Effects of wing vertical location on the stability and control characteristics at a mach number of 2.01 of a canard airplane configuration with a trapezoidal aspect-ratio-3 wing /
by Gerald V. Foster.

Description

Main Author

Foster, Gerald V.

Related Names

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 / Wings, Trapezoidal.
Airplanes > Airplanes / Wings, Canard.
Airplanes > Airplanes / Handling characteristics.

Note

"September 1959."
Cover title.

Physical Description

35 p. : 13 ill. ; 27 cm.

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