Subsonic investigation of a leading-edge boundary layer control suction system 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 ; 1999-209700.
Subjects:	Boundary layer control. Leading edges. Wind tunnel tests. Flaps (control surfaces) Pressure effects. Subsonic speed. Supersonic transports. Aerodynamic configurations.
Online Access:	https://purl.fdlp.gov/GPO/gpo84803

Description
Item Description:	"December 1999." "Performing organization: NASA Langley Research Center"--Report documentation page.
Physical Description:	1 online resource (128 pages) : illustrations.
Bibliography:	Includes bibliographical references (page 128).