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Compressor and turbine matchingCompressor and gas turbine engine matching - power turbine, turbojet, and turboprop engines
Document ID
19650013761
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Dugan, J. F., Jr. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 2, 2013
Publication Date
January 1, 1965
Subject Category
Aerodynamics
Accession Number
65N23362
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AXIAL FLOW COMPRESSOR
TURBINE ENGINE
GAS TURBINE
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IDRelationTitle19650013744Collected WorksAerodynamic Design of Axial-Flow Compressors
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