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V形槽喷管在分开式排气系统中的降噪实验
引用本文:何敬玉,邵万仁,许影博,李晓东.V形槽喷管在分开式排气系统中的降噪实验[J].航空动力学报,2015,30(2):324-330.
作者姓名:何敬玉  邵万仁  许影博  李晓东
作者单位:1. 北京航空航天大学能源与动力工程学院,北京,100191
2. 北京航空航天大学能源与动力工程学院,北京100191;中国航空工业集团公司沈阳发动机设计研究所,沈阳110015
基金项目:国家重点基础研究发展计划(2012CB720202)
摘    要:利用位于全消声室中的喷流噪声实验台研究了V形槽喷管在分开式排气系统中的降噪特性,比较了在剪切速度比为0.92工况下V形槽喷管的结构参数以及分布方式在冷喷流中对降噪效果的影响.结果表明:V形槽喷管降低了低频段的喷流噪声并增大高频段的喷流噪声;在喷管的下游方向有最好的低频段降噪效果,并具有最小的高频段喷流噪声增加量;增大V形槽喷管切入角可以增加低频段的降噪量,其降噪量最高为5dB;仅在外涵添加V形槽喷管可以增大低频段的降噪量并抑制高频段的喷流噪声的增加;V形槽喷管齿数的变化对降噪效果有一定的影响,但其影响远小于切入角的变化对降噪效果的影响;另外V形槽喷管可以显著地降低喷管下游方向的声压级大小.

关 键 词:喷流噪声  分开式排气  V形槽喷管  切入角  齿数
收稿时间:2013/11/17 0:00:00

Experiment of noise reduction in separate flow system using chevron nozzles
HE Jing-yu,SHAO Wan-ren,XU Ying-bo and LI Xiao-dong.Experiment of noise reduction in separate flow system using chevron nozzles[J].Journal of Aerospace Power,2015,30(2):324-330.
Authors:HE Jing-yu  SHAO Wan-ren  XU Ying-bo and LI Xiao-dong
Institution:School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;Shenyang Engine Design and Research Institute, Aviation Industry Corporation of China, Shenyang 110015, China;School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
Abstract:The noise reduction characteristics of chevron nozzles was investigated in separate flow system. All the experiments were carried out on the jet noise rig in the anechoic chamber. The effect of the structural parameters and distribution of chevron nozzles on cold jet noise reduction was explored in which shear velocity ratio was 0.92. The results show that chevron nozzles reduce jet noise at low frequencies, but increase jet noise at high frequencies. Besides, chevron nozzles has a best low-frequency noise reduction at downstream with lowest high-frequency noise penalty. The noise is decreased at the low frequencies and the peak noise reduction is 5dB when penetration angles of chevron nozzles are increased. The chevron nozzle only on fan has a good low frequency noise reduction and an ability of noise suppression at high frequencies. Although slight differences are observed with varying number of chevron, it seems that the effect is less significant than that of the penetration angles. The sound pressure level downstream is reduced significantly by chevron nozzles.
Keywords:jet noise  separate flow  chevron nozzle  penetration angle  number of chevrons
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