Wind tunnel investigation of passive vortex control and vortex-tail interactions on a slender wing at subsonic and transonic speeds /

Bibliographic Details
Main Author:	Erickson, Gary E. (Author)
Corporate Author:	United States. National Aeronautics and Space Administration (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, [2013]
Series:	NASA technical memorandum ; 217982.
Subjects:	Leading edges. Aerodynamic configurations. Angle of attack. Canard configurations. Flow visualization. Subsonic speed. Porosity. Transonic speed. Vortices. Reynolds number. Mach number.
Online Access:	https://purl.fdlp.gov/GPO/gpo40586 http://purl.fdlp.gov/GPO/gpo40586

Description
Item Description:	Title from title screen (viewed Oct. 18, 2013). "April 2013."
Physical Description:	1 online resource (521 pages) : illustrations.
Bibliography:	Includes bibliographical references (page 41).