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Parametric study on the distribution of flow rate and heat sink utilization in cooling channels of advanced aero-engines

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  • Jiang, Yuguang
  • Xu, Yaxing
  • Zhang, Silong
  • Chetehouna, Khaled
  • Gascoin, Nicolas
  • Qin, Jiang
  • Bao, Wen

Abstract

Recently, advanced aero-engines have become more and more important in the development of society, which are expected to be capable of higher and higher flight Mach number to meet the needs of modern life. However, considering the high total temperature of freestream and serious aerodynamic heating with high Mach numbers, the cooling and energy management thus become a serious challenge. Taking scramjet for example, the fuel flow mal-distribution in parallel cooling channels during regenerative cooling may cause severe energy waste and even over temperature. To get more information about this problem, in this work, a 3D numerical parametric analysis has been carried out for the flow distribution and energy utilization. The effects of aspect ratio, rib thickness and flow area in branch channels were studied and the mechanism of flow distribution with present configuration was analyzed.

Suggested Citation

  • Jiang, Yuguang & Xu, Yaxing & Zhang, Silong & Chetehouna, Khaled & Gascoin, Nicolas & Qin, Jiang & Bao, Wen, 2017. "Parametric study on the distribution of flow rate and heat sink utilization in cooling channels of advanced aero-engines," Energy, Elsevier, vol. 138(C), pages 1056-1068.
    • Handle: RePEc:eee:energy:v:138:y:2017:i:c:p:1056-1068
    DOI: 10.1016/j.energy.2017.07.091
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    References listed on IDEAS

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    1. Zhang, Duo & Yang, Shengbo & Zhang, Silong & Qin, Jiang & Bao, Wen, 2015. "Thermodynamic analysis on optimum performance of scramjet engine at high Mach numbers," Energy, Elsevier, vol. 90(P1), pages 1046-1054.
    2. Zhang, Silong & Cui, Naigang & Xiong, Yuefei & Feng, Yu & Qin, Jiang & Bao, Wen, 2017. "Effect of channel aspect ratio on chemical recuperation process in advanced aeroengines," Energy, Elsevier, vol. 123(C), pages 9-19.
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    Cited by:

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    4. Liu, Penghua & Wang, Renting & Liu, Shaobei & Bao, Zewei, 2023. "Experimental study on the thermal-hydraulic performance of a tube-in-tube helical coil air–fuel heat exchanger for an aero-engine," Energy, Elsevier, vol. 267(C).
    5. Bahiraei, Mehdi & Mazaheri, Nima, 2021. "Application of an ecofriendly nanofluid containing graphene nanoplatelets inside a novel spiral liquid block for cooling of electronic processors," Energy, Elsevier, vol. 218(C).
    6. Feng, Yu & Liu, Yuna & Cao, Yong & Gong, Keyu & Liu, Shuyuan & Qin, Jiang, 2020. "Thermal management evaluation for advanced aero-engines using catalytic steam reforming of hydrocarbon fuels," Energy, Elsevier, vol. 193(C).
    7. Mengqiang Dong & Hongyan Huang, 2023. "Effect of Rotating Channel Turning Section Clearance Size on Heat Transfer Characteristics of Supercritical Pressure Hydrocarbon Fuel," Energies, MDPI, vol. 16(16), pages 1-18, August.
    8. Xu, Jing & Cheng, Kunlin & Dang, Chaolei & Wang, Yilin & Liu, Zekuan & Qin, Jiang & Liu, Xiaoyong, 2023. "Performance comparison of liquid metal cooling system and regenerative cooling system in supersonic combustion ramjet engines," Energy, Elsevier, vol. 275(C).
    9. Zhang, Yueliang & Li, Jiangheng & Xie, Jin, 2022. "Effects of lateral cooling hole configuration on a swirl-stabilized combustor," Energy, Elsevier, vol. 259(C).

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