Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a variable-wing-sweep STOL configuration /
by Gerald V. Foster and Odell A. Morris.

Description

Main Author

Foster, Gerald V.

Related Names

Morris, Odell A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

Language(s)

English

Published

Washington, [D.C.] : National Aeronautics and Space Administration, 1960.

Subjects

Mach number.
Aerodynamics.
Airplanes > Airplanes / Wings, Swept-back.
Short take-off and landing aircraft > Short take-off and landing aircraft / Longitudinal stability.

Note

"October 1960."
Cover title.

Physical Description

24 p. : ill. ; 26 cm.

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