Alleviation of whirl-flutter on a joined-wing tilt-rotor aircraft configuration using active controls
By: Johannes M van Aken].
Contributors: United States. National Aeronautics and Space Administration.
Series: [NASA contractor report] -- NASA CR-196103.
Publisher: American Helicopter Society; National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1991
Place of publication: [Alexandria, Va.]; [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Active control.; Aeroelasticity.; Aircraft configurations.; Dynamic structural analysis.; Joined wings.; Structural stability.; Subsonic flutter.; Tilt rotor aircraft.
Other titles: Alleviation of whirl flutter on a joined-wing tilt-rotor aircraft configuration using active controls.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 94-0868-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994] 1 microfiche.