Experimental study of the effectiveness of cylindrical plume simulators for predicting jet-on boattail drag at Mach numberes up to 1.30 /
by David E. Reubush.

Description

Main Author

Reubush, David E.

Related Names

Lanlgely Research Center.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration ; 1974.

Subjects

Cylinders.
Drag (Aerodynamics)
Aircraft exhaust emissions > Aircraft exhaust emissions / Models.
Jet nozzles > Jet nozzles / Models.
Plumes (Fluid dynamics) > Plumes (Fluid dynamics) / Models.

Note

Prepared at Langley Research Center.
Cover title.

Physical Description

156 p. : chiefly ill. ; 27 cm.

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