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AN EXPERIMENTAL INVESTIGATION OF AN UNDEREXPANDED RECTANGULAR JET EJECTOR.

机译:展开不足的矩形射流喷射器的实验研究。

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摘要

An experimental investigation was carried out on a rectangular ejector (constant area mixing duct) with an underexpanded rectangular jet as the primary flow. The purpose of this investigation is to study the mixing behavior of the ejector flow in general and to identify the effects of the screech tones on the mixing and performance of the ejector in particular. The quantities measured include frequency and amplitude of the screech tone, surface pressure on the ejector duct wall, and the mean flow velocity at the ejector exit in the two central planes of the primary jet. Schlieren flow visualization was made in the plane containing the short dimension of the primary nozzle.; It has been found that the screech tone frequency of the ejector depends not only on the primary jet pressure ratio but also on the ejector duct width. The variations of the screech tone frequency with both the pressure ratio and the duct width show staging behavior. For a given duct width, each screech tone stage matches with one of the transverse modes of the duct. The ejector performance, as determined from the static pressure distribution on the walls, shows irregular variation with pressure ratio; and it is found to be related to the screech tone stages. A better performance was found to lie within one screech tone stage. During this stage the primary jet has a larger spreading rate. As a result, a better mixing is achieved between the primary and secondary streams. For all the ejector duct widths tested, the screech tone stage during which the flow is well mixed corresponds to a Strouhal number of about 0.13, which agrees with the most unstable Strouhal number of the free underexpanded rectangular jet. By incorporating a phase-locked technique with schlieren flow visualization, standing waves excited by the screech tones inside the ejector mixing duct were photographed.
机译:在矩形喷射器(恒定面积混合管道)上进行了实验研究,矩形喷射器的膨胀不足为主流。这项研究的目的是一般研究喷射器流的混合行为,并确定刺耳的声音对喷射器的混合和性能的影响。测得的量包括刺耳声的频率和幅度,喷射器导管壁上的表面压力以及在主喷射器两个中心平面中喷射器出口处的平均流速。在包含主喷嘴短尺寸的平面上进行了Schlieren流动可视化。已经发现,喷射器的刺耳声频率不仅取决于初级喷射压力比,还取决于喷射器导管的宽度。尖叫声频率随压力比和风管宽度的变化表现出阶段性。对于给定的风管宽度,每个尖叫声阶段与风管的横向模式之一匹配。由壁上的静压力分布确定的喷射器性能显示出压力比的不规则变化;并发现它与尖叫声阶段有关。发现更好的性能在于一个尖锐的音调阶段。在此阶段,初级射流具有较大的扩散速率。结果,在一级和二级流之间实现了更好的混合。对于所有测试的喷射器管道宽度,在良好混合期间的刺耳声阶对应于约0.13的斯托洛哈尔数,这与自由膨胀不足的矩形射流中最不稳定的斯托洛哈尔数一致。通过将锁相技术与schlieren流动可视化相结合,可以对由喷射器混合管道内部的尖叫声激发的驻波进行拍照。

著录项

  • 作者

    HSIA, YEU-CHUAN.;

  • 作者单位

    Stanford University.;

  • 授予单位 Stanford University.;
  • 学科 Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 1984
  • 页码 125 p.
  • 总页数 125
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索;
  • 关键词

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