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The use of energy thickness in prediction of throat heat transfer in rocket nozzleEnergy thickness in prediction of throat heat transfer in rocket nozzles using nozzle geometries and temperature ratios
Document ID
19690022491
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Boldman, D. R. (NASA Lewis Research Center Cleveland, OH, United States)
Graham, R. W. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1969
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TN-D-5356
Accession Number
69N31869
Funding Number(s)
CONTRACT_GRANT: 129-01-05-19-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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