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Complete User Guide148 pages · 10 chapters · Updated 2026-09-18
Getting Started Handbook139 pages · 8 chapters · Updated 2026-09-18
Training & Exercise Manual386 pages · 115 chapters · all 104 exercises · Updated 2026-09-18
Complete Theory Manual255 pages · 56 chapters · Updated 2026-09-18
Models & Workflow Manual85 pages · 9 chapters · Updated 2026-09-18

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05.6.5 / Structural

Connect process history to structural response

A laminate remembers how it was processed and the environment it experienced. Define those conditions before interpreting its loaded response.

Read time and travel distance
0501001502000204060Boundary temperature (°C)Time (min)

Cursor: 30 min · 300 mm · 120.0 °C

Teaching illustration only. Controls change this diagram, not your database or Workbench simulation. Distance = speed × time at constant speed; the boundary schedule is not a solved core-temperature or cure field.

What the study needs

ChoiceWhy it matters
Material and layupElastic properties and fiber directions determine stiffness; strengths and fracture data are needed for the selected failure models.
Geometry and supportShape, dimensions and boundary conditions determine how a component deforms and carries load.
Mechanical loadsSpecify the forces and moments, including which components increase during progressive failure.
Process and environmentTemperature, moisture and material state can produce expansion, shrinkage and residual stresses.

Define the surfaces and the material state

  • Give the upper and lower surfaces independent histories when their surroundings differ.
  • Choose prescribed temperature, convection or another supported thermal boundary condition.
  • Define moisture exposure and the corresponding diffusion properties when studying uptake or drying.
  • Provide calibrated cure or crystallization kinetics for reacting materials; use an inert material when no reaction is intended.
  • A recorded pressure history is not, by itself, proof that pressure has been mechanically coupled. Check the selected structural loads.

Named response and traceability outputs

Named result groupContents
Transport historiesTransport metadata, time, temperature, and moisture
Material-state historiesCure/crystallinity states, rates, heat sources, and shrinkage
Surface and ply summariesInterpolated surfaces and final per-ply process summary
Process-to-structure resultsStructural mapping, process-only field contributions, and process resultants
Double-Double recommendationCompatibility, recommended angles, stiffness error, and selected ply angles
Structural summaryCylinder summary plus plate/beam section, response, energy, buckling, and frequency results
Cylinder load historyCylinder loads and resultants
Cylinder stress recoveryFinal radial-coordinate and recovered-stress table

Interpret before comparing. Check the final material state and residual stresses, then compare the loaded response. Missing transport or strength data must not be treated as a validated pass. Try the coupled exercise →

Workbench availability: released models, inputs and compatible study paths. The wider theory library includes reference formulations not available in every Workbench solve.