Flight-determined, subsonic, lateral-directional stability and control derivatives of the thrust-vectoring F-18 high angle of attack research vehicle (HARV), and comparisons to the basic F-18 and predicted derivatives
By: Kenneth W. Iliff, Kon-Sheng Charles Wang.
Contributors: Wang, Kon-Sheng Charles.; Hugh L. Dryden Flight Research Center.
Series: NASA/TP -- 1999-206573; NASA technical paper -- 1999-206573.
Publisher: National Aeronautics and Space Administration, Dryden Flight Research Center; Available from National Technical Information Service
Published: 1999
Place of publication: Edwards, Calif; Springfield, Va
Language: eng
Number of pages: 83
Subjects: Airplanes -- Control systems.; Angle of attack (Aerodynamics); Hornet (Jet fighter plane); Stability of airplanes, Lateral.; Yawing (Aerodynamics)
Notes: "January 1999."

"Performing organization report number H-2252"--Report documentation page.

Includes bibliographical references.

Performed by NASA Dryden Flight Research Center for the National Aeronautics and Space Administration WU 529-50-04-00-RR-00-000