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Investigation of turbines suitable for use in a turbojet engine with high compressor pressure ratio and low compressor-tip speed VIII : internal flow conditions of a two-stage turbine with a downstream stator
Document ID
19930089969
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Petrash, Donald A
Davison, Elmer H
Schum, Harold J
Date Acquired
August 16, 2013
Publication Date
November 13, 1957
Report/Patent Number
NACA-RM-E57I19
Accession Number
93R19259
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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