用电子束荧光技术研究高超声速边界层中的扰动现象

林贞彬, 郭大华, 朱进生, 余西龙

林贞彬, 郭大华, 朱进生, 余西龙. 用电子束荧光技术研究高超声速边界层中的扰动现象[J]. 实验流体力学, 2000, 14(4): 51-57. DOI: 10.3969/j.issn.1672-9897.2000.04.010
引用本文: 林贞彬, 郭大华, 朱进生, 余西龙. 用电子束荧光技术研究高超声速边界层中的扰动现象[J]. 实验流体力学, 2000, 14(4): 51-57. DOI: 10.3969/j.issn.1672-9897.2000.04.010
LIN Zhen-bin, GUO Da-hua, ZHU Jin-sheng, YU Xi-long. The investigation of perturbation phenomena in hypersonic boundary layer with electronic beam fluorescence technique[J]. Journal of Experiments in Fluid Mechanics, 2000, 14(4): 51-57. DOI: 10.3969/j.issn.1672-9897.2000.04.010
Citation: LIN Zhen-bin, GUO Da-hua, ZHU Jin-sheng, YU Xi-long. The investigation of perturbation phenomena in hypersonic boundary layer with electronic beam fluorescence technique[J]. Journal of Experiments in Fluid Mechanics, 2000, 14(4): 51-57. DOI: 10.3969/j.issn.1672-9897.2000.04.010

用电子束荧光技术研究高超声速边界层中的扰动现象

基金项目: 

国家自然科学基金

详细信息
  • 中图分类号: 51-1499/V

The investigation of perturbation phenomena in hypersonic boundary layer with electronic beam fluorescence technique

  • 摘要: 利用电子束荧光技术对高超声速平板边界层中的扰动现象进行实验研究,实验在炮风洞中进行,自由流马赫数为7.8,单位长度雷诺数为3.5×107/m,测量了平均密度分布、脉动密度分布,并获得了湍流密度脉动的互相关分布和频谱分布。实验结果表明在过渡区中有序与随机现象并存。
    Abstract: The perturbation phenomena in hypersonic flat plate boundary layer are investigated with electronic beam fluorescence technique in a gun wind tunnel. Mach number of free stream is about 7.8 and Reynolds number per unit length is 3.5 × 107/m. Average density distribution and fluctuation desity distribution are measured. The correlation distribution of turbulent density fluctuation and frequency spectrum distribution is obtained. Our experi mental results show that the phenomena are coexisted in order and at random in transition area.
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出版历程
  • 刊出日期:  2000-03-31

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