Effect of Reynolds number on the subsonic boattail drag of several wing-body configurations /
David E. Reubush ; Langley Research Center, Hampton, Va.

Description

Main Author

Reubush, David E.

Related Names

United States. National Aeronautics and Space Administration.
Langley Research Center.

Language(s)

English

Published

Washington : U.S. National Aeronautics and Space Administration ; 1976.

Subjects

Reynolds number.
Drag (Aerodynamics)

Note

Cover title.

Physical Description

[1], 82 p. : ill., graphs ; 27 cm.

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