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Acceleration of high-pressure-ratio single-spool turbojet engine as determined from component performance characteristics : effect of compressor interstage air bleed
Document ID
19930087589
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Rebeske, John J , Jr
Dugan, James F , Jr
Date Acquired
August 16, 2013
Publication Date
July 3, 1953
Report/Patent Number
NACA-RM-E53E06
Report Number: NACA-RM-E53E06
Accession Number
93R16879
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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