Volume 42 Issue 2
Mar.  2012
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YI Shihe, HE Lin, TIAN Lifeng, ZHAO Yuxin. THE APPLICATION OF NANO-TRACER PLANAR LASER SCATTERING IN SHOCK WAVE FIELD MEASUREMENT[J]. Advances in Mechanics, 2012, 42(2): 197-205. doi: 10.6052/1000-0992-2012-2-20120207
Citation: YI Shihe, HE Lin, TIAN Lifeng, ZHAO Yuxin. THE APPLICATION OF NANO-TRACER PLANAR LASER SCATTERING IN SHOCK WAVE FIELD MEASUREMENT[J]. Advances in Mechanics, 2012, 42(2): 197-205. doi: 10.6052/1000-0992-2012-2-20120207

THE APPLICATION OF NANO-TRACER PLANAR LASER SCATTERING IN SHOCK WAVE FIELD MEASUREMENT

doi: 10.6052/1000-0992-2012-2-20120207
Funds:  The project was supported by the National Natural Science Foundation of China (11172326), the National Basic Research Program of China (2009CB724100).
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  • Corresponding author: YI Shihe
  • Received Date: 2012-02-13
  • Rev Recd Date: 2012-03-13
  • Publish Date: 2012-03-25
  • There are usually three dimensional structure in the complex flow flelds involving shock waves and interaction between shock waves and boundary layers. It is of low spatial resolution to study these flow flelds using traditional ow visualization techniques, such as schlieren, shadow and interference methods, and the three dimensional characters are usually hard to be identi ed. The Nano-tracer based Planar Laser Scattering (NPLS) technique is a new method developed recently for the measurement and visualization of supersonic three dimensional complex flow flelds. It has achieved spatiotemporal resolution, and is thus a good method for the measurement of complex flow flelds involving shock waves. In recent years, mainly with NPLS technique, we have carried out vast experimental research on typical complex flows in the area of aeronautics and aerospace, including supersonic flows over bullets, supersonic mixing layers, supersonic boundary layers and the interaction between shock waves and boundary layers. And advantages of the NPLS technique are clearly revealed in these studies. Process is elucidated in this paper for the application of NPLS technique to the measurement of complex flow flelds involving shock waves.

     

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  • 1 Dolling D S. 50 years of shock wave/boundary layer interaction-what next? AIAA 2000-2596, 2000
    2 Smits A J, Dussauge J P. Turbulent Shear Layers in Supersonic Flow. 2nd editon. New York: Springer, 2006
    3 Humble R A, Scarano F, Oudheusden B W. Experimental study of an incident shock wave/turbulent boundary layer interaction using PIV. AIAA paper, 2006-3361, 2006
    4 董志勇, 吕阳泉. 激波与边界层干扰研究综述. 浙江工业大 学学报, 2009, 29(3): 295-300
    5 Hadjadj A, Dussauge J P. Shock wave boundary layer interaction. Shock Waves, 2009, 19: 449-452
    6 Délery J, Dussauge J P. Some physical aspects of shock wave/boundary layer interactions. Shock Waves, 2009, 19:453-468
    7 Kalra C S, Zaidi S H, Alderman B J, et al. Non-thermal control of shock-wave induced boundary layer separation using magneto-hydrodynamics. AIAA paper 2007-4138,2007
    8 Palma P C, Danely P M, Houwing A F P, et al. PLIF thermometry of a free-pistion shock-tunnel nozzle ow. AIAA paper 1998-2703, 1998
    9 Danehy P M, O'Byrne S. Measurement of NO density in a free-piston shock tunnel using PLIF. AIAA paper 1999-0772, 1999
    10 O'Byrne S, Stotz I, Neely A J, et al. OH PLIF imaging of supersonic combustion using cavity injection. AIAA paper 2005-3357, 2005
    11 Danehy P M, Wilkes J A, Alderfer D W, et al. Planar laser-induced uorescence (PLIF) investigation of hypersonic ow elds in a Mach 10 wind tunnel (invited). AIAA paper 2006-3442, 2006
    12 耿辉, 翟振辰, 周松柏, 等. 欠膨胀自由射流密度场的丙酮平 面激光诱导荧光显示与测量. 实验流体力学, 2006, 20: 85-90
    13 Bathel B F, Danely P M, Inman J A, et al. PLIF visualization of active control of hypersonic boundary layers using blowing. AIAA paper 2008-4266, 2008.
    14 Miles R B, Lempert W R. Two-dimensional measurement of density, velocity, and temperature in turbulent highspeed air ows by UV Rayleigh scattering. Appl. Phys.,1990, 51: 1-7
    15 Elliott G S, Boguszko M, Carter C. Filtered Rayleigh Scattering: toward multiple property measurements (invited). In: Proceedings of the 39th AIAA Aerospace Sciences Meeting & Exhibit, Reno, NEVADA, January 8-11, 2001
    16 Panda J, Seasholtz R G. Density uctuation measurement in supersonic fully expanded jets using Rayleigh scattering. AIAA paper 1999-1870, 1999,
    17 Panda J, Seasholtz R G. Density measurement in underexpanded supersonic jets using Rayleigh scattering. In: Proceeding of the 36th Aerospace Sciences Meeting & Exhibit, Reno, NEVADA, January 12-15, 1998
    18 Mielke A F, Elam K A, Sung C J. Rayleigh scattering diagnostic for measurement of temperature, velocity, and density uctuation spectra. In: Proceedings of the 44th AIAA Aerospace Science Meeting and Exhibit, Reno, NEVADA, January 9-12, 2006
    19 王杰, 姚建铨, 于意仲, 等. 瑞利散射用于气体流场二维瞬态 密度测量. 光电子 激光, 2001, 12(1): 62-64
    20 Lempert W R, Wu P F, Miles R B. Filtered Rayleigh scattering measurements using a MHz rate pulse-burst laser system. AIAA paper 1997-0200, 1997
    21 Zhao Y X, Yi S H, Tian L F, et al. Supersonic ow imaging via nanoparticles. Sci China Ser E-Tech Sci, 2009,52(12): 3640-3648
    22 易仕和, 赵玉新, 何霖, 等. NPLS 技术及其在超声速湍流流 动显示中的应用. 力学50 周年大会, 北京, 2007
    23 Yi S H, He L, Zhao Y X, et al. A ow control study of a supersonic mixing layer via NPLS. Sci China Ser G, 2009,52: 2001-2006
    24 Zhao Y X, Yi S H, He L, et al. The experimental study of interaction between shock wave and turbulence. Chinese Sci Bull, 2007, 52: 1297-1301
    25 赵玉新, 易仕和, 何霖, 等. 超声速湍流混合层中小激波结构 的实验研究. 国防科大学报, 2007, 29: 12-15
    26 Zhao Y X, Yi S H, Tian L F, et al. The fractal measurement of experimental images of supersonic turbulent mixing layer. Sci China Ser G, 2008, 51: 1134-1143
    27 田立丰, 易仕和, 赵玉新, 等. 超声速弹头凹型光学头罩流动 显示研究. 实验流体力学, 2009, 23(1): 15-17
    28 He L, Yi S H, Zhao Y X, et al.. Visualization of coherent structures in a supersonic at-plate boundary layer. Chinese Sci Bull, 2011, 56: 489-494
    29 Tian L F, Yi S H, Zhao Y X, et al. Study of density eld measurement based on NPLS technique in supersonic ow. Sci China Ser G, 2009, 52(9): 1357-1363
    30 Yi S H, Tian L F, Zhao Y X, et al. Aero-optical aberration measuring method based on NPLS and its application. Chinese Sci Bull, 2010, 55: 3545-3549
    31 Zhao Y X, Yi S H, Tian L F, et al. Multiresolution analysis of density uctuation in supersonic mixing layer. Sci China Tech Sci, 2010, 53: 584-591
    32 Zhao Y X, Yi S H, Tian L F, et al. Density eld measurement and approximate reconstruction of supersonic mixing layer. Chinese Sci Bull, 2010, 55: 2004-2009
    33 田立丰, 易仕和, 赵玉新, 等. 超声速光学头罩流场的PIV 研究. 实验流体力学, 2010, 24(1): 26-29
    34 He L, Yi S H, Zhao Y X, et al. Experimental study of a supersonic turbulent boundary layer using PIV. Sci China Ser G, 2011, 54: 1702-1709
    35 Gilbert R A D. Evaluation of FFT based cross-correlation algorithms for particle image velocimetry: [Master Thesis]. Londen: University of Waterloo, 2002
    36 易仕和, 田立丰, 赵玉新, 等. 基于NPLS 原理的气动光学畸 变测量方法和应用的研究. 科学通报, 2010, 55(23): 2283-2288
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