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The effects of injection mass flux distributions and resonant combustion on local heat transfer in a liquid-propellant rocket engineInjection mass flux distributions and resonant combustion effects on local heat transfer in liquid propellant rocket engine
Document ID
19650003676
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Jaivin, G. I. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Rupe, J. H. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 2, 2013
Publication Date
October 1, 1964
Subject Category
Thermodynamics And Combustion
Report/Patent Number
JPL-TR-32-648
NASA-CR-59902
Report Number: JPL-TR-32-648
Report Number: NASA-CR-59902
Accession Number
65N13277
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LIQUID PROPELLANT ROCKET ENGINE
HEAT TRANSFER
PROPELLANT COMBUSTION

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