...
首页> 外文期刊>Journal of Fluid Mechanics >Intermittent modal coupling in screeching underexpanded circular twin jets
【24h】

Intermittent modal coupling in screeching underexpanded circular twin jets

机译:尖叫的舌下圆形双喷头间歇模态耦合

获取原文
获取原文并翻译 | 示例
   

获取外文期刊封面封底 >>

       

摘要

In this article the erratic coupling that can occur in screeching supersonic twin jets is characterised. Non-stationary acoustic analysis is used to investigate the temporal behaviour of the coupling phenomena. The results show that where the phase between the jets is time varying, the screech tone experiences interruptions. The interruptions are either correlated and experienced by both jets or are anti-correlated and only by one. During the anti-correlated interruption, the uninterrupted jet screeches as an isolated jet. The instantaneous velocity field shows that for the majority of snapshots during an acoustic interruption, the jets do not exhibit a coupled oscillation. When the jets are uninterrupted, they are oscillating in either a coupled symmetric or anti-symmetric mode. This behaviour manifests at a condition between two operating points characterised by different coupling modes. It suggests the interruptions arise due to a competition between two global modes of the flow. Despite the existence of multiple acoustic tones in the region where these modes are competing, analysis of the individual jets reveals energetic structures with only a single wavelength. It is found that jets whose own oscillation is characterised by a single wavelength can, through coupling either symmetrically or anti-symmetrically about their symmetry plane, produce different acoustic tones. These findings are consistent across three experimental facilities. The observed modes are a function of the jet spacing and nozzle pressure, therefore future studies investigating other spacings must recharacterise the encountered coupled modes. This article provides the signatures to characterise the behaviour for future studies.
机译:本文描述了在刺耳的超音速双射流中可能发生的不稳定耦合。非平稳声学分析用于研究耦合现象的时间行为。结果表明,当喷流之间的相位随时间变化时,尖叫声会受到干扰。中断要么是相关的,并由两个射流经历,要么是反相关的,仅由一个射流经历。在反相关中断期间,不间断喷流作为隔离喷流尖叫。瞬时速度场表明,对于声中断期间的大多数快照,射流不表现出耦合振荡。当射流不间断时,它们以耦合对称或反对称模式振荡。这种行为表现在以不同耦合模式为特征的两个工作点之间。这表明,中断是由于两种全球流动模式之间的竞争造成的。尽管在这些模式相互竞争的区域存在多个声调,但对单个喷流的分析揭示了只有单一波长的能量结构。研究发现,以单波长振荡为特征的射流,通过对称或反对称耦合,可以产生不同的声调。这些发现在三个实验设施中是一致的。观测到的模式是射流间距和喷嘴压力的函数,因此,未来研究其他间距必须重新描述遇到的耦合模式。这篇文章为将来的研究提供了表征行为的特征。

著录项

  • 来源
    《Journal of Fluid Mechanics》 |2021年第1期|共39页
  • 作者单位

    Monash Univ Dept Mech &

    Aerosp Engn Lab Turbulence Res Aerosp &

    Combust Melbourne Vic 3800 Australia;

    Ohio State Univ Gas Dynam &

    Turbulence Lab Aerosp Res Ctr Dept Mech &

    Aerosp Engn Columbus OH 43235 USA;

    Ohio State Univ Gas Dynam &

    Turbulence Lab Aerosp Res Ctr Dept Mech &

    Aerosp Engn Columbus OH 43235 USA;

    Monash Univ Dept Mech &

    Aerosp Engn Lab Turbulence Res Aerosp &

    Combust Melbourne Vic 3800 Australia;

    Monash Univ Dept Mech &

    Aerosp Engn Lab Turbulence Res Aerosp &

    Combust Melbourne Vic 3800 Australia;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 流体力学;
  • 关键词

    jet noise; aeroacoustics;

    机译:喷射噪音;航空声;

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号