超声速流体振荡器流动特性数值研究
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  • 英文篇名:Numerical Study of Flow Characteristic in Wall-Attachment Fluidic Oscillator
  • 作者:雷晗 ; 单勇 ; 谭晓茗 ; 张靖周
  • 英文作者:LEI Han;SHAN Yong;TAN Xiaoming;ZHANG Jingzhou;Aero-engine Thermal Environment and Structure Key Laboratory of Ministry of Industry and Information Technology,College of Energy and Dynamics,Nanjing University of Aeronautics and Astronautics;
  • 关键词:超声速流体振荡器 ; 延迟时间 ; 振荡周期 ; 起振机制 ; 参数影响
  • 英文关键词:supersonic fluidic oscillator;;delay time;;oscillation period;;oscillation mechanism;;influence of characteristic parameters
  • 中文刊名:CGGL
  • 英文刊名:Journal of Chongqing University of Technology(Natural Science)
  • 机构:南京航空航天大学能源与动力学院航空发动机热环境与热结构工业和信息化部重点实验室;
  • 出版日期:2019-03-15
  • 出版单位:重庆理工大学学报(自然科学)
  • 年:2019
  • 期:v.33;No.400
  • 基金:国家自然科学基金资助项目(U1508212)
  • 语种:中文;
  • 页:CGGL201903018
  • 页数:7
  • CN:03
  • ISSN:50-1205/T
  • 分类号:132-138
摘要
通过改变流体振荡器喷嘴宽度、喉道宽度,对某种结构的超声速流体振荡器进行二维非稳态数值模拟。计算结果表明:当喷嘴宽度远小于混合腔入口宽度时,振荡器的延迟时间t0随着喉道宽度的增加而减小;当喷嘴宽度接近混合腔入口宽度时,延迟时间t0随喉道宽度改变的变化不明显;当保持喷嘴宽度不变时,振荡周期随着喉道宽度的增大而逐渐减小,但减小幅度越来越小;存在一个临界喉道宽度值,一旦超过这个临界值,超声速流体振荡器不能起振。
        The numerical simulation of supersonic fluidic oscillator is carried out by changing the width of nozzle and throat. The results show that the delay time of the oscillator decreases with the increase of the throat width when the nozzle width is much smaller than the inlet width of mixing chamber,and there is no significant change of the delay time with increasing the throat width when the nozzle width is close to the inlet width of mixing chamber. the oscillation period decreases as the throat width increases under constant nozzle width. The oscillator cannot form oscillation jet when the throat width exceeds critical value.
引文
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