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RECOMBINATION AND CONDENSATION IN NOZZLES
Effects of recombination of dissociated or evaporated species during expansion in a rocket nozzle determined in order to predict jet- and rocket-engine performance
Document ID
19630026619
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Olson, W. T.
Date Acquired
August 1, 2013
Publication Date
January 1, 1962
Subject Category
Aircraft
Accession Number
63A22678
Distribution Limits
Public
Copyright
Other
Keywords
NOZZLE EXPANSION
ROCKET NOZZLE
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