| Citation: | CHEN Jiming, LÜ Jinlei, LIAO Daxiong, WU Shenghao, PEI Haitao, SHI Zhiwei. Noise reduction technology in test section of continuous transonic wind tunnel[J]. Journal of Aerospace Power, 2021, 36(8): 1712-1719. doi: 10.13224/j.cnki.jasp.20200375
|
| [1] |
廖达雄, 陈吉明, 彭强, 等. 连续式跨声速风洞设计关键技术[J].实验流体力学, 2011, 25(4):74-78. LIAO Daxiong,CHEN Jiming,PENG Qiang,et al.Key design techniques of the low noise continuous transonic wind tunnel[J].Journal of experiments in fluid mechanics,2011, 25(4):74-78.(in Chinese)
|
| [2] |
廖达雄, 陈吉明, 郑娟, 等.0.6 m连续式跨声速风洞总体性能[J].实验流体力学, 2018, 32(6):88-93. LIAO Daxiong,CHEN Jiming,ZHENG Juan,et al.General performance of 0.6m continuous transonic wind tunnel[J]. Journal of Experiments in Fluid Mechanics,2018,32(6):88-93.(in Chinese)
|
| [3] |
WDAVIS M.Optimum transonic wind tunnel[R].AIAA 86-0755,1986.
|
| [4] |
MABEY D G. Flow unsteadiness and model vibration in wind tunnels at subsonic and transonic speeds[R]. London:Aeronautical Research Council,1970.
|
| [5] |
MABEY D G.Some remarks on the design of transonic tunnels with low levels of flow unsteadiness[R].NASA CR-2722, 1976.
|
| [6] |
LOWSON M V.Prediction of boundary layer pressure fluctuations[R].AFFDL-TR-67-167.1967.
|
| [7] |
谷嘉锦.跨声速风洞试验段低噪声壁板模型的声学试验[J]. 空气动力学学报, 2001, 19(1):62-65. GU Jiajin. Transonic wind tunnel acoustical experiment of low noise wall models for test section[J].Acta Aerodynamica Sinica,2001,19(1):62-65.(in Chinese)
|
| [8] |
恽起麟. 降低0.6 m×0.6 m跨超声速风洞气流噪声的研究[J].空气动力学学报, 1985(2):51-60. YUN Qilin. Investigation on reducing the flow noise of the 0.6 m×0.6 m trisonic wind tunnel[J].Acta Aerodynamica Sinica,1985(2):51-60.(in Chinese)
|
| [9] |
凌其杨,陶祖贤. 先进跨声速风洞的设计技术[J]. 气动实验与测量控制, 1996,10(3):11-16. LING Qiyang, TAO Zuxian. Design technology for advanced transonic wind tunnel[J].1996,10(3):11-16.(in Chinese)
|
| [10] |
吕金磊, 盛美萍, 廖达雄, 等. 基于实验的跨声速风洞试验段噪声机理研究[J]. 空气动力学学报,2014,32(4):488-492. LÜ Jinlei,SHENG Meiping,LIAO Daxiong,et al.Investigation about transonic wind tunnel test section noise mechanism based on experimental[J]. Acta Aerodynamica Sinica, 2014, 32(4):488-492.(in Chinese)
|
| [11] |
马大猷, 沈壕.声学手册[M].北京:科学出版社.1983.
|
| [12] |
伍荣林, 王振羽. 风洞设计原理[M]. 北京:北京航空学院出版社, 1985.
|
| [13] |
陈吉明,吴盛豪,陈振华,等. 连续式跨声速风洞回路吸声降噪技术试验研究[J]. 西北工业大学学报, 2020, 38(4):855-861. CHEN Jiming,WU Shenghao,CHEN Zhenhua,et al.Experiment research on noise reduction for continuous transonic wind tunnel loop[J]. Journal of Northwestern Polytechnical University,2020,38(4):855-861.(in Chinese)
|
| [14] |
CREDLE O P.Perforated wall noise in the AEDC-PWT 16-FT and 4-FT transonic tunnels[R]. AEDC-TR-71-216, 1971.
|
| [15] |
SCHUTZENHOFER L A, HOWARD P W. Suppression of background noise in a transonic wind-tunnel test section[J].AIAA Journal,1975,13(11):1467-1471.
|
| [16] |
FRANK W S. Development of the porous-slot geometry of the NWTC test section[C]//Proceedings of Aerospace Sciences Meeting and Exhibit.Reno,US:AIAA,1997:1-13.
|
| [17] |
DOUGHERTY N S, ANDERSON C F, PARKER R L. An experimental study on suppression of edgetones from perforated wind tunnel walls[R].Washington:AIAA,1976.
|
| [18] |
刘光远,张林,陈德华,等. 跨声速风洞斜孔壁非线性流动试验[J].航空学报,2019,40(5):31-38. LIU Guangyuan, ZHANG Lin, CHEN Dehua, et al.Experiment on nonlinear flow near perforated wall with slanted holes in transonic wind tunnel[J].Acta Aeronautica et Astronautica Sinica,2019,40(5):31-38.(in Chinese)
|
| [19] |
丛成华,刘琴,张志峰,等. 专用跨声速风洞开孔壁试验段设计数值模拟[J].航空学报,2012,33(6):1014-1019. CONG Chenghua,LIU Qin,ZHANG Zhifeng,et al.Numerical simulation of design of transonic wind tunnel perforated test section[J]. Acta Aeronautica et Astronautica Sinica, 2012,33(6):1014-1019.(in Chinese)
|
| [20] |
鞠炼,白俊强,郭斌,等. 槽壁几何参数对跨声速风洞流场品质的影响[J].航空学报,2016,37(5):1440-1453. JU Lian, BAI Junqiang, GUO Bin, et al. Effect of geometry parameters on flow field quality in a transonic slotted wind tunnel[J].Acta Aeronautica et Astronautica Sinica,2016,37(5):1440-1453.(in Chinese)
|
DownLoad: