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Analysis of nonconstant area combustion and mixing in ramjet and rocket-ramjet hybrid enginesOne-dimensional analysis of variable area mixing and combustion process in supersonic ramjet and rocket-ramjet hybrid engines
Document ID
19660030241
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Dobrowolski, A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1966
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TN-D-3626
Report Number: NASA-TN-D-3626
Accession Number
66N39531
Funding Number(s)
CONTRACT_GRANT: 126-15-09-08-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HYBRID ROCKET
RAMJET ENGINE
BURNING PROCESS

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