Target outcome

  • ¬†Development of design methods suitable to scale combustor geometries for future aero-engine architectures
  • High fidelity LES methods and emission prediction models
  • Up to 50% reduction of combustor development time compared to state-of-the-art design processes
  • Ability to perform combustion optimization at different stages within the combustor development due to automated combustor aero-design processes
  • Applicable for direct driven and geared turbofans and open rotor, driven by kerosene or alternative fuel
  • Exploitation: B737, A320 and B777 successor aircrafts

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