Surface flow angles on an ogive cylinder at angle of attack in supersonic flow /
by Harold R. Vaughn, Oscar L. George, Jr.

Description

Main Author

Vaughn, Harold R.

Related Names

George, Oscar L., Jr., author.
Sandia Corporation.
U.S. Atomic Energy Commission.

Language(s)

English

Published

Albuquerque, New Mexico : Sandia Laboratories, 1971.

Subjects

Liquids.
Body of revolution.
Angle of attack (Aerodynamics)
Aerodynamics, Supersonic.

Summary

The surface flow angle was measured on an ogive cylinder at angles of attack and at supersonic Mach numbers. The results are compared with potential theory which is shown to be inadequate unitl modified.

Note

"Published December 1971."

Physical Description

36 pages : illustrations ; 28 cm.

Locate a Print Version

Find in a library

Viewability