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- W137492615 abstract "In aeronautical and aerospace applications boundary layer and shear layer transition is of interest and importance for small-tomoderate Reynolds numbers. The Reynolds number range of interest spans from, at the low end, the order of 104 for low speed free shear layers to, at the high end, order of 108 for hypersonic boundary layers. Such Reynolds numbers typically occur on either small bodies (i.e., RPV’s), at high altitude/low density (HALE, NASP) or for forebody regions on conventional transports (inlet, empannage, wing and even fuselage). Transition can also be of interest, via laminar flow control, for much of the wing acreage depending upon the type and extent of control utilized. Transition issues of interest include the location of significant wall transport increase (nominal “transition point”), the extent of the transitional flow region and both transition tripping and laminar flow control.KeywordsTransition DelayHypersonic Boundary LayerShear Layer TransitionHigh Lift SystemConventional TransportThese keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves." @default.
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- W137492615 date "1994-01-01" @default.
- W137492615 modified "2023-10-15" @default.
- W137492615 title "Research Status/Requirements and NASA Applications for Wall Layer Transition" @default.
- W137492615 doi "https://doi.org/10.1007/978-94-011-1032-7_1" @default.
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