Drag reduction due to gas injection through various discrete slots on a three-dimensional wing at Mach 2.01 /
Russell B. Sorrells III, K.R. Czarnecki, and Lorraine F. Satchell.

Description

Main Author

Sorrells, Russell B.

Related Names

Satchell, Lorraine F.
Czarnecki, K. R.
Langley Research Center.
United States. National Aeronautics and Space Administration.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration ; 1969.

Subjects

Turbulent boundary layer > Turbulent boundary layer / Measurement.
Drag reduction.

Physical Description

43 p. : ill. ; 27 cm.

Locate a Print Version

Find in a library

Viewability