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An experimental investigation of the aeroacoustic properties of high-speed, helium/air mixture axisymmetric jets.

机译:高速氦/空气混合轴对称射流的空气声学特性的实验研究。

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摘要

The acoustic and aerodynamic properties of high-speed axisymmetric jets are investigated experimentally in a recently refurbished high-speed jet noise facility. Mach numbers from 0.5 to 1.5 are tested with an emphasis on Mach 0.9 and 1.5 jets. Reynolds numbers for the current study range from approximately 200,000 to 600,000. The properties of heated jets which are important in aeroacoustic studies, namely low density and high velocity, are simulated in the current study by adding helium to the jet flow. In addition, an optical deflectometry system is used to provide unique two-point space-time correlation measurements within the jet shear layer.; A combination of acoustic, mean flow, and optical deflectometry measurements are made for both pure air and helium/air mixture jets at various helium concentrations. Far-field acoustic measurements indicate very reasonable agreement between previously measured heated jet directivity patterns and those at simulated temperature ratios using helium/air mixture jets. The addition of helium also shows strong similarities to the addition of heat in the mean velocity profile measurements. A shortening of the potential core and a slight decrease in jet spreading rate are observed with helium addition—the same trends observed for heated jets. Optical deflectometry measurements near the end of the potential core along the jet lip line exhibit distinct cross-correlation curves for the pure air jet cases. However, helium/air mixture jets display much lower levels of correlation and little evidence of large-scale structure in the measured spectra. It is believed the strong visual density gradients throughout the shear layer effectively mask the large-scale structure, thus reflecting a limitation of the optical deflectometer. Finally, a decrease in normalized convection velocity with simulated heating (helium addition) is observed.
机译:在最近翻新的高速喷气噪声设备中,对高速轴对称喷气的声学和空气动力学特性进行了实验研究。测试了从0.5到1.5的马赫数,重点是0.9和1.5马赫的射流。当前研究的雷诺数范围从大约200,000到600,000。在当前的研究中,通过在射流中添加氦气来模拟在空气声学研究中很重要的加热射流的特性,即低密度和高速度。另外,光学偏转测量系统用于在射流剪切层内提供独特的两点时空相关性测量。对纯空气和各种氦气浓度下的氦气/空气混合射流进行了声学,平均流量和光学偏转测量的组合。远场声学测量表明,先前测量的加热射流方向图与使用氦气/空气混合射流在模拟温度比下得到的方向图之间非常合理的一致性。在平均速度曲线测量中,氦的添加与热量的添加也显示出强烈的相似性。加入氦气可以观察到潜在核心的缩短和射流扩散速率的略微下降,这与加热射流的趋势相同。对于纯空气射流情况,沿着射流唇线的潜在磁芯末端附近的光学折光法测量显示出明显的互相关曲线。但是,氦气/空气混合射流显示出低得多的相关性,并且在被测光谱中几乎没有大规模结构的证据。可以相信,整个剪切层的强视觉密度梯度有效地掩盖了大规模结构,从而反映了光学偏转仪的局限性。最后,观察到模拟对流(添加氦气)的标准化对流速度降低。

著录项

  • 作者

    Doty, Michael Justin.;

  • 作者单位

    The Pennsylvania State University.;

  • 授予单位 The Pennsylvania State University.;
  • 学科 Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 2002
  • 页码 232 p.
  • 总页数 232
  • 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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