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: Sliwa, Steven M.; Lallman, Frederick J.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Series: NASA technical paper -- 2907.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division; For sale by the National Technical Information Service]
Published: 1989
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Airplanes -- Design and construction.
Other titles: Closed form trim solution yielding minimum trim drag for airplanes with multiple longitudinal control effectors.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1989. 1 microfiche ; 11 x 15 cm.