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Survey of the relationship between theory and experiment for convective heat transfer from rocket combustion gases.Compressible turbulent accelerating boundary layer flow model for convective heat transfer from rocket combustion gases, noting heat flux
Document ID
19690054011
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bartz, D. R.
Date Acquired
August 5, 2013
Publication Date
January 1, 1968
Publication Information
Publisher: TECHNIVISION SERVICES AND CIRCA PUBLICATIONS, INC.,
Subject Category
Thermodynamics And Combustion
Accession Number
69A32000
Funding Number(s)
CONTRACT_GRANT: NASW-6
CONTRACT_GRANT: DA-04-495-ORD-18
Distribution Limits
Public
Copyright
Other

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