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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

Internet

https://purl.fdlp.gov/GPO/gpo40586
http://purl.fdlp.gov/GPO/gpo40586

Available Online

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Call Number: NAS 1.15:2013-217982
 
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NAS 1.15:2013-217982 Available