Combining effect of optimized axial compressor variable guide vanes and bleed air on the thermodynamic performance of aircraft engine system
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DOI: 10.1016/j.energy.2016.12.076
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- Tona, Cesare & Raviolo, Paolo Antonio & Pellegrini, Luiz Felipe & de Oliveira Júnior, Silvio, 2010. "Exergy and thermoeconomic analysis of a turbofan engine during a typical commercial flight," Energy, Elsevier, vol. 35(2), pages 952-959.
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Cited by:
- Kim, Sangjo & Kim, Kuisoon & Son, Changmin, 2020. "Transient system simulation for an aircraft engine using a data-driven model," Energy, Elsevier, vol. 196(C).
- Kim, Sangjo, 2021. "A new performance adaptation method for aero gas turbine engines based on large amounts of measured data," Energy, Elsevier, vol. 221(C).
- Kim, Sangjo & Kim, Kuisoon & Son, Changmin, 2020. "A new transient performance adaptation method for an aero gas turbine engine," Energy, Elsevier, vol. 193(C).
- Qiang, Xiaoqing & Lu, Yao & Li, Jian, 2024. "Bleed air CFD modelling in aerodynamic simulation of A heavy duty gas turbine compressor," Energy, Elsevier, vol. 299(C).
- Chen, Yu-Zhi & Tsoutsanis, Elias & Xiang, Heng-Chao & Li, Yi-Guang & Zhao, Jun-Jie, 2022. "A dynamic performance diagnostic method applied to hydrogen powered aero engines operating under transient conditions," Applied Energy, Elsevier, vol. 317(C).
- Pang, Liping & Luo, Kun & Yuan, Yanping & Mao, Xiaodong & Fang, Yufeng, 2020. "Thermal performance of helicopter air conditioning system with lube oil source (LOS) heat pump," Energy, Elsevier, vol. 190(C).
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Keywords
Variable guide vanes; Bleed air; Surge margin; Axial compressor; Turbofan engine; Optimization;All these keywords.
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