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Compressor design requirementsCycle analysis of turbojet and turboprop engines - axial flow compressor requirements for gas turbine engines
Document ID
19650013746
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Bullock, R. O. (NASA Lewis Research Center Cleveland, OH, United States)
Prasse, E. I. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 2, 2013
Publication Date
January 1, 1965
Subject Category
Aerodynamics
Accession Number
65N23347
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AXIAL FLOW COMPRESSOR
TURBOPROP ENGINE
TURBOJET ENGINE
GAS TURBINE
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IDRelationTitle19650013744Collected WorksAerodynamic Design of Axial Flow Compressors19650013744Collected WorksAerodynamic Design of Axial Flow Compressors
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