
}
] | [
{
"key": "vertical_max_displacement_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, vertical case"
},
{
"key": "horizontal_max_displacement_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, horizontal case"
},
{
"key": "diagonal_max_displacement_... | {
"solids": 1,
"assembly": false,
"mass_kg": 0.644
} | {
"name": "SimJEB: simulated jet engine bracket dataset (Whalen, Beyene, Mueller, CGF 2021) / GE bracket challenge",
"url": "https://doi.org/10.7910/DVN/XFUWJG",
"license": "Dataverse CC0 / README ODC-By; GE bracket CAD from GrabCAD (non-commercial). Local research use.",
"redistributable": false
} | active | simjeb-bracket | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-SIMJEB-analysis-107 | A | source_backed_pilot | simjeb-analysis | GE bracket design 107: four-case static analysis | [
"linear static",
"multi-load-case"
] | Design task: the GE jet engine bracket. Units: millimetres, newtons, MPa. Material: Ti-6Al-4V (E = 113.8 GPa, nu = 0.342, density 4.43 g/cm^3, yield strength 903 MPa). The bracket is bolted to a flat mounting surface, the plane z = 0, with nothing below it, and carries a clevis for a pin.
Interfaces: (a) four vertical ... | [
{
"path": "tasks/A-SIMJEB-analysis-107/bracket.step",
"role": "cad",
"bytes": 662121,
"sha256": "6744bbb4935f5cfa143ecf3bb6bdee634c2978be06e752bff1d9b4da885ad973"
}
] | [
{
"key": "vertical_max_displacement_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, vertical case"
},
{
"key": "horizontal_max_displacement_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, horizontal case"
},
{
"key": "diagonal_max_displacement_... | {
"solids": 1,
"assembly": false,
"mass_kg": 1.264
} | {
"name": "SimJEB: simulated jet engine bracket dataset (Whalen, Beyene, Mueller, CGF 2021) / GE bracket challenge",
"url": "https://doi.org/10.7910/DVN/XFUWJG",
"license": "Dataverse CC0 / README ODC-By; GE bracket CAD from GrabCAD (non-commercial). Local research use.",
"redistributable": false
} | active | simjeb-bracket | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-SIMJEB-analysis-108 | A | source_backed_pilot | simjeb-analysis | GE bracket design 108: four-case static analysis | [
"linear static",
"multi-load-case"
] | Design task: the GE jet engine bracket. Units: millimetres, newtons, MPa. Material: Ti-6Al-4V (E = 113.8 GPa, nu = 0.342, density 4.43 g/cm^3, yield strength 903 MPa). The bracket is bolted to a flat mounting surface, the plane z = 0, with nothing below it, and carries a clevis for a pin.
Interfaces: (a) four vertical ... | [
{
"path": "tasks/A-SIMJEB-analysis-108/bracket.step",
"role": "cad",
"bytes": 4739924,
"sha256": "c4df79188c245fd558b869096db5be44c6597d42ad0845eb44f4da6956f32b28"
}
] | [
{
"key": "vertical_max_displacement_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, vertical case"
},
{
"key": "horizontal_max_displacement_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, horizontal case"
},
{
"key": "diagonal_max_displacement_... | {
"solids": 1,
"assembly": false,
"mass_kg": 0.4686
} | {
"name": "SimJEB: simulated jet engine bracket dataset (Whalen, Beyene, Mueller, CGF 2021) / GE bracket challenge",
"url": "https://doi.org/10.7910/DVN/XFUWJG",
"license": "Dataverse CC0 / README ODC-By; GE bracket CAD from GrabCAD (non-commercial). Local research use.",
"redistributable": false
} | active | simjeb-bracket | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-SIMJEB-analysis-131 | A | source_backed_pilot | simjeb-analysis | GE bracket design 131: four-case static analysis | [
"linear static",
"multi-load-case"
] | Design task: the GE jet engine bracket. Units: millimetres, newtons, MPa. Material: Ti-6Al-4V (E = 113.8 GPa, nu = 0.342, density 4.43 g/cm^3, yield strength 903 MPa). The bracket is bolted to a flat mounting surface, the plane z = 0, with nothing below it, and carries a clevis for a pin.
Interfaces: (a) four vertical ... | [
{
"path": "tasks/A-SIMJEB-analysis-131/bracket.step",
"role": "cad",
"bytes": 4369194,
"sha256": "4d30cf8a15c27b19b3afbc5179ce481abfc9a6366d6d1302b9437d25d8ed73f9"
}
] | [
{
"key": "vertical_max_displacement_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, vertical case"
},
{
"key": "horizontal_max_displacement_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, horizontal case"
},
{
"key": "diagonal_max_displacement_... | {
"solids": 1,
"assembly": false,
"mass_kg": 0.7921
} | {
"name": "SimJEB: simulated jet engine bracket dataset (Whalen, Beyene, Mueller, CGF 2021) / GE bracket challenge",
"url": "https://doi.org/10.7910/DVN/XFUWJG",
"license": "Dataverse CC0 / README ODC-By; GE bracket CAD from GrabCAD (non-commercial). Local research use.",
"redistributable": false
} | active | simjeb-bracket | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-SIMJEB-analysis-58 | A | source_backed_pilot | simjeb-analysis | GE bracket design 58: four-case static analysis | [
"linear static",
"multi-load-case"
] | Design task: the GE jet engine bracket. Units: millimetres, newtons, MPa. Material: Ti-6Al-4V (E = 113.8 GPa, nu = 0.342, density 4.43 g/cm^3, yield strength 903 MPa). The bracket is bolted to a flat mounting surface, the plane z = 0, with nothing below it, and carries a clevis for a pin.
Interfaces: (a) four vertical ... | [
{
"path": "tasks/A-SIMJEB-analysis-58/bracket.step",
"role": "cad",
"bytes": 1769663,
"sha256": "8950a56848935b91251c6117a1ed114c51ca00019312a6018e48c19e02e370fc"
}
] | [
{
"key": "vertical_max_displacement_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, vertical case"
},
{
"key": "horizontal_max_displacement_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, horizontal case"
},
{
"key": "diagonal_max_displacement_... | {
"solids": 1,
"assembly": false,
"mass_kg": 1.3576000000000001
} | {
"name": "SimJEB: simulated jet engine bracket dataset (Whalen, Beyene, Mueller, CGF 2021) / GE bracket challenge",
"url": "https://doi.org/10.7910/DVN/XFUWJG",
"license": "Dataverse CC0 / README ODC-By; GE bracket CAD from GrabCAD (non-commercial). Local research use.",
"redistributable": false
} | active | simjeb-bracket | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-SIMJEB-analysis-62 | A | source_backed_pilot | simjeb-analysis | GE bracket design 62: four-case static analysis | [
"linear static",
"multi-load-case"
] | Design task: the GE jet engine bracket. Units: millimetres, newtons, MPa. Material: Ti-6Al-4V (E = 113.8 GPa, nu = 0.342, density 4.43 g/cm^3, yield strength 903 MPa). The bracket is bolted to a flat mounting surface, the plane z = 0, with nothing below it, and carries a clevis for a pin.
Interfaces: (a) four vertical ... | [
{
"path": "tasks/A-SIMJEB-analysis-62/bracket.step",
"role": "cad",
"bytes": 3354928,
"sha256": "647dbf0bc70213fcee3ae3f29e6cde06e3a147a34125359a4cea3e6cad331f67"
}
] | [
{
"key": "vertical_max_displacement_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, vertical case"
},
{
"key": "horizontal_max_displacement_mm",
"unit": "mm",
"definition": "maximum displacement magnitude, horizontal case"
},
{
"key": "diagonal_max_displacement_... | {
"solids": 1,
"assembly": false,
"mass_kg": 0.47090000000000004
} | {
"name": "SimJEB: simulated jet engine bracket dataset (Whalen, Beyene, Mueller, CGF 2021) / GE bracket challenge",
"url": "https://doi.org/10.7910/DVN/XFUWJG",
"license": "Dataverse CC0 / README ODC-By; GE bracket CAD from GrabCAD (non-commercial). Local research use.",
"redistributable": false
} | active | simjeb-bracket | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
A-VALVE-transient | A | source_backed_pilot | feenox-valve-transient | Power-plant valve: nonlinear transient thermal (carbon + stainless) | [
"transient thermal",
"nonlinear material",
"multi-material"
] | Nonlinear transient heat conduction in a power-plant valve: a carbon-steel nozzle welded to stainless-steel valve bodies (half model, symmetry plane y = 0). valve.brep holds 4 solids in millimetres (112 faces). Solid 2 (the nozzle, x from 0 to 65 mm) is carbon steel; solids 1, 3 and 4 are stainless steel SA-312. faces.... | [
{
"path": "tasks/A-VALVE-transient/valve.brep",
"role": "cad",
"bytes": 1069100,
"sha256": "8d037ae89831453d87479a502361c59c499568565a8d51ecd77fc4f568a0010b"
},
{
"path": "tasks/A-VALVE-transient/asme-properties.fee",
"role": "spec",
"bytes": 6705,
"sha256": "9a58fc3baf6216e5f5a1... | [
{
"key": "scl2_dT_max_K",
"unit": "K",
"definition": "maximum over time of T(inner end) - T(outer end) on SCL2 (heat-up)"
},
{
"key": "scl2_dT_min_K",
"unit": "K",
"definition": "minimum over time of T(inner end) - T(outer end) on SCL2 (cool-down, negative)"
},
{
"key": "scl4_dT_... | {
"solids": 4,
"faces": 112,
"assembly": true,
"cad_bbox_mm": [
-784.21,
0,
-134.938,
65.003,
157.1,
185.737
]
} | {
"name": "FeenoX tutorial #3: heat conduction (valve with carbon and stainless steel parts)",
"url": "https://www.seamplex.com/feenox/doc/tutorials/320-thermal/",
"license": "GPL-3.0",
"redistributable": true
} | active | feenox-valve-transient | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
B-FEMCAD-062 | B | source_backed_pilot | femcad-hard | Plate with a hole in tension | [
"Solid Mechanics"
] | CAD + FEM task. Build the part with a CAD script and write it as part.step in millimetres in exactly the coordinate frame given (multi-region models: one STEP with one solid per region and shared, coincident interface faces; 2-D models: planar faces in the z = 0 plane); then analyse YOUR model with any open-source FEM ... | [
{
"path": "tasks/B-FEMCAD-062/figure-1.png",
"role": "figure",
"bytes": 48866,
"sha256": "e1e3ec03b30b36460927b2b6bc4d1cb63fc022df88bdc15c7449e19658368dab"
}
] | [
{
"key": "max_von_mises_MPa",
"unit": "MPa",
"definition": "maximum von Mises stress"
}
] | {
"model_kind": "3-D solid",
"assembly": false
} | {
"name": "Wolfram FEM documentation: Solid Mechanics Verification Tests",
"url": "https://reference.wolfram.com/language/PDEModels/tutorial/StructuralMechanics/SolidMechanicsVerificationTests.html",
"license": "Wolfram documentation (copyright Wolfram Research); figures not redistributable",
"redistributable":... | active | femcad-hard | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
B-FEMCAD-067 | B | source_backed_pilot | femcad-hard | Thick-walled tube heated on an inner band | [
"Heat Transfer"
] | CAD + FEM task. Build the part with a CAD script and write it as part.step in millimetres in exactly the coordinate frame given (multi-region models: one STEP with one solid per region and shared, coincident interface faces; 2-D models: planar faces in the z = 0 plane); then analyse YOUR model with any open-source FEM ... | [
{
"path": "tasks/B-FEMCAD-067/figure-1.gif",
"role": "figure",
"bytes": 50011,
"sha256": "b13c5a324d87fb9a3e1a086988ec1646adf48a5de29b4195e280a1fc4f8172ad"
}
] | [
{
"key": "T_probe_K",
"unit": "K",
"definition": "temperature at (r, z) = (40, 40)"
}
] | {
"model_kind": "3-D solid",
"assembly": false
} | {
"name": "Wolfram FEM documentation: Heat Transfer Verification Tests",
"url": "https://reference.wolfram.com/language/PDEModels/tutorial/HeatTransfer/HeatTransferVerificationTests.html",
"license": "Wolfram documentation (copyright Wolfram Research); figures not redistributable",
"redistributable": false
} | active | femcad-hard | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
B-RIGGING-test1 | B | figure_reference | rigging-plate | Rigging plate, load test 1 (from drawing) | [
"linear static"
] | Hard-anodised 7075-T6 rigging plate, load test 1 of the source's seven ANSYS load cases (Test 1 (2697.7 lbf)). Build the plate yourself from rigging-plate-drawing.pdf (the source's dimensioned manufacturing drawing, millimetres, 12 mm thick, all seams blended) and export it as part.step; then analyse your own model.
Ma... | [
{
"path": "tasks/B-RIGGING-test1/rigging-plate-drawing.pdf",
"role": "drawing",
"bytes": 7599823,
"sha256": "21bf0df8535cc7e2c4efa393c460ec64e74ea9a11fb2032f78dc1e13c541a759"
},
{
"path": "tasks/B-RIGGING-test1/boundary-conditions.png",
"role": "figure",
"bytes": 871431,
"sha256"... | [
{
"key": "max_von_mises_MPa",
"unit": "MPa",
"definition": "maximum equivalent (von Mises) stress in the plate"
}
] | {
"solids": 1,
"faces": 145,
"assembly": false
} | {
"name": "OpenRiggingPlate (mpangch)",
"url": "https://github.com/mpangch/OpenRiggingPlate",
"license": "CERN-OHL-S-2.0",
"redistributable": true
} | active | rigging-plate | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
B-CA-SSLX102 | B | source_backed_pilot | codeaster-piping | 90-degree pipe elbow under in-plane and out-of-plane end moments | [
"Solid Mechanics"
] | CAD + FEM task. Build the part with a CAD script and write it as part.step in millimetres in exactly the coordinate frame given (assemblies: one STEP with one solid per body); then analyse YOUR model with any open-source FEM library, set up exactly as under Analysis. main.py must run both steps (artifact contract below... | [
{
"path": "tasks/B-CA-SSLX102/figure-1.png",
"role": "figure",
"bytes": 6053,
"sha256": "723bcd997666328392ab7be9553f3bb21cdc84bd45dfc8d6979a6b7c4c1f46b8"
}
] | [
{
"key": "dy_D_inplane_mm",
"unit": "mm",
"definition": "load case 1: area-mean y displacement of the D end face"
},
{
"key": "dz_D_outofplane_mm",
"unit": "mm",
"definition": "load case 2: area-mean z displacement of the D end face"
}
] | {
"model_kind": "3-D thin-walled solid",
"assembly": false
} | {
"name": "Code_Aster validation test SSLX102",
"url": "https://codeaster.gitlab.io/doc/docaster/manuals/man_v/v3/v3.05.102/index.html",
"source_commit": "4ce70ac7b16b8d88243badd5b83f76f86254e47c",
"license": "Code_Aster validation documentation and test files, EDF R&D, distributed with code_aster under GNU GPL... | active | codeaster-piping | {
"independently_reproduced": true,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
B-CA-SSLV311 | B | source_backed_pilot | codeaster-fracture-3d | Quarter-elliptical corner crack at the bore of a rotating thick disc | [
"Solid Mechanics",
"Fracture"
] | CAD + FEM task. Build the part with a CAD script and write it as part.step in millimetres in exactly the coordinate frame given (assemblies: one STEP with one solid per body); then analyse YOUR model with any open-source FEM library, set up exactly as under Analysis. main.py must run both steps (artifact contract below... | [
{
"path": "tasks/B-CA-SSLV311/figure-1.png",
"role": "figure",
"bytes": 7613,
"sha256": "ddae18ba82b1c1543a5a205b1ebac09f946c494de94b061016697fb484043f7d"
}
] | [
{
"key": "K_I_s05_MPa_sqrt_m",
"unit": "MPa*m^0.5",
"definition": "K_I at front arc length 5.349 mm from the bore end"
},
{
"key": "K_I_s34_MPa_sqrt_m",
"unit": "MPa*m^0.5",
"definition": "K_I at front arc length 34.448 mm from the bore end"
}
] | {
"model_kind": "3-D solid with crack",
"assembly": false
} | {
"name": "Code_Aster validation test SSLV311",
"url": "https://codeaster.gitlab.io/doc/docaster/manuals/man_v/v3/v3.04.311/index.html",
"source_commit": "4ce70ac7b16b8d88243badd5b83f76f86254e47c",
"license": "Code_Aster validation documentation and test files, EDF R&D, distributed with code_aster under GNU GPL... | active | codeaster-fracture-3d | {
"independently_reproduced": true,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
B-CA-SSLV154 | B | source_backed_pilot | codeaster-fracture-3d | Penny-shaped crack in a cube under inclined uniaxial tension (mixed mode) | [
"Solid Mechanics",
"Fracture"
] | CAD + FEM task. Build the part with a CAD script and write it as part.step in millimetres in exactly the coordinate frame given (assemblies: one STEP with one solid per body); then analyse YOUR model with any open-source FEM library, set up exactly as under Analysis. main.py must run both steps (artifact contract below... | [
{
"path": "tasks/B-CA-SSLV154/figure-1.png",
"role": "figure",
"bytes": 15347,
"sha256": "19d6caaeb1ee09cefa49c3125c7c6eeb94433068952ab135fc96c8ee36429c6e"
},
{
"path": "tasks/B-CA-SSLV154/figure-2.png",
"role": "figure",
"bytes": 4905,
"sha256": "c609daefec8b5654c597aba781338c08... | [
{
"key": "K_I_MPa_sqrt_m",
"unit": "MPa*m^0.5",
"definition": "K_I at front point (2000, 0, 0)"
},
{
"key": "K_II_abs_MPa_sqrt_m",
"unit": "MPa*m^0.5",
"definition": "|K_II| at front point (2000, 0, 0)"
},
{
"key": "K_III_abs_MPa_sqrt_m",
"unit": "MPa*m^0.5",
"definition"... | {
"model_kind": "3-D solid with crack",
"assembly": false
} | {
"name": "Code_Aster validation test SSLV154",
"url": "https://codeaster.gitlab.io/doc/docaster/manuals/man_v/v3/v3.04.154/index.html",
"source_commit": "4ce70ac7b16b8d88243badd5b83f76f86254e47c",
"license": "Code_Aster validation documentation and test files, EDF R&D, distributed with code_aster under GNU GPL... | active | codeaster-fracture-3d | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
B-CA-SSLV155 | B | source_backed_pilot | codeaster-fracture-3d | Lens-shaped (spherical-cap) crack in a cube under hydrostatic tension | [
"Solid Mechanics",
"Fracture"
] | CAD + FEM task. Build the part with a CAD script and write it as part.step in millimetres in exactly the coordinate frame given (assemblies: one STEP with one solid per body); then analyse YOUR model with any open-source FEM library, set up exactly as under Analysis. main.py must run both steps (artifact contract below... | [
{
"path": "tasks/B-CA-SSLV155/figure-1.png",
"role": "figure",
"bytes": 254548,
"sha256": "2c02df0646ba3f1285f16d125622bf73c0f240941a6eb064fc57e304555c57ae"
}
] | [
{
"key": "K_I_MPa_sqrt_m",
"unit": "MPa*m^0.5",
"definition": "K_I on the crack front"
}
] | {
"model_kind": "3-D solid with curved crack",
"assembly": false
} | {
"name": "Code_Aster validation test SSLV155",
"url": "https://codeaster.gitlab.io/doc/docaster/manuals/man_v/v3/v3.04.155/index.html",
"source_commit": "4ce70ac7b16b8d88243badd5b83f76f86254e47c",
"license": "Code_Aster validation documentation and test files, EDF R&D, distributed with code_aster under GNU GPL... | active | codeaster-fracture-3d | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
B-CA-SSLV139 | B | source_backed_pilot | codeaster-stability | Buckling of a clamped thin circular plate under uniform edge compression | [
"Solid Mechanics",
"Buckling"
] | CAD + FEM task. Build the part with a CAD script and write it as part.step in millimetres in exactly the coordinate frame given (assemblies: one STEP with one solid per body); then analyse YOUR model with any open-source FEM library, set up exactly as under Analysis. main.py must run both steps (artifact contract below... | [
{
"path": "tasks/B-CA-SSLV139/figure-1.png",
"role": "figure",
"bytes": 25536,
"sha256": "f26601fc79d5557ea1c44a6acfecafda4d9bfc755645c98b9ced952712a4aa71"
}
] | [
{
"key": "F_cr_N_per_mm",
"unit": "N/mm",
"definition": "critical uniform radial edge load per unit rim length"
}
] | {
"model_kind": "3-D thin solid",
"assembly": false
} | {
"name": "Code_Aster validation test SSLV139",
"url": "https://codeaster.gitlab.io/doc/docaster/manuals/man_v/v3/v3.04.139/index.html",
"source_commit": "4ce70ac7b16b8d88243badd5b83f76f86254e47c",
"license": "Code_Aster validation documentation and test files, EDF R&D, distributed with code_aster under GNU GPL... | active | codeaster-stability | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
B-CA-SSNL126 | B | source_backed_pilot | codeaster-stability | Elastic and elastoplastic buckling of a clamped-free bar | [
"Solid Mechanics",
"Plasticity",
"Buckling"
] | CAD + FEM task. Build the part with a CAD script and write it as part.step in millimetres in exactly the coordinate frame given (assemblies: one STEP with one solid per body); then analyse YOUR model with any open-source FEM library, set up exactly as under Analysis. main.py must run both steps (artifact contract below... | [
{
"path": "tasks/B-CA-SSNL126/figure-1.png",
"role": "figure",
"bytes": 2401,
"sha256": "9afb489e83567089bf24178126a7b070e5b54f59356bb219094fb2e7ba100583"
}
] | [
{
"key": "p_cr_elastic_MPa",
"unit": "MPa",
"definition": "critical pressure from the state at p = 2.6 MPa"
},
{
"key": "p_cr_plastic_MPa",
"unit": "MPa",
"definition": "critical pressure from the state at p = 5.2 MPa"
}
] | {
"model_kind": "3-D solid",
"assembly": false
} | {
"name": "Code_Aster validation test SSNL126",
"url": "https://codeaster.gitlab.io/doc/docaster/manuals/man_v/v6/v6.02.126/index.html",
"source_commit": "4ce70ac7b16b8d88243badd5b83f76f86254e47c",
"license": "Code_Aster validation documentation and test files, EDF R&D, distributed with code_aster under GNU GPL... | active | codeaster-stability | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
B-CA-SSLS120 | B | source_backed_pilot | codeaster-piping | Open cylindrical water tank under hydrostatic pressure | [
"Solid Mechanics"
] | CAD + FEM task. Build the part with a CAD script and write it as part.step in millimetres in exactly the coordinate frame given (assemblies: one STEP with one solid per body); then analyse YOUR model with any open-source FEM library, set up exactly as under Analysis. main.py must run both steps (artifact contract below... | [
{
"path": "tasks/B-CA-SSLS120/figure-1.png",
"role": "figure",
"bytes": 11041,
"sha256": "140f4f4c10851d34468d86f15c1bfbeaa3f43fffd200e6a695817ccc588f9c42"
}
] | [
{
"key": "u_r_base_mm",
"unit": "mm",
"definition": "radial displacement of the mid-surface at z = 0"
},
{
"key": "u_z_top_mm",
"unit": "mm",
"definition": "axial displacement of the mid-surface at z = 16000"
},
{
"key": "sigma_hoop_base_MPa",
"unit": "MPa",
"definition":... | {
"model_kind": "3-D thin-walled solid",
"assembly": false
} | {
"name": "Code_Aster validation test SSLS120",
"url": "https://codeaster.gitlab.io/doc/docaster/manuals/man_v/v3/v3.03.120/index.html",
"source_commit": "4ce70ac7b16b8d88243badd5b83f76f86254e47c",
"license": "Code_Aster validation documentation and test files, EDF R&D, distributed with code_aster under GNU GPL... | active | codeaster-piping | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
B-CA-SSNP154 | B | source_backed_pilot | codeaster-contact | NAFEMS cylinder-roller Hertz contact (plane strain, frictionless) | [
"Solid Mechanics",
"Contact"
] | CAD + FEM task. Build the part with a CAD script and write it as part.step in millimetres in exactly the coordinate frame given (assemblies: one STEP with one solid per body); then analyse YOUR model with any open-source FEM library, set up exactly as under Analysis. main.py must run both steps (artifact contract below... | [
{
"path": "tasks/B-CA-SSNP154/figure-1.png",
"role": "figure",
"bytes": 15906,
"sha256": "5a8ccab35c71a3c89381f50d71c0cfa801e1e3a88f35f603f69881eae9650de2"
}
] | [
{
"key": "dy_B_mm",
"unit": "mm",
"definition": "y displacement of block point B (100, 200)"
}
] | {
"model_kind": "plane-strain two-body contact",
"assembly": true
} | {
"name": "Code_Aster validation test SSNP154",
"url": "https://codeaster.gitlab.io/doc/docaster/manuals/man_v/v6/v6.03.154/index.html",
"source_commit": "4ce70ac7b16b8d88243badd5b83f76f86254e47c",
"license": "Code_Aster validation documentation and test files, EDF R&D, distributed with code_aster under GNU GPL... | active | codeaster-contact | {
"independently_reproduced": true,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
B-CA-SSLV110 | B | source_backed_pilot | codeaster-fracture-3d | Embedded elliptical crack in a long block under remote tension | [
"Solid Mechanics",
"Fracture"
] | CAD + FEM task. Build the part with a CAD script and write it as part.step in millimetres in exactly the coordinate frame given (assemblies: one STEP with one solid per body); then analyse YOUR model with any open-source FEM library, set up exactly as under Analysis. main.py must run both steps (artifact contract below... | [] | [
{
"key": "K_I_minor_axis_MPa_sqrt_mm",
"unit": "MPa*mm^0.5",
"definition": "K_I at front point (0, 6, 0)"
}
] | {
"model_kind": "3-D solid with crack",
"assembly": false
} | {
"name": "Code_Aster validation test SSLV110",
"url": "https://codeaster.gitlab.io/doc/docaster/manuals/man_v/v3/v3.04.110/index.html",
"source_commit": "4ce70ac7b16b8d88243badd5b83f76f86254e47c",
"license": "Code_Aster validation documentation and test files, EDF R&D, distributed with code_aster under GNU GPL... | active | codeaster-fracture-3d | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
B-CA-HPLV102 | B | source_backed_pilot | codeaster-fracture-3d | Penny-shaped crack with cooled faces in a large sphere (thermoelastic G) | [
"Heat Transfer",
"Solid Mechanics",
"Fracture"
] | CAD + FEM task. Build the part with a CAD script and write it as part.step in millimetres in exactly the coordinate frame given (assemblies: one STEP with one solid per body); then analyse YOUR model with any open-source FEM library, set up exactly as under Analysis. main.py must run both steps (artifact contract below... | [
{
"path": "tasks/B-CA-HPLV102/figure-1.png",
"role": "figure",
"bytes": 1332,
"sha256": "a81ac2731027fa852cf57e2a4986dc503c66c33fa552a52533c840051f1ef406"
}
] | [
{
"key": "G_N_per_mm",
"unit": "N/mm",
"definition": "energy release rate on the crack front"
}
] | {
"model_kind": "3-D solid with crack, thermal + mechanical",
"assembly": false
} | {
"name": "Code_Aster validation test HPLV102",
"url": "https://codeaster.gitlab.io/doc/docaster/manuals/man_v/v7/v7.03.102/index.html",
"source_commit": "4ce70ac7b16b8d88243badd5b83f76f86254e47c",
"license": "Code_Aster validation documentation and test files, EDF R&D, distributed with code_aster under GNU GPL... | active | codeaster-fracture-3d | {
"independently_reproduced": false,
"workflow_scoring": "trusted_review_required",
"tolerances": "provisional_source_protocol"
} | [
"results.json",
"main.py",
"part.step",
"mesh.msh",
"fields.npz",
"solver.log",
"refinement.json",
"environment.json"
] |
CADFEM-Bench v1.9
Summary
CADFEM-Bench tests whether a model can carry out a complete engineering analysis from CAD: read or build the geometry, mesh it, run a finite-element solve and report the requested quantities, with the mesh, fields and a convergence record. Each submission is one Python script, replayed offline in a sandbox and scored on reference values, geometry checks and workflow artefacts.
v1.9 has 217 active tasks: 64 primary tasks with publisher reference values (135 graded outputs), 71 further source-backed tasks, and 82 generated linear-buckling tasks whose true first factor is below 1 (evaluator-computed references).
GPT-6 Astra (one code-generation call per task, no tools) failed 51 of the 79 CAD+FEM tasks it was scored on. 43 are buckling tasks: in 30 it reported, without checking, a higher mode that CalculiX 2.23 returned in place of the first one, and in 13 its script stopped with no answer. The other 8 (fracture, static, thermal, plasticity) gave no answer: 7 through errors in its own code, 1 by refusing after its own check failed. Evidence for every case: https://huggingface.co/datasets/Conditiondark/astra-cadfem-failures.
Use it as a research benchmark, not yet a leaderboard. References and evaluator files are public, so models trained
after October 2026 may have seen the answers. Only 17 of the 64 primary references are independently reproduced and
most tolerances are provisional; 6 of the 36 primary tasks run so far had defects on our side (see excluded.jsonl
and dataset-defects-found.json in the failures dataset). The hard cases are concentrated in buckling, and results so
far cover one model with one sample per task.
Evaluation scheme
- Generation (outside the sandbox). The model sees only one task's
candidate/files (or anevaluator/export_run.pyexport) and returnsmain.py. Record model and version, settings, tokens and cost. - Replay (
evaluator/sandbox_runner.py). One attempt, no retries, in a fresh job: network off, inputs read-only, evaluator files unreadable, 600 s wall time, 600 s CPU per process, 8 GiB RAM, 2 threads. Pinned Python runtime (CadQuery/OCP, Gmsh, NumPy/SciPy, meshio, scikit-fem), with CalculiX 2.23 as an optional read-only runtime. Every model compared must get the same runtime and the same inputs; drawing tasks need image input. - Scoring (
evaluator/score.py), reported separately:- Numerical:
results.jsonholds exactly the requested keys as finite numbers, each within its tolerance. For the 135 primary outputs the bands are relative 5 % (69), 10 % (54), 6 % (4), 20 % (5, stress read from figure legends), 1 % (1) and 5 % with offset (2); buckle traps use 5 %. A task passes numerically when every output does. - Artefacts: eight non-empty files (
results.json,main.py,part.step,mesh.msh,fields.npz,solver.log,refinement.json,environment.json);part.stepmust load as a solid. - Geometry (drawing and specification tasks): same solid count, volume within 2 %, point-to-surface Hausdorff distance at most max(0.5 mm, 0.1 % of the reference diagonal) in the specified frame; analytic radii within 0.01 mm where required. Boolean IoU is a diagnostic only.
- Workflow: a reviewer, blind to the model, signs off execution, geometry, setup, field outputs and convergence against the artefact hashes. A task passes end to end only with numerical pass and this sign-off.
- Numerical:
- Reporting: track A (supplied CAD) and track B (drawing or specification to CAD), engineering-family macro average, the independently reproduced subset, and buckle traps apart from the primary suite. Use several samples per task with confidence intervals, and label single-shot and agentic (tool or feedback) runs as separate conditions.
The Astra results add a failure analysis on top of this (scripts in the failures dataset): every miss is classed by mechanism (M1 silent wrong value, M2 no answer from its own code, M8 refusal), task defects and infrastructure stops are excluded, and a wrong buckling answer counts as confirmed only when the model's own CalculiX deck, rerun with loads x 0.1, recovers the reference. Those runs used a 6 GB memory limit.
Tasks
Supplied-CAD and drawing-to-CAD finite-element tasks for evaluating models that write complete CAD+FEM pipelines:
a model gets a task (prompt, STEP or drawing, face list, figures) and returns one runnable main.py that builds or
reads the geometry, meshes it, solves it and writes the requested outputs, fields, mesh and convergence record.
| suite | tasks |
|---|---|
| primary (published reference values) | 64 (135 graded outputs) |
| calibration | 7 |
| reserved-public | 63 |
| related-public | 1 |
| buckle traps (evaluator-computed references) | 82 admitted (18 held of 100) |
| active total | 217 (235 with held buckle traps) |
Topics: structural static, buckling, eigenfrequency, fracture (stress-intensity factors), plasticity (limit load), steady and transient heat conduction, contact. Sources include Code_Aster validation tests, fcVM, FeenoX, CADWorld, SimJEB, AgentFEM, NAFEMS-style benchmarks and open engineering repositories; every task names its source.
Layout (cadfem-bench-v1.9/)
candidate/: model-visible primary tasks and inputs (tasks.jsonl,tasks/<id>/) and the submission contract.evaluator/: references (references.jsonl), the other suites (suites/), scorer (score.py), sandbox runner (sandbox_runner.py), geometry and field metrics, original source evidence, verification records.held/: inactive tasks with reasons.report/: task atlas (evaluator-only).scripts/: build and check scripts.SHA256SUMS.txt: checksums of every file (shasum -a 256 -c SHA256SUMS.txtinside the folder).
Use
Give a model only candidate/ (or an export from evaluator/export_run.py); the evaluator folder, reports and source
library contain the answers, so this public copy is not an uncontaminated holdout. Replay submissions with
evaluator/sandbox_runner.py and score with evaluator/score.py; numerical accuracy, geometry gates and verified
workflow are scored separately. The package README, RELEASE_README.md and evaluator/DATASET_CARD.md give the full
protocol and limits: most primary acceptance bands are provisional and fourteen primary tasks have independent FEM
reproduction; buckle-trap references are evaluator-computed (FEniCSx P2 + SLEPc), not published.
GPT-6 Astra results on this benchmark, with code and verdict evidence for 51 tasks it failed: https://huggingface.co/datasets/Conditiondark/astra-cadfem-failures.
Licences
Source rights vary per task and are recorded in each task's source field (evaluator/references.jsonl). Some sources
are GPL-3.0 or CC BY 4.0; others are non-commercial (SimJEB's GE bracket CAD from GrabCAD), carry no licence or
'All rights reserved' (cycloidal drive files), or are documentation excerpts (Code_Aster, Wolfram). Respect each
source's terms; research use only where no licence is given. Material generated for this benchmark (buckle-trap tasks
and references, prompts, records, scripts) is CC BY 4.0.
- Downloads last month
- 76