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Internal flow dynamics and performance of pulse detonation engine with alternative fuels

Author

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  • Warimani, Mahammadsalman
  • Azami, Muhammad Hanafi
  • Khan, Sher Afghan
  • Ismail, Ahmad Faris
  • Saharin, Sanisah
  • Ariffin, Ahmad Kamal

Abstract

In this study, analytical and computational analysis is performed to determine the effect of thermodynamic detonation parameters on the performance of the pulse detonation engine. For analytical study along with pure fuels blend of hydrogen (50 %) + kerosene (50 %), hydrogen (50 %) + methane (50 %) and methane (50 %) + kerosene (50 %) are considered. The ANSYS FLUENT program is utilized two-dimensional computational fluid dynamics (CFD) simulation using a stoichiometric mixture of three pure fuels: hydrogen-air, methane-air, and kerosene-air. Time-dependent numerical simulations are used to explore the flow condition inside the detonation tube. Excellent performance is observed for hydrogen-air fuel. Hydrogen shows the highest velocity of 2524.36 m/s and a specific impulse of 6842.16 s. The lowest velocity and specific impulse are produced by kerosene of 1520 m/s and 1473.6 s, respectively. It is shown that measured parameters could vary significantly depending on the choice of fuels used. The results infer that hydrogen blends of methane and kerosene fuels are also suitable for pulse detonation engine (PDE) application. Finally, these analytical and simulated results are validated with the previously published literature and NASA CEA (national aeronautics and space administration -chemical equilibrium with applications).

Suggested Citation

  • 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).
    • Handle: RePEc:eee:energy:v:237:y:2021:i:c:s0360544221019678
    DOI: 10.1016/j.energy.2021.121719
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    References listed on IDEAS

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    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. Ekici, Selcuk, 2020. "Thermodynamic mapping of A321-200 in terms of performance parameters, sustainability indicators and thermo-ecological performance at various flight phases," Energy, Elsevier, vol. 202(C).
    4. Ekici, Selcuk, 2020. "Investigating routes performance of flight profile generated based on the off-design point: Elaboration of commercial aircraft-engine pairing," Energy, Elsevier, vol. 193(C).
    5. Ranasinghe, Kavindu & Guan, Kai & Gardi, Alessandro & Sabatini, Roberto, 2019. "Review of advanced low-emission technologies for sustainable aviation," Energy, Elsevier, vol. 188(C).
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    1. 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).

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