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高超声速平板边界层流动显示的试验研究

付佳 易仕和 王小虎 张庆虎 何霖

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高超声速平板边界层流动显示的试验研究

付佳, 易仕和, 王小虎, 张庆虎, 何霖

Experimental study on flow visualization of hypersonic flat plate boundary layer

Fu Jia, Yi Shi-He, Wang Xiao-Hu, Zhang Qing-Hu, He Lin
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  • 本文在高超声速脉冲式风洞内对基于纳米示踪的平面激光散射技术(nano-based planar laser scattering, NPLS)的应用进行了探索, 并在此基础上对平板边界层流动结构的精细测量进行了研究. 试验来流Ma=7.3, 总压4.8 MPa, 总温680 K. 通过时序的分析和调试, 对各分系统实现了高精度的同步控制; 定量的粒子注入及混合, 实现了粒子的均匀撒播, 对主流获得了均匀的显示效果; 对于边界层流动, 获得了精细的瞬态流动结构图像, 显示了层流到湍流的转捩过程, 并分析了其时空演化特性.
    The classical problem of flat plate boundary layer which involves turbulence and transition is still hot, and a mass of work should be done to reach a high accuracy measurement of this flow, especially under the condition of high velocity. In the present paper, the application of the nano-based planar laser scattering (NPLS) method in a hypersonic short-duration facility is explored, and then the high accuracy measurement of a flat plate boundary layer is studied. The Mach number of the main flow is 7.3, the total pressure is 4.8 MPa, and the total temperature is 680 K. Through analysis and tests, the synchronization control of the NPLS system with the test facility is realized, and with the quantitative control, the tracer particle is uniformly seeded. Based on this, the transient boundary layer flow in the short-duration tunnel is visualized with high resolution, and the transition from laminar to turbulent flows is captured. The development characteristic of the flow is studied finally.
    • 基金项目: 国家自然科学基金(批准号: 11172326和11302256)资助的课题.
    • Funds: Project supported by the National Natural Science Foundation of China (Grant Nos. 11172326, 11302256).
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  • [1]

    Kline S J, Reynolds W C, Schranb F A, Runstadler P W 1967 J. Fluid Mech. 30 741

    [2]

    Theodorsen T 1952 In: Proceedings of the Second Midwestern Conference on Fluid Mechanics Columbus, USA

    [3]

    Head M R, Bandyopadhyay P R 1981 J. Fluid Mech. 107 297

    [4]

    Smits A J, Spina E F, Alving A E, Smith R W, Fernando E M, Donovan J F 1989 Phys. Fluids 1 1865

    [5]

    Smith M W, Smits A J 1995 Exps. Fluids. 18 288

    [6]

    Smith M W, Smits A J, Miles R B 1988 Opt. Lett. 14 916

    [7]

    Ringuette M J, Wu M, Martin M P 2008 J. Fluid Mech. 594 59

    [8]

    Gao H, Fu D X, Ma Y W, Li X L 2005 Chin. Phys. Lett. 22 1709

    [9]

    Guarini S E, Moser R D, Shariff K, Wray A 2000 J. Fluid Mech. 414 1

    [10]

    Maeder T, Adams N A, Kleiser L J 2001 Fluid Mech. 429 187

    [11]

    Baumgartner M L, Erbland P J, Etz M R, Yalin A, Muzas B K, Smits A J, Lempert W R, Miles R B 1997 35th Aerospace Sciences Meeting & Exhibit Reno, NV 1997

    [12]

    Martin M P 2004 AIAA Paper 2004-2337

    [13]

    Liang X, LI X L 2013 Sci. Sin-Phys. Mech. Astron 56 1408

    [14]

    Forkey J N, Lempert W R, Miles R B 1998 Exps. Fluids. 24 151

    [15]

    Boguszko M, Elliott G S 2005 Exps. Fluids 38 33

    [16]

    Danehy P M, Wilkes J A, Alderfer D W 2006 AIAA Paper 2006-3442

    [17]

    Bathel B F, Danely P M, Inman J A 2008 AIAA Paper 2008-4266

    [18]

    He L, Yi S H, Tian L F, Chen Z, Zhu Y Z 2013 Chin. Phys. B 22 024704

    [19]

    Zhu Y Z, Yi S H, Chen Z, Ge Y, Wang X H, Fu J 2013 Acta Phys. Sin. 62 084219 (in Chinese) [朱杨柱, 易仕和, 陈值, 葛勇, 王小虎, 付佳 2013 物理学报 62 084219]

    [20]

    Chen Z, Yi S H, He L, Tian L F, Zhu Y Z 2012 Chinese Science Bulletin 57 584

    [21]

    Zhang Q H, Yi S H, Zhu Y Z, Chen Z, Wu Y 2013 Chin. Phys. Lett. 30 044701

    [22]

    He L, Yi S H, Zhao Y X, Tian L F, Chen Z 2011 Chinese Science Bulletin 54 1702

    [23]

    He L, Yi S H, Zhao Y X, Tian L F, Chen Z 2011 Chinese Science Bulletin 56 489

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出版历程
  • 收稿日期:  2014-06-12
  • 修回日期:  2014-09-01
  • 刊出日期:  2015-01-05

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