SAE Technical Paper Series 1996
DOI: 10.4271/965564
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Attachment-Line Transition and Boundary-Layer Relaminarization on a High-Lift Wing in Flight

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“…They found that the flows for stenosises had laminar characteristics and became turbulent through shear-layer instability under a strong adverse pressure gradient which was responsible for cellular dysfunction, leading to the development of atherosclerotic lesions [ 11 , 12 ]. The initial relaminarization of engineering applications was analyzed by Roback et al [ 13 ], who proposed a useful application of computational fluid dynamics capability to predict relaminarization. The dilation effect in relaminarization of a supersonic turbulent boundary layer was studied by Teramoto et al [ 14 ].…”
Section: Introductionmentioning
confidence: 99%
“…They found that the flows for stenosises had laminar characteristics and became turbulent through shear-layer instability under a strong adverse pressure gradient which was responsible for cellular dysfunction, leading to the development of atherosclerotic lesions [ 11 , 12 ]. The initial relaminarization of engineering applications was analyzed by Roback et al [ 13 ], who proposed a useful application of computational fluid dynamics capability to predict relaminarization. The dilation effect in relaminarization of a supersonic turbulent boundary layer was studied by Teramoto et al [ 14 ].…”
Section: Introductionmentioning
confidence: 99%