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A mixing model for rocket engine combustionModel for prediction of rocket engine combustion with performance parameters of gas phase turbulent diffusion, and mixing of oxidizer and fuel vapors
Document ID
19650017000
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Hersch, M. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1965
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TN-D-2881
Report Number: NASA-TN-D-2881
Accession Number
65N26601
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROCKET ENGINE
OXIDIZER
GAS PHASE
COMBUSTION

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