Multiple aspects to flight mission performances improvement of commercial turbofan engine via variable geometry adjustment
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DOI: 10.1016/j.energy.2022.125693
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Cited by:
- He, Honglin & Yang, Xiaojun & Li, Chunyang & Teng, Jinfang, 2024. "Numerical analysis of the landing and take-off cycle standard for supersonic engines based on pollutant emission characteristics," Energy, Elsevier, vol. 299(C).
- Korba, Peter & Balli, Ozgur & Caliskan, Hakan & Al-Rabeei, Samer & Kale, Utku, 2023. "Energy, exergy, economic, environmental, and sustainability assessments of the CFM56-3 series turbofan engine used in the aviation sector," Energy, Elsevier, vol. 269(C).
- Luo, Qiaodan & Zhao, Shengfeng & Zhou, Shiji & Yao, Lipan & Yang, Chengwu & Lu, Xingen & Zhu, Junqiang, 2024. "Influence of diversified dihedral stator on the thermodynamic performance and flow loss characteristics of a variable core driven fan stage," Energy, Elsevier, vol. 294(C).
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Keywords
Flight mission performance; Variable geometry commercial engine; Energy and exergy analysis; Sustainability level; Optimization regulation;All these keywords.
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