首页> 外文学位 >Control of the Turbulent Shear Layer Downstream of a Backward Facing Step using Nanosecond Pulse Driven Surface Plasma Discharges: Effects of Pulse Energy.
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Control of the Turbulent Shear Layer Downstream of a Backward Facing Step using Nanosecond Pulse Driven Surface Plasma Discharges: Effects of Pulse Energy.

机译:使用纳秒级脉冲驱动的表面等离子放电控制向后面向步骤下游的湍流剪切层:脉冲能量的影响。

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摘要

The influence of pulse energy on nanosecond pulse driven dielectric barrier discharge (ns-DBD) plasma actuation applied to the turbulent shear layer downstream of a backward facing step (BFS) is examined experimentally. The ns-DBD control mechanism, which is believed to be primarily thermal in contrast to most other flow control actuators, has been demonstrated in various high speed shear flows yet questions on fundamental physics and scaling remain unanswered. In this work, ns-DBD pulse amplitude is varied between 0.13mJ/cm -- 0.88mJ/cm per pulse in order to understand its effects on the excitation of a turbulent shear layer. This work is carried out at a fixed actuation frequency of 1000Hz which corresponds to Sttheta ≈ 0.005 based on initial momentum thickness. Both mean and phase-averaged data indicate a preference for the 0.33mJ/cm and 0.56mJ/cm pulse amplitudes. However, further analysis concludes that 0.33mJ/cm is the most favorable as seen from momentum thickness growth and TKE distribution. Further analysis through the use of schlieren imaging suggests that depreciating control authority for the highest pulse amplitude of 0.88mJ/cm may be a result of either increased plasma three dimensionality resulting in non-uniform heating, or a thermal saturation mechanism (overheating). Additional theoretical studies are required to substantiate these claims and to decipher between the two.
机译:实验研究了脉冲能量对纳秒脉冲驱动介电势垒放电(ns-DBD)等离子体致动的影响,该等离子体致动作用在向后的台阶(BFS)下游的湍流剪切层上。 ns-DBD控制机构被认为与大多数其他流量控制执行器相比主要是热力的,已在各种高速剪切流中得到了证明,但有关基本物理和定标的问题仍未得到解答。在这项工作中,ns-DBD脉冲幅度在每个脉冲0.13mJ / cm-0.88mJ / cm之间变化,以了解其对湍流剪切层激发的影响。这项工作在对应于Sttheta≈的固定驱动频率1000Hz下进行。基于初始动量厚度为0.005。均值和相位平均数据均表示对0.33mJ / cm和0.56mJ / cm脉冲幅度的偏爱。但是,进一步分析得出的结论是,从动量厚度增长和TKE分布来看,0.33mJ / cm是最有利的。通过使用schlieren成像进行的进一步分析表明,最高脉冲幅度0.88mJ / cm的控制权限下降可能是由于等离子体三维尺寸增加导致不均匀加热,或者是由于热饱和机制(过热)导致的。需要更多的理论研究来证实这些主张并在两者之间进行解读。

著录项

  • 作者

    Akins, David J.;

  • 作者单位

    The University of Arizona.;

  • 授予单位 The University of Arizona.;
  • 学科 Aerospace engineering.
  • 学位 M.S.
  • 年度 2016
  • 页码 50 p.
  • 总页数 50
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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