With the resurgence of supersonic passenger aircraft in aviation, the imperative for environmental sustainability has become increasingly critical. This study proposes a hydrogen-fueled distributed turbogenerator-electric propulsion system for next-generation environmentally sustainable supersonic airliners. A zero-dimensional component-level simulation model was developed using the Matlab/Simulink environment, integrating an object-oriented programming approach with S-function modules. Computational analyses validated the system’s operational feasibility and safety compliance. The proposed system achieves zero carbon emissions while fulfilling the transoceanic and supersonic operational requirements of a 10-seat business jet, thereby addressing both performance and environmental sustainability objectives.

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Verification and Validation of Propulsion Systems for Next-Generation Eco-friendly Supersonic Passenger Aircraft

  • Suyue Ding,
  • Shuang Yao,
  • Min Chen,
  • Jiyuan Zhang,
  • Hailong Tang,
  • Yihao Xu

摘要

With the resurgence of supersonic passenger aircraft in aviation, the imperative for environmental sustainability has become increasingly critical. This study proposes a hydrogen-fueled distributed turbogenerator-electric propulsion system for next-generation environmentally sustainable supersonic airliners. A zero-dimensional component-level simulation model was developed using the Matlab/Simulink environment, integrating an object-oriented programming approach with S-function modules. Computational analyses validated the system’s operational feasibility and safety compliance. The proposed system achieves zero carbon emissions while fulfilling the transoceanic and supersonic operational requirements of a 10-seat business jet, thereby addressing both performance and environmental sustainability objectives.