Rocket-model investigation of lateral stability characteristics and power effects of a jet-engine airplane configuration with tail boom at mach numbers from 1.15 to 1.37 /
by T. Bradley, Jr., and Normal L. Crabill.

Description

Main Author

Curry, T. Bradley.

Related Names

Crabill, Norman L.
United States. National Aeronautics and Space Administration.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration : [1961]

Subjects

Stability and control.
Aerodynamics, aircraft.

Note

Cover title.
"January 1961."
Aerodynamics, aircraft; Stability and control.

Physical Description

29 p. : ill. ; 26 cm.

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