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Subsonic investigation of leading-edge flaps designed for vortex- and attached-flow on a high-speed civil transport configuration /

Bibliographic Details
Main Author: Campbell, Bryan A. (Author)
Format: Government Document eBook
Language:English
Published: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, December 1999.
Series:NASA technical memorandum ; 1999-209701.
Subjects:
Subsonic wind tunnels.
Leading edge flaps.
Vortices.
Supersonic transports.
Aerodynamic configurations.
Separated flow.
Online Access:https://purl.fdlp.gov/GPO/gpo84807
Description
Item Description:"December 1999."
"Performing organization: NASA Langley Research Center"--Report documentation page.
Physical Description:1 online resource (103 pages) : illustrations.
Bibliography:Includes bibliographical references (pages 102-103 ).