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- W1975757887 abstract "Quantifiable vortex features and separated-flow origins have been determined on an F-106B aircraft at l-g subsonic speeds using the vapor-screen technique coupled with image enhancement, photogrammetry, and computer graphics. In particular, the spatial location of vortex cores, their tracks over the wing, and the approximate reattachment locations have been determined as a function of angle of attack and Reynolds number. Increasing the Reynolds number generally delays or suppresses large-scale separation and promotes the formation of multiple vortices, whereas increasing the angle of attack generally promotes the formation of a single vortex system. The multiple vortices observed may likely be attributed to small surface distortions in the wing leadingedge region. Comparisons of off-surface determined vortex core location and reattachment point approximation from the vapor-screen technique are made with those from the on-surface techniques of static pressure and oil flow and show generally good agreement. A comparison between quantified vortex features from flight and wind tunnel showed reasonably good agreement over the forward part of the wing for angles of attack from 16 to 20 deg." @default.
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- W1975757887 date "1995-05-01" @default.
- W1975757887 modified "2023-09-26" @default.
- W1975757887 title "Quantifiable vortex features of F-106B aircraft at subsonic speeds" @default.
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- W1975757887 doi "https://doi.org/10.2514/3.46743" @default.
- W1975757887 hasPublicationYear "1995" @default.
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