首页 | 本学科首页   官方微博 | 高级检索  
     

多孔喷管降低引射喷管噪声的实验研究
引用本文:方人淞,张荣学. 多孔喷管降低引射喷管噪声的实验研究[J]. 航空动力学报, 1988, 3(2): 145-148,188
作者姓名:方人淞  张荣学
作者单位:南京航空学院(方人淞),南京航空学院(张荣学)
摘    要:以多孔喷管代替普通收缩喷管或收-扩喷管作为引射喷管系统的主喷管,进行模型实验,结果表明,这种构型引射喷管不仅能显著降低噪声,而且具有良好的气动性能。

收稿时间:1987-01-01

REDUCTION OF EJECTOR NOISE WITH MULTIHOLE NOZZLE
Fang Rensong and Zhang Rongxue. REDUCTION OF EJECTOR NOISE WITH MULTIHOLE NOZZLE[J]. Journal of Aerospace Power, 1988, 3(2): 145-148,188
Authors:Fang Rensong and Zhang Rongxue
Affiliation:Nanjing Aeronautics Institute;Nanjing Aeronautics Institute
Abstract:In order to reduce the noise, an ejector with multihole nozzle is proposed as the primary nozzle, and its design method is presented. For comparison of the aerodynamic performance and the noise characteristics with those of conventional one in subsonic and supersonic ejector systems, the sound power levels and the primary and secondary mass flow rates of the ejectors were measured, and the static thrusts of the ejectors were estimated, based on the measured mass flow rates. The shroud length of the ejector system tested was altered in the experiments so as to study the effect of this parameter on noise and thrust. The exper imental results show that the multihole nozzle ejector system not only reduces noise considerably but also gains better aerodynamic performance due to a shorter shroud. The shorter the shroud, the more noise reduction and greater the static thrust increment can be achieved. For subsonic ejector, the noise reduction is about 14dB and the static thrust increment is about 30% when ratio of shroud length is 7.6. For supersonic ejector, those are about 22dB and 35% respectively when the shroud length ratio is 9.6.
Keywords:
本文献已被 CNKI 等数据库收录!
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号