Skin friction of incompressible turbulent boundary layers under adverse pressure gradients /

Experimental data for skin friction of turbulent boundary layers under adverse pressure gradient are presented from several sources. Data obtained by momentum balance are shown to follow a trend opposite to that of data obtained by a hot-wire and heat-transfer methods. A new integral energy paramete...

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Bibliographic Details
Main Author: Goldschmied, F. R
Corporate Author: United States National Advisory Committee for Aeronautics
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) ; 2431
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Stanford University

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Call Number: NACA TN 2431