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Separated laminar shear layer transition over a two-dimensional bump

  • Beihang University

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

The laminar boundary layer separation over a two-dimensional bump is experimentally investigated in a water channel with hydrogen-bubble visualization and particle image velocimetry (PIV) techniques, focusing on the characteristics of separated shear layer, the evolution of flow structure and the development of unstable disturbances. It is shown that the separation point, to a large extent, depends on the geometry of the bump, while the reattachment point is mainly affected by Reynolds number. A quite long and narrow separation bubble with its vortex centre located very close to the reattachment point is observed when the laminar boundary layer separates over the bump. The shear layer transition begins as soon as the laminar boundary layer flow is separated, with the flow field perturbation increasing rapidly to a maximum value and then decreasing slowly along the streamwise direction. The formation and shedding of two-dimensional spanwise vortex structures are observed along the shear layer due to Kelvin-Helmholtz instability. These spanwise vortices gradually lose their two-dimensionality and evolve into hairpin vortices downstream.

源语言英语
主期刊名29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014
出版商International Council of the Aeronautical Sciences
ISBN(电子版)3932182804
出版状态已出版 - 2014
活动29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014 - St. Petersburg, 俄罗斯联邦
期限: 7 9月 201412 9月 2014

出版系列

姓名29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014

会议

会议29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014
国家/地区俄罗斯联邦
St. Petersburg
时期7/09/1412/09/14

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