Workbench exercise preview

02.08 · Laminate orientation and tensile response

Level 2
Developing
Est. 25 min
Exercise workflow · Open full-size map ↗

All blocks keep the CREATE / DISCOVER / SIMULATE positions, with Equipment below Geometry; unused records remain disconnected. This changes the view only, not the exercise records.

02.08 · Laminate orientation and tensile response · Fixed layout with all supplied blocks · not solved results
∑ Used models & submodels

Only models assigned to records used by this exercise are listed here. The full-layout option preserves the supplied starter records; no Workbench records are changed.

CLT · Linear static · ASTM D3039 · Tension load

Shared laminate stiffness drives this membrane/CLT path. Failure criteria are independent comparisons, not blended models. Fatigue is a separate assessment.

∑ Theory & assumptions
Data travelling between blocks

Materials → Laminates
Stored ply stiffness, strength, density and expansion properties.

Mechanical → Simulation
SIMULATION selects this case and its analysis model; the case owns its applicable cycle and input references.

Laminates → Mechanical
Ply angles and thicknesses, stiffness, mass and ply properties.

Geometry → Mechanical
Part shape and dimensions, thickness or section definition, and model-specific geometric inputs. Each selected case consumes only the dimensions its model supports.

Models → Mechanical
Applied model assignment: CLT · Linear static. Model parameters and formulation are used by Mechanical.

Open the copied laminate and record the initial stacking sequence and total thickness.

Models: Classical laminate theory · Linear static · ASTM D3039-17(2025)-based

Study scope and limitations

ASTM-based teaching geometry, not certification. Grips, tabs, alignment and physical test validity are not simulated.

Loading reference

Common Ply Property Definition