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On the prediction of spray angle of liquid-liquid pintle injectors

机译:液-液枢轴注射器喷射角的预测

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摘要

The pintle injector is famous for its capability of deep throttling and low cost. However, the pintle injector has been seldom investigated. To get a good prediction of the spray angle of liquid-liquid pintle injectors, theoretical analysis, numerical simulations and experiments were conducted. Under the hypothesis of incompressible and inviscid flow, a spray angle formula was deduced from the continuity and momentum equations based on a control volume analysis. The formula was then validated by numerical and experimental data. The results indicates that both geometric and injection parameters affect the total momentum ratio (TMR) and then influence the spray angle formed by liquid-liquid pintle injectors. TMR is the pivotal non-dimensional number that dominates the spray angle. Compared with gas-gas pintle injectors, spray angle formed by liquid-liquid injectors is larger, which benefits from the local high pressure zone near the pintle wall caused by the impingement of radial and axial sheets.
机译:针阀式喷油器以其节流能力强和成本低而闻名。然而,很少对针形注射器进行研究。为了更好地预测液-液枢轴喷射器的喷射角度,进行了理论分析,数值模拟和实验。在不可压缩和无粘性流动的假设下,基于控制量分析,从连续性和动量方程推导了喷射角公式。然后通过数值和实验数据验证了该公式。结果表明,几何参数和喷射参数都会影响总动量比(TMR),然后会影响液-液枢轴喷射器形成的喷雾角度。 TMR是支配喷射角度的关键无量纲数。与气-气针刺喷射器相比,液-液喷射器形成的喷射角更大,这得益于径向和轴向片材的撞击导致针刺壁附近的局部高压区域。

著录项

  • 来源
    《Acta astronautica》 |2017年第9期|145-151|共7页
  • 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;

    AECC, Shenyang Engine Res Inst, Shenyang 110015, Liaoning, Peoples R China;

    CARDC, Airbreathing Hyperson Res Ctr, Mianyang 621000, 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

    Liquid rocket engine; Pintle injector; Spray angle;

    机译:液体火箭发动机;针式喷油器;喷雾角度;

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