forked from 1b-agent/fieldcraft-upstream
Christian Svensson
68aff646b2
LE2, the cylindrical shell bending patch test, in its two load cases (edge moment; pressure with the balancing edge traction) on an 8 × 8 MITC4 patch: tangential stress at E 59.936 and 59.904 against 60. LE3, the hemispherical shell with point loads, on a 32 × 32 longitude-latitude mesh (planar quad4 cells, tri3 at the pole): radial displacement at A 0.18418 against 0.185. Both meshes are written node by node from the generator each README lists, with the refinement that supports its tolerance. Targets are transcribed from the reproductions of TNSB Rev. 3 in the Abaqus 2016 Benchmarks Guide and the ESRD StressCheck NAFEMS guide. Part of #97.
16 lines
985 B
JSON
16 lines
985 B
JSON
{
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"title": "NAFEMS LE3 hemispherical shell with point loads (MITC4 shells)",
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"kind": "benchmark",
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"source": "NAFEMS, The Standard NAFEMS Benchmarks, TNSB Rev. 3, October 1990, test LE3 (target: radial displacement 0.185 m at A); the problem and target as reproduced in the Abaqus 2016 Benchmarks Guide, section 4.2.3 'LE3: Hemispherical shell with point loads', and in the ESRD StressCheck Benchmarks Guide 'The Standard NAFEMS Benchmarks: Linear Elastic Tests' (2018), p. 12",
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"quantities": [
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{
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"id": "ur_A",
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"quantity": "radial displacement at A (10, 0, 0), m",
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"measure": {"command": "solve.probe", "params": {"step": "Load", "at": [[10, 0, 0]]}, "pointer": "/nodes/0/displacement/0"},
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"value": 0.185,
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"tolerance": {"relative": 0.02},
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"reason": "the target is published to three figures; the displacement under a point load on a shear-deformable shell keeps growing slowly as the mesh is refined (32 × 32 is 0.44% low, 64 × 64 0.16%; see README)"
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}
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]
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}
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