Volume 37 Issue 6
Dec.  2023
Turn off MathJax
Article Contents
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
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

The development of the movable solid wall test section for the 5.5 m × 4.0 m acoustic wind tunnel

doi: 10.11729/syltlx20220061
  • Received Date: 2022-06-30
  • Accepted Date: 2022-09-23
  • Rev Recd Date: 2022-09-23
  • Available Online: 2023-06-15
  • Publish Date: 2023-12-30
  • According to the design indexes and functional requirements of the movable solid wall test section for the 5.5 m × 4.0 m acoustic wind tunnel, this report presents the design project of overall scheme. The simulation calculation is carried out for the strength, stiffness and mode of the frame in the movable solid wall test section. The key technologies of positioning and locking, lifting mechanism, replaceable lower wall panel and adjustable opening side wall panel are studied in detail. At the same time, specific solutions are provided for the key problems in its processing and assembly process. The above research contents have important reference value for the design of the closed test section of the large acoustic wind tunnel of the same type.
  • loading
  • [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.
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Figures(13)

    Article Metrics

    Article views (184) PDF downloads(22) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return