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Experimental research on propulsive performance of the pulse detonation rocket engine with a fluidic nozzle

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  • Zhang, Qibin
  • Wang, Ke
  • Dong, Rongxiao
  • Fan, Wei
  • Lu, Wei
  • Wang, Yongjia

Abstract

To explore an effective way for the nozzle design of a pulse detonation rocket engine (PDRE), theoretical and experimental researches have been carried out. The exhaust process and optimal converging/diverging area ratios of a nozzle were theoretically analyzed. Pressure and velocity fluctuations of the exhaust flow were considered to be the major issues. A fluidic solution which employs nitrogen flows in the nozzle throat and divergent section has been tested. The fluidic nozzle is able to adjust the effective area ratios according to the incoming flow. The effective convergent area ratio varied from 2.0 to 2.2, and the divergent one varied from 5.0 to 1.8. It is proved that the fluidic nozzle effectively improved the propulsive performance of the engine. A maximum average thrust increase of 137.8% was obtained in proper conditions.

Suggested Citation

  • 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.
    • Handle: RePEc:eee:energy:v:166:y:2019:i:c:p:1267-1275
    DOI: 10.1016/j.energy.2018.10.165
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    References listed on IDEAS

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    1. 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.
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    6. 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.
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    Cited by:

    1. 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).
    2. 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).
    3. 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.

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