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Performance analysis on the specific impulse and specific thrust of scramjet with a quasi-one-dimensional model

Author

Listed:
  • Li, Chaolong
  • Xia, Zhixun
  • Ma, Likun
  • Chen, Binbin
  • Feng, Yunchao
  • Zhang, Jiarui
  • Duan, Yifan

Abstract

A quasi-one-dimensional model for performance analysis of scramjet has been developed for rapid design and optimization in the current paper. The heat release process along the supersonic combustor is based on the assumption of chemical equilibrium. Furthermore, the effects of flight Mach number ranging from 6 to 14, equivalence ratio ranging from 0.1 to 1.0, and three types of fuel (including boron-B, hydrocarbon-CH, and hydrogen-H2) on the performance of the scramjet have been studied. The energy specific impulse is proposed for the first time to evaluate the energy conversion ability of chemical energy to mechanical energy for different fuels. The results show that mass specific impulse not only depends on the heat value of the fuel but is also closely related to the energy conversion ability of the fuel. And the condensation heat and specific heat capacity of combustion products, and the mole ratio of the gaseous products to the gaseous reactants are the three main factors affecting the energy conversion ability for different fuels. Compared with the CH-fueled scramjet and H2-fueled scramjet, the B-fueled scramjet has the potential for miniaturization and can cruise at a higher Mach number, due to its larger volume specific impulse and specific thrust, respectively.

Suggested Citation

  • Li, Chaolong & Xia, Zhixun & Ma, Likun & Chen, Binbin & Feng, Yunchao & Zhang, Jiarui & Duan, Yifan, 2023. "Performance analysis on the specific impulse and specific thrust of scramjet with a quasi-one-dimensional model," Energy, Elsevier, vol. 267(C).
  • Handle: RePEc:eee:energy:v:267:y:2023:i:c:s0360544222032868
    DOI: 10.1016/j.energy.2022.126400
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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. Bao, Wen & Zhang, Silong & Qin, Jiang & Zhou, Weixing & Xie, Kaili, 2014. "Numerical analysis of flowing cracked hydrocarbon fuel inside cooling channels in view of thermal management," Energy, Elsevier, vol. 67(C), pages 149-161.
    3. Feng, Rong & Zhu, Jiajian & Wang, Zhenguo & Sun, Mingbo & Wang, Hongbo & Cai, Zun & An, Bin & Li, Liang, 2021. "Ignition modes of a cavity-based scramjet combustor by a gliding arc plasma," Energy, Elsevier, vol. 214(C).
    4. Yu, Xuanfei & Wang, Cong & Yu, Daren, 2019. "Thermodynamic assessment on performance extremes of the fuel indirect precooled cycle for hypersonic airbreathing propulsion," Energy, Elsevier, vol. 186(C).
    5. Yang, Qingchun & Chang, Juntao & Bao, Wen, 2014. "Thermodynamic analysis on specific thrust of the hydrocarbon fueled scramjet," Energy, Elsevier, vol. 76(C), pages 552-558.
    6. Cheng, Kunlin & Qin, Jiang & Sun, Hongchuang & Li, Heng & He, Shuai & Zhang, Silong & Bao, Wen, 2019. "Power optimization and comparison between simple recuperated and recompressing supercritical carbon dioxide Closed-Brayton-Cycle with finite cold source on hypersonic vehicles," Energy, Elsevier, vol. 181(C), pages 1189-1201.
    7. Bergthorson, Jeffrey M. & Yavor, Yinon & Palecka, Jan & Georges, William & Soo, Michael & Vickery, James & Goroshin, Samuel & Frost, David L. & Higgins, Andrew J., 2017. "Metal-water combustion for clean propulsion and power generation," Applied Energy, Elsevier, vol. 186(P1), pages 13-27.
    8. Cai, Zun & Zhu, Jiajian & Sun, Mingbo & Wang, Zhenguo & Bai, Xue-Song, 2018. "Ignition processes and modes excited by laser-induced plasma in a cavity-based supersonic combustor," Applied Energy, Elsevier, vol. 228(C), pages 1777-1782.
    9. He, Yubao & Cao, Ruifeng & Huang, Hongyan & Qin, Jiang & Yu, Daren, 2017. "Overall performance assessment for scramjet with boundary-layer ejection control based on thermodynamics," Energy, Elsevier, vol. 121(C), pages 318-330.
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