Citation: | YANG W G, SHI Y, WANG R. The development of the movable solid wall test section for the 5.5 m × 4.0 m acoustic wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2023, 37(6): 86-91. DOI: 10.11729/syltlx20220061 |
[1] |
于涛, 范洁川, 贾元胜. 现代航空声学风洞技术现状与发展[J]. 实验流体力学, 2007, 21(3): 86–91. DOI: 10.3969/j.issn.1672-9897.2007.03.018
YU T, FAN J C, JIA Y S. The present situation and development of modern aeroacoustic wind tunnel technique[J]. Journal of Experiments in Fluid Mechanics, 2007, 21(3): 86–91. doi: 10.3969/j.issn.1672-9897.2007.03.018
|
[2] |
DUELL E, YEN J, ARNETTE S, et al. Recent advances in large scale aeroacoustic wind tunnels[C]//Proc of the 8th AIAA/CEAS Aeroacoustics Conference & Exhibit. 2002: 2503. doi: 10.2514/6.2002-2503
|
[3] |
SODERMAN P, JAEGER S, HAYES J, et al. Acoustic performance of the 40- by 80- foot wind tunnel test section deep acoustic lining[C]//Proc of the 6th Aeroacoustics Conference and Exhibit. 2000: 1939. doi: 10.2514/6.2000-1939
|
[4] |
MATHEW J, BAHR C, CARROLL B, et al. Design, fabrication, and characterization of an anechoic wind tunnel facility[C]//Proc of the 11th AIAA/CEAS Aeroacoustics Conference. 2005: 3052. doi: 10.2514/6.2005-3052
|
[5] |
中国人民解放军总装备部. 高速风洞和低速风洞流场品质要求: GJB 1179A–2012[S]. 北京: 总装备部军标出版发行部, 2012.
|
[6] |
李鹏, 汤更生, 余永生, 等. 航空声学风洞的声学设计研究[J]. 实验流体力学, 2011, 25(3): 82–86. DOI: 10.3969/j.issn.1672-9897.2011.03.018
LI P, TANG G S, YU Y S, et al. Research of acoustic design for aeroacoustic wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2011, 25(3): 82–86. doi: 10.3969/j.issn.1672-9897.2011.03.018
|
[7] |
恽起麟. 实验空气动力学[M]. 北京: 国防工业出版社, 1991.
YUN Q L. Experimental aerodynamics[M]. Beijing: National Defense Industry Press, 1991.
|
[8] |
虞择斌, 刘政崇, 陈振华, 等. 2 m超声速风洞结构设计与研究[J]. 航空学报, 2013, 34(2): 197–207.
YU Z B, LIU Z C, CHEN Z H, et al. Structure design and research of 2 m supersonic wind tunnel[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(2): 197–207.
|
[9] |
中国人民解放军总装备部军事训练教材编辑工作委员会. 高低速风洞气动与结构设计[M]. 北京: 国防工业出版社, 2003.
|
[10] |
赖欢, 祝长江, 陈万华, 等. 大型低温风洞结构设计关键技术分析[J]. 实验流体力学, 2022, 36(1): 19–26. DOI: 10.11729/syltlx20210040
LAI H, ZHU C J, CHEN W H, et al. Key technology for mechanical design in large-scale cryogenic wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2022, 36(1): 19–26. doi: 10.11729/syltlx20210040
|
[11] |
陈吉明, 吕金磊, 廖达雄, 等. 连续式跨声速风洞试验段降噪技术[J]. 航空动力学报, 2021, 36(8): 1712–1719. DOI: 10.13224/j.cnki.jasp.20200375
CHEN J M, LÜ J L, LIAO D X, et al. 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
|
[12] |
孙启志, 巢根明, 凌岗, 等. 高超声速风洞试验段优化设计[J]. 机械工程与自动化, 2019(1): 134–135, 138. DOI: 10.3969/j.issn.1672-6413.2019.01.053
SUN Q Z, CHAO G M, LING G, et al. Optimized design of hypersonic wind tunnel test section[J]. Mechanical Engineering & Automation, 2019(1): 134–135, 138. doi: 10.3969/j.issn.1672-6413.2019.01.053
|
[13] |
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. DOI: 10.11729/syltlx20170086
LIAO D X, CHEN J M, ZHENG J, et al. General performance of 0.6 m continuous transonic wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2018, 32(6): 88–93. doi: 10.11729/syltlx20170086
|
[14] |
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.
|
[15] |
中国机械工程学会焊接学会焊接结构设计与制造(XV)委员会. 焊接结构设计手册[M]. 北京: 机械工程出版社, 1990.
|
[16] |
陈建兵, 高鑫宇, 蔡清青, 等. 0.3 m风洞第二喉道结构设计与分析[J]. 机械设计, 2015, 32(1): 35–38.
CHEN J B, GAO X Y, CAI Q Q, et al. Structural design and analysis of the second throat in 0.3 m wind tunnel[J]. Journal of Machine Design, 2015, 32(1): 35–38.
|