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- W2324334942 abstract "A separation bubble often exists on high altitude airfoils, for vhich natural laminar flov extends from 60 to 70 per cent of the chord to provide a lov drag, high performance airfoil under cruise conditions. A short laminar separation bubble occurring on this type of airfoil is the subject of this paper. Utilizing coincident laser velocimeter (LV) measurements. the mean velocities of the tangential and normal components of the velocity relative to the airfoil surface and the tvo-dimensional Reynoids stress tensor were measured at designated chord locations throughout the separated region. The data shov the essential features of the bounded shear layer as i t transitions above the recirculation zone. The mean momentum transfer influenced by the Reynolds stress production represents the dominant feature in the reattachment region. The LV measurements provide insight into the physical processes as the boundary layer transitions to a fully developed, turbulent profile dormstrean." @default.
- W2324334942 created "2016-06-24" @default.
- W2324334942 creator A5014080878 @default.
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- W2324334942 date "1987-03-24" @default.
- W2324334942 modified "2023-09-25" @default.
- W2324334942 title "An experimental investigation of a laminar separation on a natural laminar flow airfoil" @default.
- W2324334942 cites W2019568122 @default.
- W2324334942 cites W2054364861 @default.
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- W2324334942 doi "https://doi.org/10.2514/6.1987-458" @default.
- W2324334942 hasPublicationYear "1987" @default.
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