Lateral directional stability characteristics at mach 2.3 to 3.5 of a supersonic transport model with various outboard vertical-tail locations /
by William A. Corlett.

Description

Main Author

Corlett, William A.

Related Names

Langley Research Center.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration ; 1965.

Subjects

Tail assemblies.
Swept wings.
Supersonic transports.
Supersonic speed.
Stabilizers (fluid dynamics).
Position (location).
Mach number.
Lateral stability.
Directional stability.
Body-wing and tail configurations.
Aircraft models.
Aerodynamic stability.

Note

"NASA TM X-1151"--Cover.
"Langley Research Center, Langley Research Center, Hampton, Va."--Cover.
"August 1965"--Cover.
Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 7/28/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19650025803_1965025803.pdf.

Physical Description

30 p. : ill. ; 27 cm.

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