IDEAS home Printed from https://ideas.repec.org/a/eee/energy/v216y2021ics0360544220323781.html
   My bibliography  Save this article

Research on the operating boundary of the dual mode scramjet with a constant area combustor through thermodynamic cycle analysis

Author

Listed:
  • Wang, Youyin
  • Hou, Wenxin
  • Zhang, Junlong
  • Tang, Jingfeng
  • Chang, Juntao
  • Bao, Wen

Abstract

The maximum pressure ratio of the isolator is important for studying the operating boundary of the dual mode scramjet. In this paper, the pressure rise mechanism of the dual mode scramjet engine and the characteristic of the isolator maximum pressure rise are analyzed. The operating range and performance of scramjet under the pressure rise limit are investigated using the constant cross-sectional area combustor. The maximum pressure ratio of the isolator confines the back pressure from the combustor so that the scramjet engine has a minimum freestream Mach number of each equivalence ratio. When the freestream Mach number is smaller than the minimum freestream Mach number, an expansion section may be arranged between the combustor and the isolator to balance the pressure of the combustor and that of the isolator. The expression of the minimum freestream Mach number is derived and it is found that the minimum freestream Mach number of the dual mode scramjet in both modes increases with the increase of equivalence ratio and compression ratio of the inlet. A variable divergent section is suggested to balance the pressure under different freestream Mach numbers and equivalence ratios.

Suggested Citation

  • Wang, Youyin & Hou, Wenxin & Zhang, Junlong & Tang, Jingfeng & Chang, Juntao & Bao, Wen, 2021. "Research on the operating boundary of the dual mode scramjet with a constant area combustor through thermodynamic cycle analysis," Energy, Elsevier, vol. 216(C).
    • Handle: RePEc:eee:energy:v:216:y:2021:i:c:s0360544220323781
    DOI: 10.1016/j.energy.2020.119271
    as

    Download full text from publisher

    File URL: http://www.sciencedirect.com/science/article/pii/S0360544220323781
    Download Restriction: Full text for ScienceDirect subscribers only
    File URL: https://libkey.io/10.1016/j.energy.2020.119271?utm_source=ideas
    LibKey link: if access is restricted and if your library uses this service, LibKey will redirect you to where you can use your library subscription to access this item
    ---><---

    As the access to this document is restricted, you may want to search for a different version of it.

    References listed on IDEAS

    as
    1. 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.
    2. Li, Zhixiong & Manh, Tran Dinh & Barzegar Gerdroodbary, Mostafa & Nam, Nguyen Dang & Moradi, R. & Babazadeh, Houman, 2020. "The effect of sinusoidal wall on hydrogen jet mixing rate considering supersonic flow," Energy, Elsevier, vol. 193(C).
    3. 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.
    4. Du, Zhao-bo & Huang, Wei & Yan, Li, 2019. "Parametric study on mixing augmentation mechanism induced by air injection in a shock-induced combustion ramjet engine," Energy, Elsevier, vol. 186(C).
    5. Li, Jianping & Liao, Zilong & Jiao, Guiqian & Song, Wenyan, 2019. "The mode transition characteristics in a dual-mode combustor at different total temperatures," Energy, Elsevier, vol. 188(C).
    6. Zhang, Tiantian & Wang, Zhenguo & Huang, Wei & Ingham, Derek & Ma, Lin & Porkashanian, Mohamed, 2020. "An analysis tool of the rocket-based combined cycle engine and its application in the two-stage-to-orbit mission," Energy, Elsevier, vol. 193(C).
    7. 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.
    8. Amati, V. & Bruno, C. & Simone, D. & Sciubba, E., 2008. "Exergy analysis of hypersonic propulsion systems: Performance comparison of two different scramjet configurations at cruise conditions," Energy, Elsevier, vol. 33(2), pages 116-129.
    9. 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.
    10. Qin, Jiang & Cheng, Kunlin & Zhang, Silong & Zhang, Duo & Bao, Wen & Han, Jiecai, 2016. "Analysis of energy cascade utilization in a chemically recuperated scramjet with indirect combustion," Energy, Elsevier, vol. 114(C), pages 1100-1106.
    11. Zhang, Silong & Qin, Jiang & Bao, Wen & Feng, Yu & Xie, Kaili, 2014. "Thermal management of fuel in advanced aeroengine in view of chemical recuperation," Energy, Elsevier, vol. 77(C), pages 201-211.
    12. Li, Xiaojie & Huang, Xiaobin & Liu, Hong & Du, Jianke, 2020. "Fuel reactivity controlled self-starting and propulsion performance of a scramjet: A model investigation," Energy, Elsevier, vol. 195(C).
    13. 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.
    Full references (including those not matched with items on IDEAS)

    Citations

    Citations are extracted by the CitEc Project, subscribe to its RSS feed for this item.
    as


    Cited by:

    1. Lv, Chengkun & Xu, Haiqi & Chang, Juntao & Wang, Youyin & Chen, Ruoyu & Yu, Daren, 2022. "Mode transition analysis of a turbine-based combined-cycle considering ammonia injection pre-compressor cooling and variable-geometry ram-combustor," Energy, Elsevier, vol. 261(PB).
    2. Lv, Chengkun & Huang, Qian & Chang, Juntao & Wang, Ziao & Zheng, Jialin & Yu, Daren, 2023. "Mode transition path optimization for turbine-based combined-cycle ramjet stage under uncertainty propagation of integrated airframe-propulsion system," Energy, Elsevier, vol. 268(C).
    3. Liu, Yunfeng & Han, Xin & Zhang, Zijian, 2024. "Study on the propulsive performance of oblique detonation engine," Energy, Elsevier, vol. 292(C).

    Most related items

    These are the items that most often cite the same works as this one and are cited by the same works as this one.
    1. Ambe Verma, Kumari & Murari Pandey, Krishna & Ray, Mukul & Kumar Sharma, Kaushal, 2021. "Effect of transverse fuel injection system on combustion efficiency in scramjet combustor," Energy, Elsevier, vol. 218(C).
    2. Li, Xiaojie & Huang, Xiaobin & Liu, Hong & Du, Jianke, 2020. "Fuel reactivity controlled self-starting and propulsion performance of a scramjet: A model investigation," Energy, Elsevier, vol. 195(C).
    3. 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).
    4. 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).
    5. Qin, Jiang & Cheng, Kunlin & Zhang, Silong & Zhang, Duo & Bao, Wen & Han, Jiecai, 2016. "Analysis of energy cascade utilization in a chemically recuperated scramjet with indirect combustion," Energy, Elsevier, vol. 114(C), pages 1100-1106.
    6. Xiong, Yuefei & Qin, Jiang & Cheng, Kunlin & Wang, Youyin, 2020. "Influence of water injection on performance of scramjet engine," Energy, Elsevier, vol. 201(C).
    7. Li, Xin & Zhang, Silong & Ye, Mai & Qin, Jiang & Bao, Wen & Cui, Naigang & Liu, Xiaoyong & Zhou, Chaoying, 2020. "Effect of enhanced heat transfer structures on the chemical recuperation process of advanced aero-engine," Energy, Elsevier, vol. 211(C).
    8. Liu, Yunfeng & Han, Xin & Zhang, Zijian, 2024. "Study on the propulsive performance of oblique detonation engine," Energy, Elsevier, vol. 292(C).
    9. Zhang, Tiantian & Wang, Zhenguo & Huang, Wei & Ingham, Derek & Ma, Lin & Porkashanian, Mohamed, 2020. "An analysis tool of the rocket-based combined cycle engine and its application in the two-stage-to-orbit mission," Energy, Elsevier, vol. 193(C).
    10. Yan, Li & Liao, Lei & Meng, Yu-shan & Li, Shi-bin & Huang, Wei, 2020. "Investigation on the mode transition of a typical three-dimensional scramjet combustor equipped with a strut," Energy, Elsevier, vol. 208(C).
    11. Tian, Ke & Tang, Zicheng & Wang, Jin & Ma, Ting & Zeng, Min & Wang, Qiuwang, 2022. "Numerical investigation of pyrolysis and surface coking of hydrocarbon fuel in the regenerative cooling channel," Energy, Elsevier, vol. 260(C).
    12. Luo, Feiteng & Song, Wenyan & Li, Jianping & Chen, Wenjuan & Long, Yaosong, 2021. "Experimental study of kerosene supersonic combustion with pilot hydrogen and fuel additive under low flight mach conditions," Energy, Elsevier, vol. 222(C).
    13. Yu, Xuanfei & Wang, Cong & Yu, Daren, 2019. "Precooler-design & engine-performance conjugated optimization for fuel direct precooled airbreathing propulsion," Energy, Elsevier, vol. 170(C), pages 546-556.
    14. 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.
    15. 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.
    16. Zhao, Wei & Huang, Chen & Zhao, Qingjun & Ma, Yingqun & Xu, Jianzhong, 2018. "Performance analysis of a pre-cooled and fuel-rich pre-burned mixed-flow turbofan cycle for high speed vehicles," Energy, Elsevier, vol. 154(C), pages 96-109.
    17. Zhang, Duo & Qin, Jiang & Feng, Yu & Ren, Fengzhi & Bao, Wen, 2014. "Performance evaluation of power generation system with fuel vapor turbine onboard hydrocarbon fueled scramjets," Energy, Elsevier, vol. 77(C), pages 732-741.
    18. 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.
    19. Peng, Yeping & Barzegar Gerdroodbary, M. & Sheikholeslami, M. & Shafee, Ahmad & Babazadeh, Houman & Moradi, R., 2020. "Mixing enhancement of the multi hydrogen fuel jets by the backward step," Energy, Elsevier, vol. 203(C).
    20. Ma, Guangwei & Zhao, Guoyan & Sun, Mingbo & Xiong, Dapeng & Li, Fan & Liu, Mingjiang & Wang, Hongbo, 2024. "On compression level of hypersonic airflow in high-mach scramjet," Energy, Elsevier, vol. 295(C).

    Corrections

    All material on this site has been provided by the respective publishers and authors. You can help correct errors and omissions. When requesting a correction, please mention this item's handle: RePEc:eee:energy:v:216:y:2021:i:c:s0360544220323781. See general information about how to correct material in RePEc.

    If you have authored this item and are not yet registered with RePEc, we encourage you to do it here. This allows to link your profile to this item. It also allows you to accept potential citations to this item that we are uncertain about.

    If CitEc recognized a bibliographic reference but did not link an item in RePEc to it, you can help with this form .

    If you know of missing items citing this one, you can help us creating those links by adding the relevant references in the same way as above, for each refering item. If you are a registered author of this item, you may also want to check the "citations" tab in your RePEc Author Service profile, as there may be some citations waiting for confirmation.

    For technical questions regarding this item, or to correct its authors, title, abstract, bibliographic or download information, contact: Catherine Liu (email available below). General contact details of provider: http://www.journals.elsevier.com/energy .

    Please note that corrections may take a couple of weeks to filter through the various RePEc services.

    IDEAS is a RePEc service. RePEc uses bibliographic data supplied by the respective publishers.