IDEAS home Printed from https://ideas.repec.org/a/eee/energy/v264y2023ics0360544222030560.html
   My bibliography  Save this article

Initiation of an upstream propagating detonation wave near the open end of the detonation tube operating in the valveless and purgeless scheme

Author

Listed:
  • Tan, Fengguang
  • Fan, Wei
  • Wang, Ke
  • Jin, Shufeng
  • Chen, Shuping

Abstract

Controllable and sustainable operations are the basic need for the practical pulse detonation engines (PDEs). Previous works have demonstrated that the valveless and purgeless scheme is beneficial to achieve high frequency detonations. However, steady deflagration often arises in the implementation of a long duration operation, especially when the more reactive fresh mixture is employed. To this end, three types of detonation tubes, named as type-A, type-B, and type-C, in which an upstream propagating detonation wave will be produced are experimentally investigated. In this study, the detonation wave is initiated near the open end of the detonation tube through the deflagration to detonation transition (DDT) process, and thus, the fresh reactive mixture was consumed by the upstream propagating detonation wave. Experimental results indicate that the detonation cycles can be maintained by utilizing the upstream detonation waves, and the sustainability has been dramatically improved. Especially, the available oxygen volume fraction of the oxidizer is improved to about 80% for the type-C detonation tube. In addition, the propulsive performance has been improved by 9.5% utilizing the upstream propagating detonation wave in the type-C detonation tube, and meanwhile the fluctuation of the thrust during the detonation cycle can be decreased.

Suggested Citation

  • Tan, Fengguang & Fan, Wei & Wang, Ke & Jin, Shufeng & Chen, Shuping, 2023. "Initiation of an upstream propagating detonation wave near the open end of the detonation tube operating in the valveless and purgeless scheme," Energy, Elsevier, vol. 264(C).
    • Handle: RePEc:eee:energy:v:264:y:2023:i:c:s0360544222030560
    DOI: 10.1016/j.energy.2022.126170
    as

    Download full text from publisher

    File URL: http://www.sciencedirect.com/science/article/pii/S0360544222030560
    Download Restriction: Full text for ScienceDirect subscribers only
    File URL: https://libkey.io/10.1016/j.energy.2022.126170?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, Qibin & Wang, Ke & Dong, Rongxiao & Fan, Wei & Lu, Wei & Wang, Yongjia, 2019. "Experimental research on propulsive performance of the pulse detonation rocket engine with a fluidic nozzle," Energy, Elsevier, vol. 166(C), pages 1267-1275.
    2. Wang, Ke & Fan, Wei & Lu, Wei & Chen, Fan & Zhang, Qibin & Yan, Chuanjun, 2014. "Study on a liquid-fueled and valveless pulse detonation rocket engine without the purge process," Energy, Elsevier, vol. 71(C), pages 605-614.
    3. Wang, Ke & Wang, Zhicheng & Zhao, Minghao & Sun, Tianyu & Tan, Fengguang & Zhu, Yiyuan & Lu, Wei & Yu, Xiaodong & Sha, Yu & Fan, Wei, 2019. "Study on the valveless and purgeless scheme to produce high frequency detonations in a long duration," Energy, Elsevier, vol. 189(C).
    Full references (including those not matched with items on IDEAS)

    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. Warimani, Mahammadsalman & Azami, Muhammad Hanafi & Khan, Sher Afghan & Ismail, Ahmad Faris & Saharin, Sanisah & Ariffin, Ahmad Kamal, 2021. "Internal flow dynamics and performance of pulse detonation engine with alternative fuels," Energy, Elsevier, vol. 237(C).
    2. Wang, Ke & Fan, Wei & Lu, Wei & Zhang, Qibin & Chen, Fan & Yan, Chuanjun & Xia, Qiang, 2015. "Propulsive performance of a pulse detonation rocket engine without the purge process," Energy, Elsevier, vol. 79(C), pages 228-234.
    3. Liu, Junyu & Wang, Zhiwu & Qin, Weifeng & Li, Junlin & Zhang, Zixu & Huang, Jingjing, 2023. "Effects of detonation initial conditions on performance of pulse detonation chamber-axial turbine combined system," Energy, Elsevier, vol. 278(PA).
    4. Zhang, Qibin & Wang, Ke & Dong, Rongxiao & Fan, Wei & Lu, Wei & Wang, Yongjia, 2019. "Experimental research on propulsive performance of the pulse detonation rocket engine with a fluidic nozzle," Energy, Elsevier, vol. 166(C), pages 1267-1275.
    5. Peng, Hao-Yang & Liu, Wei-Dong & Liu, Shi-Jie & Zhang, Hai-Long & Jiang, Lu-Xin, 2020. "Hydrogen-air, ethylene-air, and methane-air continuous rotating detonation in the hollow chamber," Energy, Elsevier, vol. 211(C).
    6. Wang, Ke & Wang, Zhicheng & Zhao, Minghao & Sun, Tianyu & Tan, Fengguang & Zhu, Yiyuan & Lu, Wei & Yu, Xiaodong & Sha, Yu & Fan, Wei, 2019. "Study on the valveless and purgeless scheme to produce high frequency detonations in a long duration," Energy, Elsevier, vol. 189(C).
    7. Saadia Afridi & Tariq Amin Khan & Syed Irtiza Ali Shah & Taimur Ali Shams & Khawar Mohiuddin & David John Kukulka, 2023. "Techniques of Fluidic Thrust Vectoring in Jet Engine Nozzles: A Review," Energies, MDPI, vol. 16(15), pages 1-33, July.
    8. Huang, Si-Yuan & Zhou, Jin & Liu, Shi-Jie & Peng, Hao-Yang & Yuan, Xue-Qiang, 2022. "Continuous rotating detonation engine fueled by ammonia," Energy, Elsevier, vol. 252(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:264:y:2023:i:c:s0360544222030560. 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.