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Results of heat transfer tests on sharp and spherically blunted 4 deg half angle conical models in a plasma jet and in a hypervelocity wind tunnelHeat transfer tests on sharp and spherically blunted conical graphite nose cones in plasma jet and in hypervelocity wind tunnel
Document ID
19660007297
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hester, J. C. (LTV Aerospace Corp. Dallas, TX, United States)
Martin, D. M. (LTV Aerospace Corp. Dallas, TX, United States)
Date Acquired
August 3, 2013
Publication Date
December 17, 1965
Subject Category
Thermodynamics And Combustion
Report/Patent Number
LTV-00.725
NASA-CR-66040
Report Number: LTV-00.725
Report Number: NASA-CR-66040
Accession Number
66N16586
Funding Number(s)
CONTRACT_GRANT: NAS1-3915
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HYPERVELOCITY WIND TUNNEL
PLASMA JET
GRAPHITE
NOSE CONE
HEAT TRANSFER

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