A survey is presented of factors affecting blunt leading-edge separation for swept and semi-slender wings. This class of separation often results in the onset and progression of separation-induced vortical flow over a slender or semi-slender wing. The term semi-slender is used to distinguish wings with moderate sweeps and aspect ratios from the more traditional highly-swept, low-aspect-ratio slender wing. Emphasis is divided between a selection of results obtained through literature survey a section of results from some recent research projects primarily being coordinated through NATO s Research and Technology Organization (RTO). An aircraft context to these studies is included.
A Survey of Factors Affecting Blunt Leading-Edge Separation for Swept and Semi-Slender Wings
28th AIAA Applied Aerodynamics Conference ; 2010 ; Chicago, IL, United States
2010-06-28
Conference paper
No indication
English
A Survey of Factors Affecting Blunt-Leading-Edge Separation for Swept and Semi-Slender Wings
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