Effect of fineness ratio on boattail drag of circular-arc afterbodies having closure ratios of 0.50 with jet exhaust at Mach numbers up to 1.30 /
by David E. Reubush and Jack F. Runckel.

Description

Main Author

Reubush, David E.

Related Names

Runckel, Jack F.
Langley Research Center.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration ; 1973.

Subjects

Jet nozzles.
Drag (Aerodynamics)

Note

Prepared at Langley Research Center.
Cover title.

Physical Description

92 p. : ill. ; 27 cm.

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