Effect of diffusers, shrouds, and mass injection on the starting and operating characteristics of a Mach 5 free jet tunnel /
by John K. Molloy, Ernest A. Mackley, and J. Wayne Keyes.

Description

Main Author

Molloy, John K.

Related Names

Keyes, J. Wayne.
Mackley, Ernest A.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Language(s)

English

Published

Washington : National Aeronautics and Space Administration : 1971.

Subjects

Aerodynamics, Supersonic.
Supersonic wind tunnels.
Diffusers > Diffusers / Aerodynamics.

Note

Prepared at Langley Research Center.
N 71-34243.

Physical Description

30 p. : ill. ; 27 cm.

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