Gao Yongwei, Huang Peng, Zhu Qiliang, Liang Chenggang. Experimental study on pressure fluctuation sensor-based diagnostic for boundary layer transition with long-fine tubing system[J]. Journal of Experiments in Fluid Mechanics, 2014, (6): 98-103. DOI: 10.11729/syltlx20140021
Citation: Gao Yongwei, Huang Peng, Zhu Qiliang, Liang Chenggang. Experimental study on pressure fluctuation sensor-based diagnostic for boundary layer transition with long-fine tubing system[J]. Journal of Experiments in Fluid Mechanics, 2014, (6): 98-103. DOI: 10.11729/syltlx20140021

Experimental study on pressure fluctuation sensor-based diagnostic for boundary layer transition with long-fine tubing system

More Information
  • Low speed flow transition zone of boundary layer can be detected by means of pres-sure fluctuation measurement over the surface of the test model.It is convenient that fluctuation pressure transducers are arranged outside the model through long-fine tubing system.The distor-tion of pressure signal caused by the tubing system should be recognized.Under the static condi-tion(V= 0m/s),the authors measured a series of sound signals over an airfoil model surface through the tubing system.The sound signal source come from a speaker actuated by a signal generation.The model chord length is 0.8m and the model span is 1.6m in length.The tubes are about 1.2m long and their inner diameters are 0.8mm.The tubing system has proved to be able to transmit the characteristics of the surface pressure fluctuation for the transition detection.Un-der the condition of section flow velocity V= 30m/s,signals of the surface pressure fluctuation transmitted along the chord of the model were measured and the boundary layer transition zones were located.This experiment was conducted in NF-3 low-speed wind tunnel of Northwestern Polytechnical University.The authors suggest that the pressure fluctuation transition diagnostic method with long-fine tubing system is promising and further researches should be carried out.
  • Related Articles

    [1]LIU Qiang, LI Qiang, WEI Chunhua, YIN Xiwei, JIANG Hailin, LIANG Lei. The dynamic calibration method of PSP and its characteristics research considering the influence of temperature[J]. Journal of Experiments in Fluid Mechanics. DOI: 10.11729/syltlx20230161
    [2]CAI Yanqing, YANG Xiaoli, WANG Kaixing, LIU Fuqiang, LENG Xianyin, WANG Shaolin, LIU Cunxi, MU Yong, XU Gang. Experimental study on the effect of two-stage radial spacing on flow field and atomization in LDI staged combustor[J]. Journal of Experiments in Fluid Mechanics, 2023, 37(6): 15-24. DOI: 10.11729/syltlx20220082
    [3]WANG Lei, LI Zhe, FENG Lihao. Parameter influence and optimization of energy conversion efficiency of synthetic jet actuators[J]. Journal of Experiments in Fluid Mechanics, 2023, 37(4): 87-95. DOI: 10.11729/syltlx20230039
    [4]ZHAO Rongjuan, LIU Shiran, ZHOU Zheng, WU Liyin, LYU Zhiguo. Research of scramjet thrust test in shock tunnel[J]. Journal of Experiments in Fluid Mechanics, 2022, 36(4): 103-108. DOI: 10.11729/syltlx20210025
    [5]CHEN Lin, FENG Jing. Thermophysical properties research progress of ferroelastic RETaO4 ceramics[J]. Journal of Experiments in Fluid Mechanics, 2022, 36(4): 56-76. DOI: 10.11729/syltlx20220020
    [6]LIU Yu, XIAO Baoguo, WANG Lan, CHEN Weiqiang. Standing stability enhancement method of oblique detonation waves in a confined space and its experimental validation[J]. Journal of Experiments in Fluid Mechanics, 2021, 35(1): 109-116. DOI: 10.11729/syltlx20200084
    [7]ZHAO Rongjuan, HUANG Jun, LIU Shiran, LYU Zhiguo, LI Guozhi. Application of ANSYS in piezoelectric balance design[J]. Journal of Experiments in Fluid Mechanics, 2020, 34(1): 96-102. DOI: 10.11729/syltlx20190005
    [8]Zhang Shiyu, Fu Zengliang, Zhao Junbo, Gao Qing, Qian Er. Development of near-space-vehicle anemometer and calibration tests in low-temperature-low-static-pressure wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2017, 31(2): 81-85, 103. DOI: 10.11729/syltlx20160137
    [9]Miao Bo, Zhu Chunling, Zhu Chengxiang, Zhang Huijun, Fu Bin. Vibration de-icing method with piezoelectric actuators on airfoil surface[J]. Journal of Experiments in Fluid Mechanics, 2016, 30(2): 46-53. DOI: 10.11729/syltlx20160010
    [10]LIU Chu-ping, MENG Song-he, DU Bai-he, WANG Guo-lin. Preliminary tests of non-ablative thermal protection materials[J]. Journal of Experiments in Fluid Mechanics, 2009, 23(3): 50-53,69. DOI: 10.3969/j.issn.1672-9897.2009.03.011
  • Cited by

    Periodical cited type(4)

    1. 苏鑫,管润程,王桥,苑伟政,吕湘连,何洋. 基于深度学习的结冰区域和厚度检测方法. 航空学报. 2023(S2): 205-213 .
    2. 郝云权,赵大志,李伟斌,赵炜,陈江涛. 飞机结冰的不确定性量化研究进展. 航空动力学报. 2022(09): 1855-1871 .
    3. 王良禹,徐浩军,张喆,裴彬彬,薛源. 结冰对飞机横航向飞行品质的影响. 飞行力学. 2018(01): 16-19 .
    4. 易贤,李维浩,王应宇,马洪林. 飞机结冰传感器安装位置确定方法. 实验流体力学. 2018(02): 48-54 . 本站查看

    Other cited types(4)

Catalog

    Article Metrics

    Article views (141) PDF downloads (7) Cited by(8)
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return
    x Close Forever Close