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Author Sullivan, John P., author.

Title Quantitative global heat transfer in a Mach-6 quiet tunnel [electronic resource] / John P. Sullivan [and ten others].

Publication Info. Hampton, Va.: National Aeronautics and Space Administration, Langley Research Center, [2012]
Connect to
Connect to https://permanent.fdlp.gov/gpo32903/20120002664-2012002700.pdf
Connect to https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20120002664.pdf

Copies

Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.26:2012-217331    ---  Available
Description 1 online resource (148 pages) : color illustrations.
text txt rdacontent
computer c rdamedia
online resource cr rdacarrier
Series [NASA contractor report] ; NASA-CR 2012-217331
NASA contractor report ; NASA CR-217331.
Note Title from title screen (viewed Jan. 15, 2013).
"February 2012."
Bibliography Includes bibliographical references (pages 126-128).
Funding Prepared for Langley Research Center under cooperative agreement NNX08AC97A 599489.02.07.07.04.11.01
Subject Heat transfer.
Hypersonic speed.
Temperature sensitive paints.
Wind tunnel tests.
Hypersonic wind tunnels.
Heat flux.
Mathematical models.
Added Author Langley Research Center, issuing body.
United States. National Aeronautics and Space Administration, sponsoring body.
Gpo Item No. 0830-H-14 (online)
Sudoc No. NAS 1.26:2012-217331

 
    
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