Topology · FSI · Thermofluid
Let the physics decide the geometry.
XLAB Innovations is the design-intelligence layer between your simulation stack and your engineering decisions. Define the objective, the loads and the manufacturing envelope — get performance-driven geometry and validated results, in hours.
34%
Median mass removed on structural parts
12×
Faster design iteration vs. manual CAD loops
< 2h
From CAD upload to first converged candidate
Built for the engineering teams shipping the hardest hardware
Disciplines
Three coupled physics domains, one design loop
Topology optimization
Generate load-path-optimal geometry under stress, stiffness, buckling and manufacturing constraints — not a post-processed mesh you have to redraw.
ExploreFluid-structure interaction
Two-way coupled aeroelastic and hydroelastic analysis: flutter margins, gust response, sloshing and seal deflection under real operating envelopes.
ExploreThermofluid & CHT
Conjugate heat transfer driven design for cold plates, heat exchangers, battery packs and electronics — optimising ΔT and Δp simultaneously.
Explore
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
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.