NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Shock Tube Study of the Thermal Conductivity of ArgonAnalysis of end-wall thermal boundary layer behind reflected shock to determine thermal conductivity of argon over temperatures 3150 to 9225 K
Document ID
19670027090
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bunting, J. O. (Stanford Univ. CA, United States)
Devoto, R. S. (Stanford Univ. CA, United States)
Date Acquired
August 3, 2013
Publication Date
July 1, 1967
Subject Category
Thermodynamics And Combustion
Report/Patent Number
SUDAAR-313
SU-IPR-176
NASA-CR-88360
Report Number: SUDAAR-313
Report Number: SU-IPR-176
Report Number: NASA-CR-88360
Accession Number
67N36419
Funding Number(s)
CONTRACT_GRANT: NGR-05-020-091
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
THERMAL BOUNDARY LAYER
HIGH TEMPERATURE RESEARCH
ARGON

Related Records

There are no records associated with this record.
No Preview Available