Structure

Compressor Blade Linear Static Response

Adjust total tip force on the fixed twisted compressor blade; predict SI displacement and stress with an ideal isotropic elastic material.

Published scope

The inputs, geometry and outputs below follow the registered public case. Published verification applies only to the stated conditions. Service availability requires a live request.

supervised structural field MLP

Geometry
Imported compressor blade SI-unit mesh
Geometry scope
fixed_geometry_material_and_boundaries
Fixed conditions
material: isotropic elastic; youngs_modulus_gpa: 210.0; poisson_ratio: 0.3; density_kg_per_m3: 7850.0; support: root plane z=0 m, all three translational displacements fixed; load_direction: negative Y; load_distribution: equal nodal forces on the registered tip-plane node group; geometry_and_mesh: fixed imported compressor blade C3D10; geometric_nonlinearity: False

Adjustable inputs

InputRangeDefault
Total downward force10.0 – 100.0 N60.0

Output fields

Registered verification

registered_status
passed
registered_reference
Frozen independent native Abaqus same-point holdout
registered_parameters
load_force_n: 60.0
holdout_metrics
Relative L2: 0.19082337419534928; Correlation: 0.9814776675200986
thresholds
per_field_relative_l2_maximum: 0.2; per_field_correlation_minimum: 0.95
summary
Registered output fields passed the declared independent pointwise thresholds at the registered force only.

Recorded workflow evidence

Project opening
PASS
Save and reopen
PASS
Training
NOT_RUN
Prediction
NOT_RUN
Independent accuracy
RETAINED_EXISTING_EVIDENCE_NOT_RECOMPUTED
Portable validation
PASS

These are recorded checks; they do not establish live service availability or accuracy for every new request.

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