CAD FEA · Virtual Labs · AquinTutor

← LABS CAD FEA PLANE-STRESS FINITE ELEMENTS · PHASE 4

Model

Part Material Thickness (mm) 10 Tip load (N, downward) 2000 Mesh density medium

Display

Deformation scale auto

von Mises

—

MPa

Set up the model, then Solve FEA.

Results

Nodes—

Elements—

DOF solved—

Solve time—

Max deflection—

Max von Mises—

Yield strength—

Safety factor —

Constant-strain-triangle plane-stress FEA. Left edge fully fixed; load applied at the free end. Stress is exact for the mesh; refine the mesh near concentrations (the hole) for a tighter peak — that convergence behaviour is real FEA, not an artefact.