Estimated benefits of variable-geometry wing camber control for transport aircraft /

Bibliographic Details

Main Authors:	Bolonkin, Alexander (Author), Gilyard, Glenn B. (Author)
Format:	Government Document eBook
Language:	English
Published:	Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Center, October 1999.
Series:	NASA technical memorandum ; 1999-206586.
Subjects:	Wing camber. Wind tunnel tests. Transport aircraft. Adaptive control. Cambered wings.
Online Access:	https://purl.fdlp.gov/GPO/gpo83942