Shock interference heat transfer to tank configurations mated to a straight-wing space shuttle orbiter at mach number 10.3 /
Davis H. Crawford ; Langley Research Center, Hampton, Va.

Description

Main Author

Crawford, Davis H.

Related Names

United States. National Aeronautics and Space Administration.
Langley Research Center.

Language(s)

English

Published

Washington : National Aeronautics and Space Administration ; 1976.

Subjects

Aerothermodynamics.
Space vehicles.
Heat > Heat / Transmission.

Note

Cover title.

Physical Description

[1], 48 p. : ill. ; 27 cm.

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