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Aerospace & Advanced Manufacturing · Simulation Study

Certify composite structures and qualify AM parts with fewer physical test campaigns.

Simulation studies for CFRP damage tolerance, repair substantiation, residual stress prediction, and additive manufacturing distortion compensation.

Grab a scoping call
USD 1.5–2.1M
Saved vs physical fatigue test campaign (simulation + 5 coupons vs 25 specimens, 18–24 months)
50:1
Risk-adjusted ROI: USD 170k simulation vs USD 8–15M rework risk at first-article stage
6–10 wks
Study to certification evidence package
Applications

What we can study for you

  • Composite damage tolerance analysis for certification evidence
  • Impact damage prediction for bird strike and hail scenarios
  • Repair substantiation with predicted residual strength recovery
  • Fatigue life prediction with manufacturing variability effects
  • Cure cycle residual stress and spring-back prediction
  • AM distortion compensation for first-time-right builds

Material Spec & Layup

Laminate Failure Simulation

Fatigue & Damage Modelling

Certification Evidence Package

Test Article Reduction Plan

Our Approach

Physics-based prediction of damage tolerance and fatigue life

We run simulation studies that predict composite failure with manufacturing defects explicitly modelled. The goal is to reduce the number of physical tests needed for certification, not by lowering the standard, but by providing higher-fidelity predictions that the certification authority can assess.

  • Progressive damage analysis with explicit modelling of matrix cracking, delamination, and fibre failure under fatigue loading
  • Manufacturing defect simulation including porosity, fibre waviness, and ply drops, predicting their effect on structural performance
  • Residual stress prediction from cure cycle simulation through to in-service thermal loading
  • Repair substantiation analysis that predicts restored structural capability for specific defect geometries and repair configurations
Studies We Offer

Specific studies, fixed scope.

4–6 week study
Composite Damage Tolerance Analysis

Simulating high-velocity impacts (hail, bird strikes, runway debris) to predict internal disbonding and residual strength without physical test campaigns.

3–5 week engagement
Additive Manufacturing Residual Stress

Predicting thermal gradients and microstructural evolution during 3D printing to compensate for part distortion before the first build.

Describe your Aerospace & Advanced Manufacturing challenge.

We'll scope a study within 48 hours and tell you whether our platform can help. No commitment required.

Grab a scoping call

or email [email protected]