SA-FEA finite element analysis (FEA) application online. Import, mesh, and solve locally with WebAssembly. No install.
The cantilever beam shown above is the first of many samples that are free to run.
| Mesher | Tetrahedra | Outside the limits | Smallest dihedral angle | Skin triangles outside | Time |
|---|---|---|---|---|---|
| SA-FEA | 13,346 | 0 | 18.0° | 124 (2.6%) | 0.9 s |
| Frontal-Delaunay, best of eight settings | 46,698 | 2,097 (4.5%) | 2.2° | 2,542 (11.8%) | 2.3 s |
| Advancing front, crease angle 60° (its default aborts) | 5,251 | 138 (2.6%) | 3.8° | 261 (6.9%) | 1.8 s |
| Constrained Delaunay refinement | 137,305 | 3,223 (2.3%) | 1.3° | 8,931 (22.2%) | 2.9 s |
| Envelope-based robust tetrahedralization | 3,236 | 931 (28.8%) | 8.7° | 1,719 (69.1%) | 15.3 s |
| Delaunay refinement, surface then volume | 21,533 | 2,360 (11.0%) | 7.0° | 4,191 (29.4%) | 4.3 s |
The Verification & Benchmarks page lists the cases the solver is checked against, each with its target and reading: NAFEMS and MacNeal-Harder benchmarks, NASA demonstration problems, closed forms for statics, modes, large deflection, plasticity, and contact, patch tests, mesh quality, and CAD import against an independent kernel.
A TET10 element has four corner nodes and six mid-side nodes: displacement varies quadratically inside each element, stress varies linearly, and curved faces follow the surface. A TET15 adds a node on each face and one at the centre, which improves the near-incompressible response and the contact pressure at the same mesh size.

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