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Physics-resolved design, from field to geometry.

Fig. 1.1 — A multi-load aerospace bracket resolved through constrained topology optimisation. XLAB couples the mesh, governing physics and design variables inside one inspectable study.

34%

Median mass removed on structural parts

12×

Faster design iteration vs. manual CAD loops

< 2h

From CAD upload to first converged candidate

Ref: TOP-A24Topology-optimized titanium aerospace bracket with von Mises stress colormap
BRACKET_01_TOPO_OPTMASS −34.6%SF 1.86

Archive index

Recent computational studies

Disciplines

Three coupled physics domains, one design loop

CFD render of a generatively designed liquid cold plate with temperature colormap

Platform

Your solvers, your data, your certification trail

XLAB Innovations is solver-agnostic. It orchestrates the tools you already trust, learns from the test data you already own, and keeps every run reproducible.

One study definition

Load cases, materials, constraints and objectives are declared once and reused across every discipline and every design candidate.

Traceable design history

Every run is versioned with its mesh, solver settings and results, so certification evidence is a query rather than an archaeology project.

Surrogate acceleration

Trained on your own historic test and simulation data, surrogate models screen thousands of candidates before the expensive solver is called.

Case study · eVTOL programme

Flutter-clear wing structure in one design cycle

A two-way coupled FSI campaign across 640 flight points replaced a six-week manual sweep. The team cleared flutter margins at maximum dive speed while removing 41 kg from the primary structure.

640

Coupled flight points

41 kg

Structural mass removed

6 → 1

Weeks per design cycle

Aeroelastic fluid-structure interaction simulation of a deforming aircraft wing

Put physics in the loop, not at the end of it.

See XLAB Innovations run a topology, FSI or thermofluid study on one of your own components in a 45-minute technical session.