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An experimental investigation of ionization of supersonic air by a corona discharge.

机译:电晕放电使超音速空气电离的实验研究。

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摘要

A technique is developed to ionize supersonic air flow in a shock tube by a weak corona discharge. The driven section of the tube is open to the atmosphere. The shock propagates in the driven section at about 1 km/s by means of an area contraction near the downstream end of the driven section. Air is ionized by a unipolar corona discharge device comprising of a sharp-edged wedge as a high-field electrode inserted in a 41.25 mm (2") ID tube that forms a low-field electrode. The device requires less than 0.5 W. A ring probe, downstream of the corona discharge device, collects charges (ions and electrons) from the air; its output voltage is thus a measure of the degree of ionization. The degree of ionization is varied by varying the corona discharge voltage and the flow speed.; Corona generation was initially demonstrated with bench tests. These indicated an increased degree of ionization with an air flow created by a fan, relative to that in static air. Tests in a shock tube, with subsonic and supersonic air flow, and with a negative corona, provided results with the same ionization behavior. The operating range of discharge voltages is relatively small for a positive corona; hence, shock tube tests were confined to a negative corona.; Shock tube test results indicate that, on a 10 millisecond time scale, corona generated ionization was convected downstream to the probe location in a supersonic flow. An anomalous shock tube result is a probe signal, without a corona discharge, that is similar, but weaker, to the signal with a discharge.; Although the tests were done with shock speeds up to about 1 km/s and with atmospheric air ahead of shock wave, the technique of ionization and plasma measurement can be extended to higher speeds and lower pressures. It is also suggested that a supersonic wind tunnel with a Langmuir probe be used for this type of work.
机译:通过弱电晕放电,开发了一种技术使电击管中的超声波气流电离。管的从动部分通向大气。震动通过从动部分下游端附近的区域收缩以大约1 km / s的速度在从动部分传播。空气由单极电晕放电设备电离,该设备包括一个尖锐的楔形作为高场电极,插入到形成低场电极的41.25毫米(2英寸)内径管中。该设备的功率小于0.5W。环形探针位于电晕放电装置的下游,可从空气中收集电荷(离子和电子),因此其输出电压是电离度的量度,通过改变电晕放电电压和流速可改变电离度。;最初通过台架试验证明了电晕的产生,这表明风扇产生的空气流相对于静态空气具有更高的电离度,在冲击管中进行亚音速和超音速空气流测试,负电晕,提供与电离行为相同的结果;对于正电晕,放电电压的工作范围相对较小;因此,冲击管测试仅限于负电晕;冲击管测试结果表明,在10毫秒的时间范围内,电晕产生的电离在超音速流中在探头位置的下游对流。冲击管的异常结果是没有电晕放电的探测信号,与带有放电的信号相似但较弱。尽管测试是在高达1 km / s的冲击速度下进行的,并且大气在冲击波之前进行,但是电离和等离子体测量技术可以扩展到更高的速度和更低的压力。还建议将带有Langmuir探头的超音速风洞用于此类工作。

著录项

  • 作者

    Satyanand, Udyavar S.;

  • 作者单位

    The University of Texas at Arlington.;

  • 授予单位 The University of Texas at Arlington.;
  • 学科 Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 2005
  • 页码 96 p.
  • 总页数 96
  • 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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