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Assessment of multi-fuel powered turbofans:Performance,dimensions and emissions

Xin ZHAO Tomas GRÖNSTEDT Moritz G.KOLB

中国航空学报(英文版)2026,Vol.39Issue(9):44-62,19.
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中国航空学报(英文版)2026,Vol.39Issue(9):44-62,19.DOI:10.1016/j.cja.2026.104082

Assessment of multi-fuel powered turbofans:Performance,dimensions and emissions

Assessment of multi-fuel powered turbofans:Performance,dimensions and emissions

Xin ZHAO 1Tomas GRÖNSTEDT 1Moritz G.KOLB2

作者信息

  • 1. Department of Mechanics and Maritime Sciences,Chalmers University of Technology,Göteborg 41296,Sweden
  • 2. Bauhaus Luftfahrt e.V.,Taufkirchen 82024,Germany
  • 折叠

摘要

关键词

Chemical equilibrium/Emissions/Engine performance/Hydrogen/Jet-A/Multi-fuel/Turbofan engine/Weight estimation

Key words

Chemical equilibrium/Emissions/Engine performance/Hydrogen/Jet-A/Multi-fuel/Turbofan engine/Weight estimation

引用本文复制引用

Xin ZHAO,Tomas GRÖNSTEDT,Moritz G.KOLB..Assessment of multi-fuel powered turbofans:Performance,dimensions and emissions[J].中国航空学报(英文版),2026,39(9):44-62,19.

基金项目

This work had received funding from the Horizon Europe Research and Innovation Programme(No.101096275).This work was co-funded by UK Research and Innovation(UKRI)under the UK Government's Horizon Europe Guarantee Funding(No.10068673). (No.101096275)

中国航空学报(英文版)

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