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Some measurements of a wake-boundary layer interaction by Eichhorn, R., is a nonfiction available to read on EtoBox.

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When a strut or other object is attached to a surface along which a fluid flows, the strut disturbs the boundary layer flow and the wake region of the strut interacts with the boundary layer along the surface giving rise to complicated three dimensional effects. In the present paper these effects were investigated for the geometry consisting of a 2 in. diameter cylinder in uniform axial flow to which was attached normally a 3/16 inch diameter dowel forming a strut. The measurements reported include both static and total pressure surveys in the wake-boundary layer region behind the strut. The resulting wake velocity profiles far from the interaction region behave normally but those within this region do note. The existence of vortices is in some cases clearly seen

Who reads Some measurements of a wake-boundary layer interaction?

Author

Eichhorn, R.,

Publisher

Aeronautical Research Laboratories, Air Force Research Division, Air Research and Development Command, United States Air Force, 1960.

Published

1960

Language

EN

Category

nonfiction