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A shock tube study of jet fuel pyrolysis and ignition at elevated pressures and temperatures

机译:在高压和高温下喷气燃料热解和点火的冲击管研究

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摘要

The development of compact HyChem hybrid models for jet fuels requires datasets of pyrolysis product yields to constrain the model and of kinetic targets to evaluate the model. To this end, we have measured selected species time-histories during fuel pyrolysis using laser absorption, and ignition delay times using multiple methods behind reflected shock waves in a heated shock tube. Measurements were performed for three different jet fuels diluted in air or argon over a temperature range of 1000-1400 K, a pressure range of 12-40 atm, and equivalence ratios of 0.5-1. Fuel loading was measured using an IR He-Ne laser at 3391 nm; ethylene with a CO2 gas laser at wavelengths of 10532 nm and 10674 nm; and methane with a tunable diode laser at wavelengths of 3175 nm and 3177 nm. Ignition delay times were measured in three ways: by monitoring fuel removal with laser absorption, by sidewall pressure, and by OH* emission. Particular care was taken in mixture preparation and efficient transfer of the gaseous fuel mixture to the shock tube. The current HyChem model by Wang et al. shows good agreement with these data.
机译:紧凑的航空燃料HyChem混合模型的开发需要热解产物产率的数据集来约束模型,而动力学目标则需要数据集来评估模型。为此,我们已经使用激光吸收测量了燃料热解过程中选定物种的时间历史,并使用了加热冲击管中反射冲击波背后的多种方法来测量了点火延迟时间。对在空气或氩气中稀释的三种不同喷气燃料进行了测量,温度范围为1000-1400 K,压力范围为12-40 atm,当量比为0.5-1。使用IR He-Ne激光在3391 nm处测量燃料负载;乙烯与CO2气体激光器在10532 nm和10674 nm的波长下;甲烷和带有可调二极管激光器的甲烷,波长分别为3175 nm和3177 nm。点火延迟时间以三种方式测量:通过激光吸收监测燃料去除,侧壁压力和OH *排放。在混合物制备和将气态燃料混合物有效转移到激波管方面要格外小心。 Wang等人当前的HyChem模型。与这些数据显示出很好的一致性。

著录项

  • 来源
    《Fuel》 |2018年第15期|338-344|共7页
  • 作者单位

    Stanford Univ, Dept Mech Engn, 418 Panama Mall,Room 104, Stanford, CA 94305 USA;

    Stanford Univ, Dept Mech Engn, 418 Panama Mall,Room 104, Stanford, CA 94305 USA;

    Stanford Univ, Dept Mech Engn, 418 Panama Mall,Room 104, Stanford, CA 94305 USA;

    Stanford Univ, Dept Mech Engn, 418 Panama Mall,Room 104, Stanford, CA 94305 USA;

    Stanford Univ, Dept Mech Engn, 418 Panama Mall,Room 104, Stanford, CA 94305 USA;

  • 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

    Jet fuel; Shock tubes; Laser absorption; Fuel characterization; Hybrid models;

    机译:喷气燃料;激波管;激光吸收;燃料表征;混合模型;
  • 入库时间 2022-08-18 03:53:39

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