A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane
By: Frederick J. Lallman, John B. Davidson, and Patrick C. Murphy.
Contributors: Davidson, John B.; Murphy, Patrick C.; Langley Research Center.
Series: [NASA technical paper] -- NASA/TP-1998-208464.; NASA technical paper -- 208464.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1998
Place of publication: Hampton, Va; Springfield, VA
Language: eng
Format: Microform
Subjects: Thrust vector control.; Fighter aircraft.; Flight control.; Feedback control.; Directional control.; Control stability.; Angular acceleration.; Angle of attack.; F-18 aircraft.
Other titles: Method for integrating thrust vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane.
Notes: Shipping list no.: 1999-0479-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1998] 1 microfiche.