Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring
By: Kenneth W. Iliff, Kon-Sheng Charles Wang.
Contributors: Wang, Kon-Sheng Charles.; Hugh L. Dryden Flight Research Center.; United States. National Aeronautics and Space Administration.
Series: NASA/TP -- 97-206539.; NASA technical paper -- 97-206539.
Publisher: NASA, Dryden Flight Research Center; Available from National Technical Information Service
Published: 1997
Place of publication: Edwards, Calif; Springfield, Va
Language: eng
Number of pages: 65
Subjects: Airplanes -- Control surfaces.; Airplanes -- Control systems.; Angle of attack (Aerodynamics); Hornet (Jet fighter plane); Stability of airplanes, Longitudinal.; Yawing (Aerodynamics)
Notes: "December 1997."

"Performing organization report number H-2175"--Report documentation page.

Includes bibliographical references.

Prepared by NASA Dryden Flight Research Center for National Aeronautics and Space Administration WU 505 68 50 00 R R 00 000