Effect of canard leading-edge sweep and dihedral angle on the longitudinal and lateral aerodynamic characteristics of a close-coupled canard-wing configuration /
by Blair B. Gloss.

Description

Main Author

Gloss, Blair B.

Related Names

Langley Research Center.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration ; 1974.

Subjects

Stability of airplanes, Lateral.
Stability of airplanes, Longitudinal.
Leading edges (Aerodynamics)
Airplanes > Airplanes / Wings, Canard.

Note

Prepared at Langley Research Center.
Cover title.

Physical Description

68 p. : ill. ; 27 cm.

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