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Use Adam to set up a structural study, inspect an existing one, or compare design revisions. Name the solver if you have a requirement; otherwise ask Adam to check an available formulation appropriate to the problem.

Choose the right physical model

A small-displacement linear study can answer some stiffness questions. Contact separation, snap fits, large deformation, impact, or material yielding may require different physics. A modal shape shows a vibration mode with arbitrary normalization; its plotted amplitude is not an operating displacement prediction. Provide geometry and units, sourced material properties, physical attachment, loads, and the quantity you need. Distinguish an applied force from a prescribed displacement: the latter can be used to calculate the reaction needed to impose that motion.

Start with a controlled example

Set up a simple stiffness calculation
This is a numerical learning example, not a qualification of a real bracket or joint.

Compare with the beam estimate

For the idealized end load above, the elementary bending estimate is deflection = F L³ / (3 E I), with I = width × thickness³ / 12. In consistent N and mm units, E = 70,000 N/mm² and I = 106.67 mm⁴. These are beam-theory reference values. A three-dimensional finite-element model can differ because of its formulation and end constraints. Ask Adam to explain the difference and mesh sensitivity. A factor-of-1,000 discrepancy is a reason to check units before changing the physics.

Inspect setup and results

1

Verify the physical inputs

Read back material assignments, units, load direction and total, support locations, and contact assumptions.
2

Run and preserve evidence

Keep the input deck or native study, mesh, solver version, logs, and achieved load or time step.
3

Check numerical behavior

Review termination, finite results, equilibrium where available, and refinement of the requested response.
4

Interpret the engineering result

Compare against the supplied requirement and explain the effect of assumptions, singularities, or missing checks.

Compare a design change

Compare two revisions at the same conditions
A stress peak at an idealized constraint may not be a meaningful failure criterion. A factor of safety needs the appropriate material limit and failure mode; displacement alone does not establish strength. For native studies, see Native CAE setup. For deliverables, see Results and comparison.
Last modified on October 14, 2026