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Effect of micro-ramps on supersonic boundary layer past a double wedge

  • Zhang Qinghu*
  • , Xu Xiaobin
  • , Wang Xiong
  • , Lin Jingzhou
  • , Tong Hua
  • *此作品的通讯作者
  • China Aerodynamics Research and Development Center

科研成果: 期刊稿件文章同行评审

摘要

Abstract: The effect of micro-ramps on Mach 3 boundary layer structures past a double wedge was experimentally investigated in a supersonic low-noise wind tunnel using nano-tracer planar laser scattering (NPLS) technique. The fine structures of supersonic flow over the double wedge with and without the micro-ramps, as well as temporal and spatial evolutionary characteristics of the vortex structures with the micro-ramps, were revealed. Graphical abstract: [Figure not available: see fulltext.].

源语言英语
页(从-至)1-4
页数4
期刊Journal of Visualization
21
1
DOI
出版状态已出版 - 1 2月 2018
已对外发布

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