张馨元.[J].民用飞机设计与研究,2017,(4):42-
A Review of the Attachment Line Instability for Hybrid Laminar Flow Control
  
DOI:
中文关键词:
英文关键词:attachment line  hybrid laminar flow control (HLFC)  boundary layer  subcritical instability  leading edge
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作者单位
张馨元 上海飞机设计研究院上海 201210 
中文摘要:
英文摘要:This paper focuses on the investigation of the attachment line instability for Hybrid Laminar Flow Control (HLFC), one of the most promising drag reduction technologies for modern transport aircraft respect to high Reynolds numbers and large sweep angles. The attachment line instability also plays an important role during laminar turbulent transition control and HLFC design on a swept wing. The overview of historical research is presented and knowledge gaps are pointed out as the conclusion.
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