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Measurement of the vapor-phase and liquid-phase fuel distributions downstream of an integrated flameholder in heated stream

机译:在加热物流中的综合炭持有者下游的气相和液相燃料分布的测量

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摘要

Understanding the vapor-phase and liquid-phase fuel distributions are necessary for conducting combustion performance research, especially under high-temperature inflow or fuel conditions. In this study, we propose physical and optical quantitative methods for measuring the total fuel distribution in the dual-modal (after-burner/ramjet) combustor with an integrated flameholder. The vapor-phase equivalence ratio is deduced from the n-decane (C10H22) concentration (determined using an n-decane detector). Raw images of the fuel spray field are captured using a high-speed camera. The droplets Sauter mean diameter (SMD) can be obtained using an image processing technology. The liquid-phase equivalence ratio is further derived by analyzing the droplet size and distribution. Finally, the total equivalence ratio can be obtained by adding the equivalence ratios of the vapor and liquid phases. The vapor-phase and liquid-phase fuel distributions were measured on different cross-sections downstream of an integrated flameholder. The global equivalence ratio, inflow velocity, inflow temperature, and fuel temperature were set to empty set=0.3-0.6, V-1 = 50m/s, T-1 = 450K, and T-f = 373K, respectively. Further, the vapor- and liquid-phase equivalence ratios for the measurement points increased and decreased, respectively, with increasing flow distance. The flow characteristics and the vapor-phase fuel distribution were consistent behind the flameholder, confirming the rationality of deducing the vapor-phase fuel concentration from the n-decane concentration. The maximum error of the SMD obtained using the image processing technology was lower than the value reported in the literature (5.1%). Finally, the total equivalence ratio was almost conserved along the flow distance, proving the credibility of the proposed measurement methods.
机译:理解气相和液相燃料分布对于进行燃烧性能研究是必要的,特别是在高温流入或燃料条件下。在这项研究中,我们提出了用于测量与集成耐壳的双模(后燃烧器/拉姆喷射)燃烧器中的总燃料分布的物理和光学定量方法。从N-癸烷(C10H22)浓度(使用N-癸烷检测器测定)推导出气相等效率。使用高速相机捕获燃料喷射场的原始图像。可以使用图像处理技术获得液滴制冷器平均直径(SMD)。通过分析液滴尺寸和分布,进一步推导出液相等效率。最后,通过添加蒸汽和液相的等效比来获得总等值比。在整合炭持有人下游的不同横截面上测量气相和液相燃料分布。全局等效率,流入速度,流入温度和燃料温度分别设定为空设定= 0.3-0.6,V-1 = 50m / s,T-1 = 450K,以及T-F = 373k。此外,测量点的气相和液相等效比分别增加和减少,流量距离增加。流动特性和气相燃料分布均一致地在剥夺者后面,确认从N-癸烷浓度推导出蒸汽相燃料浓度的合理性。使用图像处理技术获得的SMD的最大误差低于文献中报告的值(5.1%)。最后,总等价率几乎沿流量距离保守,证明了所提出的测量方法的可信度。

著录项

  • 来源
    《Fuel 》 |2019年第1期| 115808.1-115808.11| 共11页
  • 作者单位

    Nanjing Univ Aeronaut & Astronaut Coll Energy & Power Engn Nanjing 210016 Jiangsu Peoples R China;

    Nanjing Univ Aeronaut & Astronaut Coll Energy & Power Engn Nanjing 210016 Jiangsu Peoples R China;

    Nanjing Univ Aeronaut & Astronaut Coll Energy & Power Engn Nanjing 210016 Jiangsu 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

    Physical method; Optical method; Vapor-phase fuel; Liquid-phase fuel; Equivalence ratio; Sauter mean diameter (SMD);

    机译:物理方法;光学方法;气相燃料;液相燃料;等效率;燃烧器平均直径(SMD);

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