Transonic wind-tunnel investigation of the fin loads of a 1/8-scale model simulating the first stage of the Scout research vehicle /
by Thomas C. Kelly.

Description

Main Author

Kelly, Thomas C.

Related Names

Langley Research Center.

Language(s)

English

Published

Washington : National Aeronautics and Space Administration, [1961]

Subjects

Angle of attack (Aerodynamics)
Aerodynamic load.
Rockets (Aeronautics) > Rockets (Aeronautics) / Fins > Rockets (Aeronautics) / Fins / Testing.

Note

Prepared at Langley Research Center.
"June 1961."
Cover title.

Physical Description

28 p. : ill. ; 26 cm.

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