Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65° delta wings varying in leading-edge radius and camber /

Bibliographic Details

Main Author:	McMillin, S. Naomi (Susan Naomi) (Author)
Corporate Author:	United States. National Aeronautics and Space Administration (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Hampton, VA : National Aeronautics and Space Administration, Langley Research Center, December 1996.
Series:	NASA technical memorandum ; 4673.
Subjects:	Delta wings. Flow visualization. Leading edges. Reynolds number. Boundary layer transition.
Online Access:	https://purl.fdlp.gov/GPO/gpo65356