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Theoretical Investigation of Submerged Inlets at Low SpeedsThe general characteristics of the flow field in a submerged air inlet are investigated by theoretical, wind-tunnel, and visual-flow studies. Equations are developed for calculating the laminar and turbulent boundary-layer growth along the ramp floor for parallel, divergent, and convergent ramp walls, and a general equation is derived relating the boundary-layer pressure losses to the boundary-layer thickness. It is demonstrated that the growth of the boundary layer on the floor of the divergent-ramp inlet is retarded and that a vortex pair is generated in such an inlet. Functional relationships are established between the pressure losses in the vortices and the geometry of the inlet. A general discussion of the boundary layer and vortex formations is included, in which variations of the various losses and of the incremental external drag with mass-flow ratio are considered. Effects of compressibility are also discussed.
Document ID
19890067876
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Technical Note
Authors
Sacks, Alvin H.
(National Advisory Committee for Aeronautics. Ames Aeronautical Lab. Moffett Field, CA, United States)
Spreiter, John R.
(National Advisory Committee for Aeronautics. Ames Aeronautical Lab. Moffett Field, CA, United States)
Date Acquired
August 14, 2013
Publication Date
August 1, 1951
Subject Category
Aerodynamics
Report/Patent Number
NACA-TN-2323
Accession Number
89N70249
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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