Performance evaluation of a turbojet engine integrated with interstage turbine burner and solid oxide fuel cell
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DOI: 10.1016/j.energy.2018.11.088
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- Ji, Zhixing & Rokni, Marvin Mikael & Qin, Jiang & Zhang, Silong & Dong, Peng, 2021. "Performance and size optimization of the turbine-less engine integrated solid oxide fuel cells on unmanned aerial vehicles with long endurance," Applied Energy, Elsevier, vol. 299(C).
- Zhao, Hang & Liao, Zengbu & Liu, Jinxin & Li, Ming & Liu, Wei & Wang, Lei & Song, Zhiping, 2022. "A highly robust thrust estimation method with dissimilar redundancy framework for gas turbine engine," Energy, Elsevier, vol. 245(C).
- Cihangir, Serhan Ahmet & Aygun, Hakan & Turan, Onder, 2022. "Energy and performance analysis of a turbofan engine with the aid of dynamic component efficiencies," Energy, Elsevier, vol. 260(C).
- Ji, Zhixing & Qin, Jiang & Cheng, Kunlin & Guo, Fafu & Zhang, Silong & Dong, Peng, 2019. "Thermodynamics analysis of a turbojet engine integrated with a fuel cell and steam injection for high-speed flight," Energy, Elsevier, vol. 185(C), pages 190-201.
- Seyam, Shaimaa & Dincer, Ibrahim & Agelin-Chaab, Martin, 2021. "Investigation of two hybrid aircraft propulsion and powering systems using alternative fuels," Energy, Elsevier, vol. 232(C).
- Huang, Yu & Turan, Ali, 2022. "Flexible power generation based on solid oxide fuel cell and twin-shaft free turbine engine: Mechanical equilibrium running and design analysis," Applied Energy, Elsevier, vol. 315(C).
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Keywords
More/all-electric aircraft; Turbojet engine; Solid oxide fuel cell; Interstage turbine burner; Specific thrust; Electric generation;All these keywords.
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