Static stability and control characteristics of an airplane model with tail surfaces outboard of the wing tips at a mach number of 2.01 /
by Cornelius Driver and M. Leroy Spearman.

Description

Main Author

Driver, Cornelius.

Related Names

Spearman, M. Leroy.
United States. National Aeronautics and Space Administration.

Language(s)

English

Published

Washington [D.C.] : National Aeronautics and Space Administration, [1959]

Subjects

Aerodynamics, Supersonic.
Airplanes > Airplanes / Tail surfaces.
Stability of airplanes.

Note

"September 1959."
Cover title.

Physical Description

28 p. : 11 ill. ; 27 cm.

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