Cover Image

Quantitative global heat transfer in a Mach-6 quiet tunnel /

Bibliographic Details
Main Author: Sullivan, John P. (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, [2012]
Series:NASA contractor report ; NASA CR-217331.
Subjects:
Heat transfer.
Hypersonic speed.
Temperature sensitive paints.
Wind tunnel tests.
Hypersonic wind tunnels.
Heat flux.
Mathematical models.
Online Access:https://purl.fdlp.gov/GPO/gpo32903
Description
Item Description:Title from title screen (viewed Jan. 15, 2013).
"February 2012."
Physical Description:1 online resource (148 pages) : color illustrations.
Bibliography:Includes bibliographical references (pages 126-128).