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0.3 m低温风洞液氮供给系统研制

张伟 高荣 张双喜

张伟, 高荣, 张双喜. 0.3 m低温风洞液氮供给系统研制[J]. 航空动力学报, 2020, 35(5): 1009-1017. doi: 10.13224/j.cnki.jasp.2020.05.013
引用本文: 张伟, 高荣, 张双喜. 0.3 m低温风洞液氮供给系统研制[J]. 航空动力学报, 2020, 35(5): 1009-1017. doi: 10.13224/j.cnki.jasp.2020.05.013
ZHANG Wei, GAO Rong, ZHANG Shuangxi. Development of liquid nitrogen supplying system of 0.3 m cryogenic wind tunnel[J]. Journal of Aerospace Power, 2020, 35(5): 1009-1017. doi: 10.13224/j.cnki.jasp.2020.05.013
Citation: ZHANG Wei, GAO Rong, ZHANG Shuangxi. Development of liquid nitrogen supplying system of 0.3 m cryogenic wind tunnel[J]. Journal of Aerospace Power, 2020, 35(5): 1009-1017. doi: 10.13224/j.cnki.jasp.2020.05.013

0.3 m低温风洞液氮供给系统研制

doi: 10.13224/j.cnki.jasp.2020.05.013
基金项目: 国家自然科学青年基金(51806234)

Development of liquid nitrogen supplying system of 0.3 m cryogenic wind tunnel

  • 摘要: 基于系统级的一维热流体模拟分析,建立了适用于研究分析0.3 m低温风洞液氮供给系统的数学模型,并开展了系统漏热、两相流及缓冲罐中液氮容积等流体动力学分析;在系统现有控制策略及试验数据的基础上,基于该数学模型开展了系统压力动态响应分析,获得了在阀门动态调节过程中管网压力的瞬态响应,计算结果与试验值的总体误差控制在10%以内。喷射压力一致化改造避免了阀间干扰,添加的回流管道消除了供给末端的两相流现象,使喷射压力控制精度达到1.1%,调节时间减少到23 s,实现了风洞总温快速安全调节和精确控制。

     

  • [1] ZHANG Zhen,NIU Ling.Current status and key technologies of cryogenic wind tunnel[J].Cryogenics,2015,204(2):57-62.
    [2] BOSNYAKOV S M,CHEVAGIN A F,VLASENKO V V.TsAGI’s experience in numerical simulation of flow in cryogenic wind tunnel[C]∥International Conference on the Methods of Aerophysical Research.Perm,Russia:2016:020007.1-020007.13.
    [3] 廖达雄,黄知龙,陈振华,等.大型低温高雷诺数风洞及其关键技术综述[J].实验流体力学,2014,28(2):1-6. LIAO Daxiong,HUANG Zhilong,CHEN Zhenhua,et al.Review on large-scale cryogenic wind tunnel and key technologies[J].Journal of Experiments in Fluid Mechanics,2014,28(2):1-6.(in Chinese)
    [4] ADCOCK J B.Effect of LN2 injection station location on the drive fan power and LN2 requirement of a cryogenic wind tunnel[R].NASA-TM-X-74036,1977.
    [5] LI Jingfeng,WANG Kai,ZHANG Xiaobin,et al.A parametric sensitivity study by numerical simulations on plume dispersion of the exhaust from a cryogenic wind tunnel[J].Journal of Zhejiang University-Science A (Applied Physics & Engineering),2018,19(10):746-757.
    [6] KILGORE R A.Design features and operational characteristics of the Langley pilot transonic cryogenic tunnel[R].NASA-N74-34676,1974.
    [7] 陈振华,张伟,高荣,等.液氮抽真空制冷的理论及试验[J].航空动力学报,2019,34(9):1971-1976. CHEN Zhenhua,ZHANG Wei,GAO Rong,et al.Theoretical and experiment studies of vacuum cooling of liquid nitrogen[J].Journal of Aerospace Power,2019,34(9):1971-1976.(in Chinese)
    [8] GOBERT J L.ETW control system:design and first results[R].AIAA 94-2514,1994.
    [9] SAUNDERS T B.The European transonic wind tunnel-testing at flight Reynolds numbers[R].AIAA 96-0227,1996.
    [10] OWEN W,BISSETT C,MICHAEL H.Selected major modifications to the national transonic facility[R].AIAA 2009-419,2009.
    [11] VENKI S,OWEN W,BISSETT R,et al.Reactivation of the NTF 3000 ton liquid nitrogen tank from ambient condition[R].AIAA 2015-3009,2015
    [12] REBSTOCK R,ZHAI J N,SCHAFFARCZYK A.Experimental investigation of Reynolds number effect on wind turbine profiles in the cryogenic wind tunnel Cologne DNW-KKK[J].Journal of Energy and Power Engineering,2013,7(10):1957-1965.
    [13] 周廷波,高超,张正科,等.NF-6风洞喷液氮降温系统研制[J].航空动力学报,2018,33(2):327-337. ZHOU Tingbo,GAO Chao,ZHANG Zhengke,et al.Development of liquid nitrogen injection cooling system of NF-6 wind tunnel[J].Journal of Aerospace Power,2018,33(2):327-337.(in Chinese)
    [14] 张蓓乐,陈小砖,薛绒,等.采用液氮喷雾技术的低温环路结构模拟系统研究[J].西安交通大学学报,2019,53(5):109-114. ZHANG Beile,CHEN Xiaozhuan,XUE Rong,et al.Study on the low-temperature air loop simulation system based on liquid nitrogen spray technology[J].Journal of Xi’an Jiaotong University,2019,53(5):109-114.(in Chinese)
    [15] 阮一逍,薛绒,赖欢,等.单液氮液滴在气流中的蒸发运动特性研究[J].西安交通大学学报,2017,51(6):147-152. RUAN Yixiao,XUE Rong,LAI Huan,et al.Evaporation and movement characteristics of single liquid nitrogen droplet in high-speed gas flow[J].Journal of Xi’an Jiaotong University,2017,51(6):147-152.(in Chinese)
    [16] 廖达雄,张海洋,阮一逍,等.氮液滴在气流中的破碎和碰撞模拟[J].哈尔滨工业大学学报,2018,50(7):185-191. LIAO Daxiong,ZHANG Haiyang,RUAN Yixiao,et al.Numerical study on the breakup and collision of nitrogen droplets in high-speed gas flow[J].Journal of Harbin Institute of Technology,2018,50(7):185-191.(in Chinese)
    [17] THIBODEAUX J J,BALAKRISHNA S.Automatic control of a 0.3 m cryogenic test facility[J].Journal of Guidance and Control,1980,4(4):428-432.
    [18] BALAKRISHNA S.Automatic control of a liquid nitrogen cooled,closed circuit,cryogenic pressure tunnel[R].NASA-CR-162636,1980.
    [19] ZHU Rusong,YIN Guofu,TANG Gengsheng,et al.Temperature trajectory control of cryogenic wind tunnel with robust L1 adaptive control[J].Transactions of the Institute of Measurement and Control,2018,40(13):3675-3689.
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出版历程
  • 收稿日期:  2019-11-25
  • 刊出日期:  2020-05-28

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