• Title/Summary/Keyword: Multi-step Quasi-gloabl Reaction

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Numerical Study on the Effect Recess on the Turbulent Combustion of Kerosene/LOx Coaxial Rocket Injector (케로신-산소 로켓 동축 분사기 난류 연소에서 리세스의 영향에 대한 수치해석)

  • Choi, Jeong-Yeol;Shin, Jae-Ryul
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.11a
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    • pp.92-95
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    • 2011
  • A multi-step quasi-global mechanism is developed for the kerosene/oxygen combustion analysis including dissociation products. Reaction constants of the global reaction are determined to have agreement with experimental data. The mechanism is used for the numerical analysis of the combustion flow field of the kerosene/oxygen shear coaxial injector. The results from high-resolution numerical analysis confirmed qualitatively that the recess enhance the fuel/air mixing and combustion efficiency by the increased flow instabilities.

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Numerical Analysis of Turbulent Combustion of a Kerosene/Oxygen Coaxial Injector with a Recess (리세스가 있는 케로신/산소 동축 분사기의 난류 연소 유동 해석)

  • Choi, Jeong-Yeol;Shin, Jae-Ryul
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.04a
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    • pp.77-78
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    • 2011
  • A multi-step quasi-global mechanism is developed for the kerosene/oxygen combustion analysis including dissociation products. Reaction constants of the global reaction are determined to have agreement with experimental data. The mechanism is used for the numerical analysis of the combustion flow field of the kerosene/oxygen shear coaxial injector. The results from high-resolution numerical analysis confirmed qualitatively that the recess enhance the fuel/air mixing and combustion efficiency by the increased flow instabilities.

  • PDF