Theoretical investigation of submerged inlets at low speeds / Alvin H. Sacks and John R. Spreiter.

The flow field in a submerged inlet is investigated by theoretical, wind-tunnel, and visual-flow stuides. Equations are developed for the growth of the ramp-floor boundary layer for parallel, divergent, and convergent ramp walls; and a general equation is derived relating the boundary-layer pressure...

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Bibliographic Details
Main Author: Sacks, Alvin H.
Corporate Author: United States. National Advisory Committee for Aeronautics
Other Authors: Spreiter, John R.
Other title:Technical report archive and image library.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1951.
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 2323.
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Call Number: Y 3.N 21/5:6/2323
Y 3.N 21/5:6/2323 Available Place a Hold