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Subsonic and supersonic longitudinal stability and control characteristics of an aft tail fighter configuration with cambered and uncambered wings and cambered fuselage /
by Samuel M. Dollyhigh.



Main Author: Dollyhigh, Samuel M.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration ; 1974.
Subjects: Fighter planes.
Camber (Aerofoils)
Stability of airplanes, Longitudinal.
Note: Prepared at Langley Research Center.
Cover title.
Physical Description: 96 p. : chiefly ill. ; 27 cm.
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