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Thermal Protection System and Thermal Management for Combined-Cycle Engine: Review and Prospects

Author

Listed:
  • Yiwei Dong

    (School of Aerospace Engineering, Xiamen University, 422 South Siming Road, Xiamen 361005, China
    Shenzhen Research Institute, Xiamen University, No.19, Gaoxin South 4th Road, Nanshan District, Shenzhen 518057, China)

  • Ertai Wang

    (School of Aerospace Engineering, Xiamen University, 422 South Siming Road, Xiamen 361005, China)

  • Yancheng You

    (School of Aerospace Engineering, Xiamen University, 422 South Siming Road, Xiamen 361005, China)

  • Chunping Yin

    (School of Aerospace Engineering, Xiamen University, 422 South Siming Road, Xiamen 361005, China)

  • Zongpu Wu

    (School of Aerospace Engineering, Xiamen University, 422 South Siming Road, Xiamen 361005, China)

Abstract

Combined-cycle engine is a potential propulsion system for hypersonic aircraft. To ensure long-term, normal operation of combined-cycle engine under the harsh environment of high thermal load, it is of great significance to study the thermal protection and management of the propulsion system. In this study, the objective and development status of thermal protection and thermal management systems for the combined-cycle propulsion system were described. The latest research progresses of thermal protection, thermal barrier coating, and thermal management system of the combined-cycle propulsion system were summarized. Moreover, the problems and shortcoming in current researches were summarized. In addition, a prospect for the future development of thermal protection and management of the combined-cycle propulsion system was presented, pointing out a direction of great value and vital research significance to thermal protection and management of the combined-cycle propulsion system.

Suggested Citation

  • Yiwei Dong & Ertai Wang & Yancheng You & Chunping Yin & Zongpu Wu, 2019. "Thermal Protection System and Thermal Management for Combined-Cycle Engine: Review and Prospects," Energies, MDPI, vol. 12(2), pages 1-51, January.
    • Handle: RePEc:gam:jeners:v:12:y:2019:i:2:p:240-:d:197574
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    References listed on IDEAS

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    Cited by:

    1. Liang Guo & Liping Pang & Jingquan Zhao & Xiaodong Yang, 2022. "Optimization of Power and Thermal Management System of Hypersonic Vehicle with Finite Heat Sink of Fuel," Energies, MDPI, vol. 15(15), pages 1-19, July.
    2. Xiaota Cheng & Yi-Tao Liu & Yang Si & Jianyong Yu & Bin Ding, 2022. "Direct synthesis of highly stretchable ceramic nanofibrous aerogels via 3D reaction electrospinning," Nature Communications, Nature, vol. 13(1), pages 1-8, December.
    3. Xu, Qing & Li, Haowei & Feng, Yaoxun & Li, Xiaoning & Ling, Changming & Zhou, Chaoying & Qin, Jiang, 2020. "Dynamic thermo-physical characteristics of high temperature gaseous hydrocarbon fuel thermal power generation for regeneratively cooled hypersonic propulsion system," Energy, Elsevier, vol. 211(C).
    4. Runlin Zhang & Nuo Xu & Kai Zhang & Lei Wang & Gui Lu, 2023. "A Parametric Physics-Informed Deep Learning Method for Probabilistic Design of Thermal Protection Systems," Energies, MDPI, vol. 16(9), pages 1-20, April.

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