Preliminary experimental investigation of low-speed turbulent boundary layers in adverse pressure gradients / Virgil A. Sandborn.

Measurements of velocity profiles and skin friction in subsonic turbulent boundary layers with adverse pressure gradients are presented. The skin friction was measured by using a local heat-transfer instrument and employing a calibrated relation between heat transfer and skin friction.

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Bibliographic Details
Main Author: Sandborn, Virgil A.
Corporate Author: United States. National Advisory Committee for Aeronautics
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1953.
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 3031.
Subjects:

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Call Number: Y 3.N 21/5:6/3031
Y 3.N 21/5:6/3031 Available Place a Hold