Separation, stability, and other properties of compressible boundary layer with pressure gradient and heat transfer / Morris Morduchow and Richard C. Grape.

A theoretical study is made of the effect of pressure gradient, wall temperature, and Mach number on laminar boundary-layer characteristics and, in particular, on the skin-friction and heat-transfer coefficients, on the separation point in an adverse pressure gradient, on the wall temperature requir...

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Bibliographic Details
Main Author: Morduchow, Morris
Corporate Author: United States. National Advisory Committee for Aeronautics
Other Authors: Grape, Richard G.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1955.
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 3296.
National Advisory Committee for Aeronautics ; 3296.
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Call Number: Y 3.N 21/5:6/3296
Y 3.N 21/5:6/3296 Available Place a Hold