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Effects of exhaust nozzle recombination of hypersonic ramjet performance. i. experimental investigation of recombination in exhaust nozzlesEffect of exhaust nozzle recombination on hypersonic ramjet performance
Document ID
19640013357
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Franciscus, L. C. (NASA Lewis Research Center Cleveland, OH, United States)
Lezberg, E. A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
August 25, 1963
Subject Category
Facilities, Research, And Support
Report/Patent Number
AIAA PAPER-63-118
Report Number: AIAA PAPER-63-118
Accession Number
64N23271
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
EXHAUST NOZZLE
HYPERSONIC AIRCRAFT
RECOMBINATION
RAMJET ENGINE
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