Aerodynamic characteristics of a swept-wing cruise missile at Mach numbers from 0.50 to 2.86 /
by M. Leroy Spearman and Ida K. Collins.

Description

Main Author

Spearman, M. Leroy.

Related Names

Collins, Ida K.
Langley Research Center.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration ; 1972.

Subjects

Aerodynamics, Transonic.
Aerodynamics, Supersonic.
Cruise missiles > Cruise missiles / Aerodynamics.

Note

Prepared at Langley Research Center.
Cover title.

Physical Description

40 p. : ill. ; 27 cm.

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