Static stability characteristics at Mach numbers from 1.90 to 4.63 of a 76° swept arrow wing model with variations in horizontal-tail height, wing height, and dihedral /
Dennis E. Fuller.

Description

Main Author

Fuller, Dennis E.

Related Names

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

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration ; 1967.

Subjects

Airplanes > Airplanes / Models > Airplanes / Models / Testing.
Stability of airplanes, Lateral.
Stability of airplanes, Longitudinal.
Airplanes > Airplanes / Wings > Airplanes / Wings / Stability.

Physical Description

116 p. : ill. ; 27 cm.

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