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Large eddy simulation of combustion instability in a tripropellant air heater

机译:三环空气加热器中燃烧不稳定性的大涡模拟

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摘要

This research is motivated by the issue associated with high frequency combustion instability. Large eddy simulation was performed to investigate spontaneous combustion instability in an air/LO2/C2H5OH tri-propellant air heater. The simulation predicts self-excited transverse oscillations. Overall behavior of combustion instability including pressure time histories, mode shapes, Rayleigh index and unsteady response of the injector were studied in detail. Special emphasis was given to the flame behavior, droplet trajectories, pressure evolutions, and formation of large-scale vortical structures during combustion instability in present air heater. Furthermore, in contrast to previous investigations, a new process is identified in the simulation that may feed energy into the acoustic mode and drive combustion instability. (C) 2016 IAA. Published by Elsevier Ltd. All rights reserved.
机译:这项研究的动机是与高频燃烧不稳定性有关的问题。进行了大涡模拟,以研究空气/ LO2 / C2H5OH三推进剂空气加热器中的自燃不稳定性。该模拟预测了自激横向振荡。详细研究了燃烧不稳定性的整体行为,包括压力时间历史,模式形状,瑞利指数和喷油器的不稳定响应。在当前空气加热器的燃烧不稳定性期间,特别强调了火焰行为,液滴轨迹,压力演变以及大规模旋涡结构的形成。此外,与以前的研究相反,在模拟中确定了一个新过程,该过程可能会将能量输入到声波模式中,并导致燃烧不稳定。 (C)2016 IAA。由Elsevier Ltd.出版。保留所有权利。

著录项

  • 来源
    《Acta astronautica》 |2016年第12期|59-73|共15页
  • 作者

    Yuan Lei; Shen Chibing;

  • 作者单位

    Natl Univ Def Technol, Sci & Technol Scramjet Lab, Changsha 410073, Hunan, Peoples R China|Natl Univ Def Technol, Coll Aerosp Sci & Engn, Changsha 410073, Hunan, Peoples R China;

    Natl Univ Def Technol, Sci & Technol Scramjet Lab, Changsha 410073, Hunan, Peoples R China|Natl Univ Def Technol, Coll Aerosp Sci & Engn, Changsha 410073, Hunan, Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Combustion instability; Sustaining mechanisms; Flame dynamics; Numerical simulation; Air heater;

    机译:燃烧不稳定性;维持机理;火焰动力学;数值模拟;空气加热器;
  • 入库时间 2022-08-18 02:28:56

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