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Simultaneous Measurements of Temperature and Major Species Concentration in a Hydrocarbon-Fueled Dual Mode Scramjet Using WIDECARS.

机译:使用WIDECARS同时测量碳氢化合物燃料双模超燃冲压发动机中的温度和主要物种浓度。

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摘要

Width increased dual-pump enhanced coherent anti-Stokes Raman spectroscopy (WIDECARS) measurements were conducted in a McKenna air-ethylene premixed burner, at nominal equivalence ratio range between 0.55 and 2.50 to provide quantitative measurements of six major combustion species (C2H 4, N2, O2, H2, CO, CO2) concentration and temperature simultaneously. The purpose of this test was to investigate the uncertainties in the experimental and spectral modeling methods in preparation for an subsequent scramjet C2H4/air combustion test at the University of Virginia-Aerospace Research Laboratory. A broadband Pyrromethene (PM) PM597 and PM650 dye laser mixture and optical cavity were studied and optimized to excite the Raman shift of all the target species. Two hundred single shot recorded spectra were processed, theoretically fitted and then compared to computational models, to verify where chemical equilibrium or adiabatic condition occurred, providing experimental flame location and formation, species concentrations, temperature, and heat losses inputs to computational kinetic models. The Stark effect, temperature, and concentration errors are discussed. Subsequently, WIDECARS measurements of a premixed air-ethylene flame were successfully acquired in a direct connect small-scale dual-mode scramjet combustor, at University of Virginia Supersonic Combustion Facility (UVaSCF). A nominal Mach 5 flight condition was simulated (stagnation pressure p0 = 300 kPa, temperature T0 = 1200 K, equivalence ratio range ER = 0.3 -- 0.4). The purpose of this test was to provide quantitative measurements of the six major combustion species concentration and temperature. Point-wise measurements were taken by mapping four two-dimensional orthogonal planes (before, within, and two planes after the cavity flame holder) with respect to the combustor freestream direction. Two hundred single shot recorded spectra were processed and theoretically fitted. Mean flow and standard deviation are provided for each investigated case. Within the flame limits tested, WIDECARS data were analyzed and compared with CFD simulations and OH-PLIF measurements.
机译:在McKenna空气-乙烯预混燃烧器中进行宽度增加的双泵增强相干抗斯托克斯拉曼光谱(WIDECARS)测量,标称当量比范围为0.55至2.50,以定量测量六种主要燃烧物质(C2H 4,N2 ,O2,H2,CO,CO2)浓度和温度同时显示。该测试的目的是调查实验和光谱建模方法中的不确定性,以便为随后的弗吉尼亚大学航空研究实验室的超燃冲压空气C2H4 /空气燃烧测试做准备。研究并优化了宽带吡咯二烯(PM)PM597和PM650染料激光混合物以及光学腔,以激发所有目标物种的拉曼位移。处理了200个单发记录的光谱,进行了理论拟合,然后与计算模型进行了比较,以验证发生化学平衡或绝热条件的位置,从而为计算动力学模型提供了实验火焰位置和形成,物种浓度,温度和热损失的输入。讨论了斯塔克效应,温度和浓度误差。随后,在弗吉尼亚大学超音速燃烧设施(UVaSCF)的直接连接小型双模超燃冲压燃烧器中成功获取了预混空气乙烯火焰的WIDECARS测量值。模拟了标称5马赫飞行条件(停滞压力p0 = 300 kPa,温度T0 = 1200 K,当量比范围ER = 0.3-0.4)。该测试的目的是对六种主要燃烧物质的浓度和温度进行定量测量。通过相对于燃烧器自由流方向映射四个二维正交平面(腔火焰保持器之前,之内和之后的两个平面)进行逐点测量。对200张单发记录的光谱进行了处理并进行了理论拟合。为每个调查案例提供了平均流量和标准偏差。在测试的火焰极限内,分析了WIDECARS数据,并将其与CFD模拟和OH-PLIF测量进行了比较。

著录项

  • 作者单位

    The George Washington University.;

  • 授予单位 The George Washington University.;
  • 学科 Aerospace engineering.;Mechanical engineering.;Optics.
  • 学位 Ph.D.
  • 年度 2016
  • 页码 138 p.
  • 总页数 138
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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