Cover Image

Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3 /

Bibliographic Details
Main Authors: Stallings, Robert L. (Author), Lamb, Milton (Author)
Corporate Author: Langley Research Center
Format: Government Document eBook
Language:English
Published: [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
Series:NASA technical paper ; 1789.
Subjects:
Boundary layer flow.
Boundary layer stability.
Heat transfer.
Reynolds number.
Wind tunnel tests.
Aerothermodynamics.
Boundary layer.
Supersonic wind tunnels.
Online Access:https://purl.fdlp.gov/GPO/gpo71443
Description
Item Description:Title from title screen (viewed on Aug. 23, 2016).
"December 1980."
"Performing Organization: NASA Langley Research Center"--Report documentation page.
Physical Description:1 online resource (45 pages) : illustrations.
Bibliography:Includes bibliographical references (pages 17-18).