Volume 37 Issue 1
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LIU Jing, HU Erjiang, HUANG Zuohua, ZENG Wen. Experiment and numerical calculation on low-temperature oxidation characteristics of RP-3 aviation kerosene[J]. Journal of Aerospace Power, 2022, 37(1): 36-45. doi: 10.13224/j.cnki.jasp.20210074
Citation: LIU Jing, HU Erjiang, HUANG Zuohua, ZENG Wen. Experiment and numerical calculation on low-temperature oxidation characteristics of RP-3 aviation kerosene[J]. Journal of Aerospace Power, 2022, 37(1): 36-45. doi: 10.13224/j.cnki.jasp.20210074
shu

Experiment and numerical calculation on low-temperature oxidation characteristics of RP-3 aviation kerosene

doi: 10.13224/j.cnki.jasp.20210074
  • 1.

    State Key Laboratory of Multiphase Flow in Power Engineering，School of Energy and Power Engineering， Xi'an Jiaotong University，Xi'an 710049，China

  • 2.

    Key Laboratory of Advanced Measurement and Test Technique for Aviation Propulsion System，Liaoning Province，School of Aero-engine， Shenyang Aerospace University，Shenyang 110136，China

  • Received Date: 2021-02-18
  • Publish Date: 2022-01-28
    Abstract
  • The low-temperature oxidation of RP-3 aviation kerosene and its surrogate fuel （n-decane （mole fraction of 0.14）/n-dodecane （0.1）/iso-cetane （0.3）/methylcyclohexane（0.36）/toluene （0.1）），were experimentally tested in a jet stirring reactor （JSR） at the conditions of the pressure of 0.1 MPa，the temperature range of 550-1 100 K，the equivalence ratios of 0.5 and 1.0，and the residence time of 2 s.Meanwhile，through the reaction class-based global sensitivity analysis，decoupling methodology and multi-objective genetic algorithm，the reduced reaction kinetic mechanism of the surrogate fuel （including 181 species and 872 reactions） was established，and the low- temperature oxidation characteristics of the surrogate fuel were simulated.The results showed that the temperature-dependent trends of the mole fractions of main species in the low-temperature oxidation process of the surrogate fuel were in good agreement with RP-3 aviation kerosene.The reduced reaction mechanism of the surrogate fuel for RP-3 aviation kerosene had a good prediction of the temperature-dependent trends of the mole fractions of main species during the low-temperature oxidation of the surrogate fuel.However，there were still some deviations in the prediction of the peak mole fractions and negative temperature coefficient （NTC） effect of some species.

     

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