A closed-form trim solution yielding minimum trim drag for airplanes with multiple longitudinal-control effectors
By: Kenneth H. Goodrich, Steven M. Sliwa and Frederick J. Lallman.
Contributors: Lallman, Frederick J.; Sliwa, Steven M.; Langley Research Center
Publisher: Langley Research Center
Published: 1989
Place of publication: Hampton, Va
Number of pages: 24
Subjects: Aerodynamic balance; Thrust vector control
Notes: Bibliography: p.24.