Wind tunnel investigation of passive porosity applied to the leading-edge extension and leading-edge flaps on a slender wing at subsonic speed /

Bibliographic Details

Main Author:	Erickson, Gary E. (Author)
Format:	Government Document eBook
Language:	English
Published:	Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, March 2017.
Series:	NASA technical memorandum ; 2017-219596.
Subjects:	Angle of attack. Delta wings. Leading edge flaps. Static pressure. Subsonic speed. Vortices.
Online Access:	https://purl.fdlp.gov/GPO/gpo81470 http://purl.fdlp.gov/GPO/gpo81470