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Visualization of cavitating and flashing flows within a high aspect ratio injector.

机译:可视化高纵横比进样器中的空化和闪烁流动。

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摘要

Thermal management issues necessitate the use of fuel as a heat sink for gas turbine and liquid rocket engines. There are certain benefits to using heated fuels, namely, increased sensible enthalpy, increased combustion efficiency, a decrease in certain emissions, and enhanced vaporization characteristics. However, the thermal and pressure enviornment inside an injector can result in the fuel flashing to vapor. Depending on the injector design, this can have deleterious effects on engine performance. As interest in heated fuels inreases, it is important to understand what occurs in the flow path of an injector under flashing conditions.;At the High Pressure Laboratory at Purdue University's Maurice J. Zucrow Laboritories, a test rig was designed and built to give visual access into the flow path of a 2-D slot injector. The rig is capable of pressurizing and heating a liquid to superheated conditions and utilizes a pneumatically actuated piston to pusth the liquid through the slot injector. Methanol was chosen as a surrogate fuel to allow for high levels of superheat at relatively low temperatures. Testing was completed with acrylic and quartz injectors of varying L/DH..;Flashing conditions inside the injector flow path were induced via a combination of heating and back pressure adjustments. Volume flow rate, pressure measurements, and temperature measurements were made which allowed the discharge characteristics, the level of superheat, and other parameters to be calculated and compared. To give a basis for comparison the flashing results are compared to the flow through the injector under cavitating conditions. Cavitation and flashing appear to be related phenomena and this relationship is shown. Bubble formation under cavitating or flashing conditions is observed to attenuate the injector's discharge characteristics.;High speed videos of the flow field were also collected. Several flow regimes and flow structures, unique to these regimes, were observed. A frequency analysis was also performed on the video files. Bubble formation in the flow field dominates the frequency spectrum, which is confined below 1 kHz.;The test campaign was successful. The result is a possible way to predict an injector's performance under flashing conditions without running heated fuel through the injector. These results may be applicable to real world injector design and testing.
机译:热管理问题使得必须将燃料用作燃气轮机和液体火箭发动机的散热器。使用加热的燃料有某些好处,即增加了显热焓,增加了燃烧效率,减少了某些排放物并增强了汽化特性。但是,喷油器内部的热和压力环境会导致燃料闪蒸成蒸气。根据喷射器的设计,这可能会对发动机性能产生不利影响。随着对加热燃料的兴趣的增加,重要的是要了解在闪蒸条件下喷油器的流路中会发生什么。进入2-D狭缝注入器的流路。该钻机能够将液体加压并加热到过热状态,并利用气动活塞将液体喷入缝隙喷射器中。选择甲醇作为替代燃料,以在相对较低的温度下实现高水平的过热。测试使用L / DH变化的丙烯酸和石英喷油器完成。喷油器流路内部的闪蒸条件是通过加热和背压调节的组合而引起的。进行体积流量,压力测量和温度测量,以计算和比较排放特性,过热水平和其他参数。为了提供比较的依据,将闪蒸结果与在空化条件下通过喷油器的流量进行了比较。空化和闪烁似乎是相关现象,并且显示出这种关系。在空化或闪蒸条件下观察到气泡形成,从而削弱了喷射器的排放特性。还收集了流场的高速视频。观察到了几种流态和流结构,这是这些流态唯一的。还对视频文件进行了频率分析。流场中气泡的形成主导了频谱,频谱被限制在1 kHz以下。结果是一种可能的方法,可以在不使加热的燃料流过喷油器的情况下,在闪蒸条件下预测喷油器的性能。这些结果可能适用于现实世界中的喷油器设计和测试。

著录项

  • 作者

    Thompson, Andrew S.;

  • 作者单位

    Purdue University.;

  • 授予单位 Purdue University.;
  • 学科 Aerospace engineering.;Mechanical engineering.
  • 学位 Ph.D.
  • 年度 2014
  • 页码 245 p.
  • 总页数 245
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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