Estimated benefits of variable-geometry wing camber control for transport aircraft
By: Alexander Bolonkin, Glenn B. Gilyard.
Contributors: Gilyard, Glenn B.; Hugh L. Dryden Flight Research Center.
Series: [NASA technical memorandum] -- NASA/TM-1999-206586.; NASA technical memorandum -- 206586.
Publisher: National Aeronautics and Space Administration, Dryden Flight Research Center; National Technical Information Service, distributor
Published: 1999
Place of publication: Edwards, Calif; Springfield, VA
Language: eng
Format: Microform
Subjects: Wing camber.; Wind tunnel tests.; Transport aircraft.; Adaptive control.; Cambered wings.
Other titles: Estimated benefits of variable geometry wing camber control for transport aircraft.
Notes: Shipping list no.: 2000-0197-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1999] 1 microfiche.