Effect of camber on the trimmed lift capability of a close-coupled canard-wing configuration /
Blair B. Gloss, Langley Research Center.

Description

Main Author

Gloss, Blair B.

Related Names

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

Language(s)

English

Published

[Washington] : National Aeronautics and Space Administration : 1978.

Subjects

Airplanes > Airplanes / Wings, Canard.
Camber (Aerofoils)

Note

July 1978.

Physical Description

91 p. : ill. ; 27 cm.

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