Cover Image

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
Description
Item Description:Title from title screen (viewed March 2, 2016).
"December 1996."
"Performing organization: NASA Langley Research Center, Hampton, VA"--Report documentation page.
Physical Description:1 online resource (iii, 262 pages) : illustrations.
Bibliography:Includes bibliographical references (page 262).