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Combustion process influence on stability.Vaporization and atomization theoretically calculated to be controlling parts of combustion process in determining rocket combustion instability
Document ID
19650039757
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Priem, R. J.
Date Acquired
August 2, 2013
Publication Date
May 1, 1965
Subject Category
Thermodynamics And Combustion
Report/Patent Number
AICE PREPRINT 28D
Report Number: AICE PREPRINT 28D
Accession Number
65A22461
Distribution Limits
Public
Copyright
Other
Keywords
VAPORIZATION HEAT
LIQUID ATOMIZATION
ROCKET COMBUSTOR
COMBUSTION STABILITY

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