Jet effects on cylindrical afterbodies housing sonic and supersonic nozzles which exhaust against a supersonic stream at angles of attack from 90 ̊to 180 ̊/
by Lovick O. Hayman, Jr., amd Russell W. McDearmon.

Description

Main Author: Hayman, Lovick O.
Related Names: McDearmon, Russell W.
Langley Research Center.
Language(s): English
Published: Washington : National Aeronautics and Space Administration, [1962]
Subjects: Aerodynamics, Supersonic.
Cylinders.
Aerodynamic load.
Angle of attack (Aerodynamics)
Jet nozzles.
Jets > Jets / Fluid dynamics.
Note: Prepared at Langley Research Center.
"March 1962."
Cover title.
Physical Description: 49 p. : ill. ; 26 cm.
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Item Link	Original Source
Full view	University of Illinois at Urbana-Champaign