The effects of steady, three-dimensional perturbations in boundary layers /
by Raymond Sedney.

Description

Main Author

Sedney, Raymond.

Related Names

U.S. Army Ballistic Research Laboratory.

Language(s)

English

Published

Aberdeen Proving Ground, Maryland : Ballistic Research Laboratories, 1974.

Subjects

Boundary layer > Boundary layer / Mathematical models.

Summary

The primary purpose of this report is to survey the available information mainly experimental, on the subject. Most attention is given to the complex flow field resulting when a 3-D protuberance is introduced into a laminar boundary layer; less can be said about the turbulent case or 2-D protuberances because enough detailed, careful experiments have not been made. There are some features of the induced flow fields common to all speed ranges; applications range from flow in the atmospheric boundary layer to hypersonic vehicle problems. Some attempts to analyze the downstream flow are also summarized.

Note

"November 1974."

Physical Description

52 pages : illustrations ; 28 cm.

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